source report
Green Energy and Technology
Panagiotis Grammelis Editor
Energy, Transportation and Global Warming
Green Energy and Technology
More information about this series at http://www.springer.com/series/8059
Panagiotis Grammelis
Editor
Energy, Transportation and Global Warming
Editor Panagiotis Grammelis Chemical Process and Energy Resources Institute Centre for Research and Technology Hellas Athens, Greece
ISSN 1865-3529 ISSN 1865-3537 (electronic) Green Energy and Technology ISBN 978-3-319-30126-6 ISBN 978-3-319-30127-3 (eBook) DOI 10.1007/978-3-319-30127-3
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Preface
This book is associated with the Global Conference on Global Warming: Focus on
Energy-Transport-Greenhouse Effects, held in Athens on May 24–27, 2015. Objec-
tives are in accordance with the conference’s presentations and mainly concern the exchange of technical information, dissemination of high-quality research results
and presentation of new policy and scientific developments, while promoting future
priorities for a more sustainable development and energy security.
In particular, energy-related issues in all engineering disciplines for a wide area
of applications in the renewables and fossil fuels sectors are described, incorporat-
ing cross-cutting effects. It includes main aspects of transportation discipline with
emphasis on the elimination of the impact on greenhouse effects.
High-quality technical knowledge and research results from specific test cases
around the world are being analysed, providing a holistic view in the main aspects
of the Global Warming issue. The latter also concern current policies and emissions
from air and maritime transport, in addition to the fossil fuel applications. Novel
technologies such as Carbon Capture and Storage are investigated along with
process/systems analysis and optimization for mitigating CO2 emissions. Water
resources management and waste water treatment as well as waste management
issues are also tackled. Biomass, hydrogen and solar energy technologies are
presented along with an insight on green buildings.
The utmost scope of this book is to contribute to the scientific community, since
it includes scientific approaches from many organisations around the globe,
presenting key issues, challenges and research results in a variety of scientific
areas that relate to the Global Warming effects.
Athens, Greece Panagiotis Grammelis
v
Contents
Part I Global Warming and Climate Change:
General Issues and Challenges
General Aspects of Global Warming, Current Policies
and Challenges Policies and General Aspects of Global
Warming with Focus on Specific Examples
1 Urban Development Policy and Urban Sprawl
in Turkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
Münevver Özge Balta
2 Perspectives on the Implementation of Climate Change Public Policies in Brazil . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
Rommel de Santana Freire, Monica Carvalho,
Charles Ulises de Montreuil Carmona, and
Alexandre Magno Vieira Gonçalves de Brito
3 30 Years Air Temperature Data Analysis in Athens
and Thessaloniki, Greece . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
T. Slini and K.T. Papakostas
4 Mitigation and Adaptation Policies Related to Climate
Change in Greece . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35
I. Sebos, A. Progiou, L. Kallinikos, P. Eleni, I. Katsavou,
K. Mangouta, and I. Ziomas
5 Assessing Air Quality in the Urban Environment:
the Gender Gap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 51
Theodora Slini and Fotini-Niovi Pavlidou
vii
6 Promotion of Sustainability by Quantifying
and Reducing the Carbon Footprint:
New Practices for Organizations . . . . . . . . . . . . . . . . . . . . . . . . . . . 61
Monica Carvalho, Rommel de Santana Freire,
and Alexandre Magno Vieira Gonçalves de Brito
Part II Global Warming and Climate Change:
General Issues and Challenges
Climate Change Mitigation Measures and Prospects
7 Group Comparison, Trends and Cluster Analysis
to Understand Historical Precipitation . . . . . . . . . . . . . . . . . . . . . . 77
Raphael Abrah~ao
8 Ground Response to Global Warming . . . . . . . . . . . . . . . . . . . . . . 89
Mohamad Kharseh and Mohammed Al-Khawaja
9 Specific Case: Regional Estimates of Global Climate Change: A Dynamical Downscaling Approach to Southeast Europe . . . . . . . 99
Rafaella-Eleni P. Sotiropoulou, Efthimios Tagaris,
Andreas Sotiropoulos, Ioannis Spanos, Panagiotis Milonas,
and Antonios Michaelakis
Part III Global Warming and Climate Change:
General Issues and Challenges
Climate Change Observatory
10 Drought Conditions in Turkey Between 2004 and 2013
Via Drought Indices Derived from Remotely Sensed Data . . . . . . . 113
Nazila Molavizadeh, Elif Sertel, and Hande Demirel
11 Carbon Foot Print of a Passanger Aircraft Engine
at Landing and Take-Off Cycle . . . . . . . . . . . . . . . . . . . . . . . . . . . 123
Yasin Ş€ohret and T. Hikmet Karakoç
12 Greenhouse Gas Emissions Trends from Waste in Greece . . . . . . . 131
L. Kallinikos, I. Sebos, A. Progiou, P. Eleni, I. Katsavou,
K. Mangouta, and I. Ziomas
Part IV Global Warming and Climate Change:
General Issues and Challenges
Climate Prediction Tools
13 Development of Models for the Estimation of Global
Solar Radiation Over Selected Stations in India . . . . . . . . . . . . . . . 149
M. Maroof Khan, M. Jamil Ahmad, and Basharat Jamil
viii Contents
14 Effect of Gap Between Absorber Plate and Condenser
Cover on the Performance of a Solar Still . . . . . . . . . . . . . . . . . . . . 161
Basharat Jamil and Naiem Akhtar
15 Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative Analysis for Natural Working Fluids . . . . . . . . . . . 175
Önder Kizilkan, Sandro Nižetić, and Gamze Yildirim
16 Rainfall Trend Analysis in the Region of Curitiba
Using Regional Climate Model Scenarios . . . . . . . . . . . . . . . . . . . . 193 Robinson Ploszai and Miriam Rita Moro Mine
17 Modelling of Wind Speed Using Artificial Neural Networks
for University Campus of Burdur (Turkey) . . . . . . . . . . . . . . . . . . 209 Alper Kerem, Önder Kizilkan, and Serdar Salman
18 Cultural Landscapes as a Means of Energy Reduction
at Global Warming . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 223
Afroditi Venetsanou, Alexandros-Theodoros Venetsanos,
and Lena Mantziou
Part V Energy Technologies and Their Effect
on Global Warming
Solar Energy
19 Solar-Driven Continuous Methane Reforming Reactor . . . . . . . . . 249
M. Lange, J. Lapp, R. Rieping, L. de Oliveira, M. Roeb,
and C. Sattler
20 Specific Applications/Examples: Use of Solar Energy
in Fishing: Community Initiatives . . . . . . . . . . . . . . . . . . . . . . . . . . 257 J. Vincent Jain and Satish Babu
21 Diagnostic of Sensors for Induction Machine Powered
by Photovoltaic Generator Based on Fuzzy Logic Techniques . . . . 269
A. Amrane, A. Larabi, and A. Hamzaoui
22 Air Conditioning Based on Hydroxides with Solar Driving
for Low GHG Emissions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 285
R.J. Romero, S. Silva-Sotelo, Y.R. Galindo-Luna,
C.V. Valdéz-Morales, J. Ibarra-Bahena, A. Hdz-Jasso,
and A. Rodrı́guez-Martı́nez
23 Life Cycle Analysis as a Decision Criterion
for the Implementation of Solar Photovoltaic Panels in as Northeast Brazil Hospital . . . . . . . . . . . . . . . . . . . . . . . . . . . . 295
Monica Carvalho, Danielle Bandeira de Mello Delgado,
and Ricardo Chacartegui
Contents ix
Part VI Energy Technologies and Their Effect
on Global Warming
Green Buildings Technology
24 Energy Conservation Through Sunrays Reflecting Coating
on Buildings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 315
Imre Benk€o
25 Comparison of Heating and Cooling Loads of a Typical
Building with TRNSYS and eQUEST . . . . . . . . . . . . . . . . . . . . . . . 327
E. Bellos, C. Tzivanidis, A. Kouvari, and K.A. Antonopoulos
26 Optimum Insulation Thickness for Cooling Applications
Through Exergy Analysis and Environmental Methods . . . . . . . . . 339
Beyza Nur Daldal, İbrahim Sarıo�glu, Gülcan Özel Erol, Emin Açıkkalp, and Hasan Yamık
27 Novel Tungsten Bronze Nanoparticles for Shielding
Near Infrared Ray and Decreasing CO2 Emission . . . . . . . . . . . . . 349
Tsugio Sato, Chong-shen Guo, and Shu Yin
28 Modelling of a Solar Assisted Floor Heating System
with TRNSYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 355
E. Bellos, C. Tzivanidis, A. Prassas, and K.A. Antonopoulos
Part VII Energy Technologies and Their Effect
on Global Warming
Bioenergy–Biofuel Technologies
29 Biogas Production from Napier Grass at Various
Cutting Intervals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 375
Nusara Sinbuathong, Yuwadee Sangsil, and Suriya Sawanon
30 Sustainability Assessment of Fuels Production
via Hydrotreating Waste Lipids and Co-processing
Waste Lipids with Petroleum Fractions . . . . . . . . . . . . . . . . . . . . . 387
Stella Bezergianni and Loukia P. Chrysikou
Part VIII Energy Technologies and Their Effect on Global Warming
Hydrogen Energy and Technologies
31 Spark-Ignition Engine Fueled with Methane-Hydrogen
Blends . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 405
G.M. Kosmadakis, F. Moreno, J. Arroyo, M. Mu~noz, and C.D. Rakopoulos
x Contents
32 Hydrogen Fueled Airplanes, Test Case: Aviation in Libya . . . . . . . 421
Satya P. Bindra, Ali Alwafi, Ashour Saasi, Elbahlul Musa Abogrean,
Mohsen Masaud A. Maatugh, and Khaled Khalifa
33 Perspectives of Hydrogen Automotive Applications in Croatia . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 433
Ankica Ðukić, Ivan Güttler, and Robert Pašičko
Part IX Energy Technologies and Their Effect
on Global Warming
Fossil Fuels and Climate Change
34 Contribution to Multi-Criteria Evaluation of the Impacts of Air Pollution: Case of Cement Plant
(Ain Touta-ALGERIA) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 451
Lylia Bahmed, Samia Daas, Mourad Chebila,
and Loubna Khadoudja Aggabou
35 Environmental Impact Assessment of Electricity
Production, A Case Study of Turkey . . . . . . . . . . . . . . . . . . . . . . . . 463
Fatih Yılmaz, M. Tolga Balta, Reşat Selbaş,
and Do�gan Demiral
36 Hybridization of Parabolic Trough Power Plants
with Natural Gas Through Integration of Industrial
Gas Turbines . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 475
Tobias Vogel, Gerd Oeljeklaus, and Klaus G€orner
Part X Energy Technologies and Their Effect
on Global Warming
Thermodynamic System Analysis and Optimization
37 Performance Analyses of CO2-N2O Cascade System
for Cooling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 499
Fatih Yılmaz, Reşat Selbaş, Arif Emre Özgür,
and M. Tolga Balta
38 Comparison of Thermal Repowering Alternatives
for Thermal Power Plants . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 513
M. Zeki Yilmazoglu
39 Experimental Study of Heat Transfer for a Non-Newtonian
Fluid in a Heated Cylindrical Pipe . . . . . . . . . . . . . . . . . . . . . . . . . 527
Mounir Mellal, Hacina Abchiche, and Sabrina Ait Ouazzou
40 The SOC Estimation of LCO Battery Based on BP Neural
Network . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 543
Sy-Ruen Huang, Yen-Huai Ma, Jheng-Shyun Li,
and Jun-Han Chan
Contents xi
41 Investigating the Effect of Different Refrigerants
on the Performance of a Supercritical Organic
Rankine Cycle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 553
Duygu Melek Çakıcı and Can Özgür Çolpan
Part XI Environmental Technologies Related
to Global Warming
Carbon Capture and Storage (CCS)
and Geotechnology Issues
42 CaO-Based Sorbents for Post Combustion CO2 Capture
via Carbonate Looping . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 571
Zinovia Skoufa, Andy Antzara, Ioannis Milios, Eleni Heracleous,
and Angeliki A. Lemonidou
43 Kinetics of CO2 Capture by Carbon Dioxide Binding
Organic Liquids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 591
Ozge Yuksel Orhan, Hakan Kayi, and Erdogan Alper
44 Flue Gas CO2 Sequestration by Turkish Coal Fly Ashes
and Anatolian Geothermal Hot Waters . . . . . . . . . . . . . . . . . . . . . 605
Yıldırım İsmail Tosun
45 Geo.: Gas Production in Offshore Reservoirs in Brazil’s Pre-salt Region . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 617
Isabella Vaz Leal da Costa, Pedro Rochedo, Mariana Império,
Alexandre Salem Szklo, and Roberto Schaeffer
Part XII Environmental Technologies Related
to Global Warming
Water Resources and Management Issues
46 Spatial and Temporal Patterns of the Water Quality
in the Hammam Boughrara Reservoir in Algeria . . . . . . . . . . . . . . 635
Belkheir DJELITA, Souaad Bouzid-Lagha,
and Kheira Camellia NEHAR
47 Natural Tracers for Identifying Causes of the Quality
Reduction in Groundwater Emerging Along the Aegean
Volcanic Arc (Greece) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 655
E. Dotsika and P. Chantzi
48 Experimental Study of Longitudinal Dispersion
on Trapezoidal Open Channel . . . . . . . . . . . . . . . . . . . . . . . . . . . . 667
Ali Mansour Lagoun and Salim Benziada
xii Contents
49 Mygdonia Basin (N. Greece) in the View of Isotope
Geochemistry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 677
P. Chantzi and E. Dotsika
50 Sustainable Management of Sewage Sludge Conditioning and Valorization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 685
S. Igoud, F. Souahi, and C.-E. Chitour
51 Photocatalytic Degradation of Tylosin and Spiramycin
in Water by Using TiO2 and ZnO Catalysts Under UV Radiation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 695
D. Tassalit, N. Chekir, O. Benhabiles, F. Bentahar,
and N.A. Laoufi
52 Comparison Between the Photocatalytic Degradation
of a Textile Dye Under Sun Light and Artificial Irradiation . . . . . . 707
N. Sahraoui, N. Chekir, and D. Tassalit
53 Vulnerability and Impact of Climate Change Processes on Water Resource in Semi-Arid Areas: In Essaouira
Basin (Morocco) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 719
Salah Ouhamdouch, Mohammed Bahir, Abdellatif Souhel,
and Carreira Paula
Part XIII Environmental Technologies Related
to Global Warming
Waste Management
54 Experimental Study of Transverse Mixing
of Pollutants in Trapezoidal Open Channel . . . . . . . . . . . . . . . . . . 741
Ali Mansour Lagoun and Salim Benziada
55 Elimination of Micropollutent Lysine Acetylsalicylate
by Adsorption on Natural and Synthetical Supports . . . . . . . . . . . . 755
Amel Djouadi and Fatiha Bentahar
56 Integrated System for Optimized Data Collection
and processing of End of Life Tires: Case of Greece . . . . . . . . . . . . 759
Panagiotis Vounatsos, John Vournas, George Mavrias,
and Panagiotis Grammelis
57 Smart Recovery of Materials and Upgrade of Organic
Compost and RDF in Existing Mechanical Biological
Treatment Plants by Using NIR Technology . . . . . . . . . . . . . . . . . . 771
Dimitrios-Sotirios Kourkoumpas, Georgios Kontopoulos,
Ioannis Vournas, Dimitrios Koulocheris, Panagiotis Grammelis,
and Emmanouel Kakaras
Contents xiii
Part XIV Securing Sustainable Mobility to Mitigate
Climate Change
Transport Operation and Resilience Issues
58 Road Transport Induced GHG Emissions Calculation
for Urban Transportation Networks: The Case of Athens
and Thessaloniki in Greece . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 783
Christos Samaras, Iraklis Stamos, Leonidas Ntziachristos,
Evangelos Mitsakis, Zissis Samaras, and Georgia Ayfantopoulou
59 The Effect of Parameter Selection on Fume Formation Rate
in SMAW of AH36 Shipbuilding Steel and Analysis
with ANOVA Method . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 795 Tolga Mert, Levent Bilgili, Kutsi Mert Senoz,
U�gur Bu�gra Çelebi, and Serkan Ekinci
60 An Online Visualization Tool for Assessing the Robustness
of Multimodal Transport Networks in Case of Extreme Weather Events and Natural Hazards . . . . . . . . . . . . . . . . . . . . . . 803
Iraklis Stamos, Evangelos Mitsakis, and Georgia Aifadopoulou
Part XV Securing Sustainable Mobility to Mitigate
Climate Change
Climate Impact Effects of Air and Maritime Transport
61 Manmade Changes in Cirrus Clouds from 1984 to 2007: A Preliminary Study . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 827
Kostas Eleftheratos, Gunnar Myhre, Patrick Minnis,
Ioannis Kapsomenakis, and Christos Zerefos
62 Emission Routing in Maritime Transportation . . . . . . . . . . . . . . . . 837
Levent Bilgili and Ugur Bugra Celebi
63 Pollution Effects Onboard and Its Generated Solution
for Minimized Pollution Effect . . . . . . . . . . . . . . . . . . . . . . . . . . . . 851 Munir Suner and Tankut Yildiz
64 Carbon-Mitigating Air Transport: Analysis
of Current Policy Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . 867 Ioanna Pagoni and Voula Psaraki-Kalouptsidi
65 Ship Life Cycle Greenhouse Gas Emissions . . . . . . . . . . . . . . . . . . 883
Stefanos Chatzinikolaou, Nikolaos Ventikos, Levent Bilgili,
and Ugur Bugra Celebi
xiv Contents
Part I
Global Warming and Climate Change: General Issues and Challenges
General Aspects of Global Warming, Current Policies and Challenges Policies and General Aspects of Global Warming
with Focus on Specific Examples
Chapter 1
Urban Development Policy and Urban Sprawl in Turkey
Münevver €Ozge Balta
Introduction
Metropolitan areas are rapidly changing in response to urban development dynam-
ics. Urban sprawl is defined as a form of urbanization which inefficient,
low-density, suburban development around the periphery. Sprawl is a leading
process at the edges of urban growth and implies deficient and weak planning
control on land policy.
Since the beginning of twentieth century, the world population has increased
dramatically, and especially metropolitan areas have undergone diverse structural
changes. As many other developing countries, Turkey was faced with the fast
urbanization which necessitated immediate formulation of new planning policies
in metropolitan areas. Metropolitan development areas have spread out into rural
areas, so planning policies supposedly regulate this new pattern of development.
In Turkey, local governments frequently use partial plans with a tendency for
discontinuity for urban fringe areas. In actuality, the urban space is patchy and the
applications can be different from the plan decisions. Partial plans may completely
change the urban settlement character. Since 1980, urban development in metro-
politan areas in Turkey has been especially piecemeal, rather than holistic. So, in
the process, urban development planning has tended to be piecemeal, resulting
urban sprawl.
M.Ö. Balta (*) Department of Architecture, Faculty of Architecture and Design, Aksaray University,
68100 Aksaray, Turkey
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_1
5
This paper is concerned with the notion of urban sprawl, particularly planning
policies in metropolitan areas. It aims to discuss the impacts of planning tools and
regulations for urban sprawl. The paper also investigates a research problem that
could show the characteristic of metropolitan development and planning procedure
in Turkey.
Urban Sprawl
“Urban sprawl” is used to describe low-density, inefficient, suburban development
around the periphery. Sprawl is defined as a form of urbanization distinguished by
leapfrog development, commercial strips, low density, separated land uses, auto-
mobile dominance and a minimum of public open space (Table 1.1).
Squires (2002) defines sprawl as “a pattern of urban and metropolitan growth that
reflects low density, automobile-dependent, exclusionary new development on the
fringe of settled areas often surrounding a deteriorating city”. Urban sprawl is a
consequence of many factors, such as the need for industrial establishment for larger
and less expensive locations which force them to move out of the city centre where
they were previously settled, the increasing mobility of middle and high income
groups due to private car ownership and changing socio economic value systems.
Urban sprawl is a consequence of many factors, such as the need for industrial
establishment for larger and less expensive locations which force them to move out
of the city centre where they were previously settled, the increasing mobility of
middle and high income groups due to private car ownership and changing socio
economic value systems (Balta and Eke 2011).
European Environment Agency defines the stimulants of urban sprawl as macro
economic factors, micro-economic factors, demographic factors, housing prefer-
ences, inner city problems, transportation and regulatory frameworks (Table 1.2).
Sprawl is the leading edge of urban growth and implies deficient and weak planning
control on land subdivision.
Table 1.1 Characteristics of sprawl (Ewing 1997)
Leapfrog or scattered
development
It means subdivisions shopping centers and office parks widely
spread apart
Commercial strip
development
It is characterized by huge roads with shopping centres,
gas-stations, fast-food restaurants, banks, parking lots, etc.
Low density Suburban buildings are often single-story and widely spaced,
with intervening parking lots and roadways
Large expanses of single-use
development
Housing consist predominantly of single-family homes on indi-
vidual lots
Poor accessibility (Automo-
bile dominance)
The longer distances between activities
Lack of public open space In suburban area, public open space can be difficult to find
except school yard
6 M.Ö. Balta
In summary, some scholars (Beauregard 2006; Gillette 2005; Teaford 2006) thus
conclude that urban sprawl should be accepted as one of the forms of metropolitan
growth while others (Burchell et al. 1998; Cox and Utt 2004; Ewing et al. 2002;
Snyder and Bird 1998) condemn urban sprawl because of its detrimental affects
such as social segregation, upheave and change or economic prosperity; urban
sprawl is one of the evitable spatial attributes of metropolitan development (Balta
and Eke 2011).
There are two main reasons of urban sprawl. First reason is lack of laws and
regulations supporting planning, second, reason is lack of goodwill and determina-
tion of local authorities to keep the urban macroform as planned.
Urban Sprawl and Energy Consumption
In the last years, cities have gone through problems as global climate change.
Together with the urban growth, greenhouse gases (GHGs) are receiving increas-
ingly more attention (Glicksman 2007). The rise in population and individual car
ownership is mainly attributed to urban sprawl. Suburban areas is often believed to
Table 1.2 Stimulants of urban sprawl (EEA 2006)
Economic factors Macro-economic Globalization
Economic development
Integration
Micro-economic Quality of life
Land value
Land availability
Competition between local governments
Demographic factors Population growth
Increase in household formation
Physical factors Housing Housing preferences
More space per person
Urban problems Poor air quality
Small houses
Noise
Unsafe urban environment
Lack of open and green areas
Poor quality of schools
Transportation Private car ownership
Roads accessibility
Fuel cost
Lack of public transportation
Urban planning Weak land use planning
Lack of enforcement of existing plans
Lack of coordination and organization
1 Urban Development Policy and Urban Sprawl in Turkey 7
be less energy efficient than urban core. Overall energy consumption of a territory,
especially as far as travel energy consumption is concerned with urban sprawl
(Ewing 1994).
Urban sprawl is a consequence of many factors, such as the need for industrial
establishment for larger and less expensive locations which force them to move out
of the city centre where they were previously settled, the increasing mobility of
middle and high income groups due to private car ownership and changing socio
economic value systems.
Urban sprawl has many effects on urban environment as unplanned expansion of
the city may not coordinate with the public transportation system which brings loss
of time in journeys towards the city centre, increased energy consumption and
increased traffic congestion. Motorization has increased energy demand.
Urban Development Policy in Turkey
Metropolitan growth of Turkey is due to fast urbanization and results in urban
sprawl. The formulation and implementation of urban development plans in Turkey
is guided by the statutory provisions of the country’s planning system. The multiple
plans are lack of determined policies and the multiplicity of speculative market
forces and their heavy demands in Turkey. Thus, metropolitan growth was
transformed into an oil-spill form in most of the Turkish cities.
Metropolitan areas have been attracting a large population from rural areas since
the 1960s. Although the rate of migration has slowed down in the last two decades,
it has caused a considerable increase in the population of the metropolitan areas of
Turkey (Erkip 2005). Turkey was urbanizing fast, changing from an agriculture to
an urban-based economy. Two major steps were taken in 1960s. A new ministry of
planning was established to deal with planning, housing and infrastructural issues,
being responsible to draw urban development strategies, to undertake housing
programmes and improvement of squatter housing, and above all to approve all
plans prepared and adopted in local municipal councils (Balta and Eke 2011).
The new value systems, procedures and concepts brought to the era by global-
ization, privatization and neoliberalism affected Turkey as well. Two major reforms
were undertaken in the Turkish planning system in 1984. Besides the classical
municipal administration for cities, metropolitan municipalities were established
responsible for larger cities to plan and control the metropolitan region and the
municipalities in that area, the Metropolitan Planning Offices being joined to the
metropolitan municipalities. Metropolitan planning offices were established in
large cities with the collaboration of both local and central authorities which had
the aim of formulating new policies, models and methods to confront the negative
consequences of metropolitanism. The second major reform was the decentraliza-
tion of several administrative powers including planning. The local authorities were
now responsible for all the stages of planning practice, several administrative
powers including approval (Balta and Eke 2011).
8 M.Ö. Balta
In Turkey, local municipalities is flexible regulation of urban development. Cities
can be changed by partial plans or planning decisions (Ozuduru and Varol 2009).
This process has led to piecemeal implementation through partial plans and plan
amendments in metropolitan areas.
As many other developing countries Turkey was faced with the problem of fast
urban growth. However, the globalisation trends coupled with the decentralization
demands of the age which also affected Turkey caused the abolishment of the
planning units, leaving the ground to local authorities which could not stand against
the pressures of market forces so easily and urban sprawl has been occurred.
In Turkey, urban development plans are detailed end-state blueprint plans,
which envision that a time would come and the spatial development of any city
would be completed in the specific planning period. The allegation of the planning
system is to control every detail during urban development. Development plans, of
which structure and content are defined in planning legislation, are the main
planning control tools in the Turkish system. Urban Development Law (3194),
issued in 1985, exists at the very center of this legislation and is the main law
directly related to production of the urban built environment (Ünlü 2005).
Urban planning in Turkey are guided by the statutory provisions of the country’s
planning system. In metropolitan cities, master plans are prepared by metropolitan
municipalities, and implementation plans by county municipalities, and are then
approved. The process stimulates the development of entities’ individual behavior,
and individual acts come to the foreground primarily through piecemeal
implementations as partial plans and plan amendments. Local governments fre-
quently use partial plans for the purpose of steering the public benefit. In actuality,
the urban space is broken into pieces and is privatized through these plans, and
public spaces are turned over to the private sector through urban projects/partial
plans. To allay reactions that the public may put forth, local governments define the
plans in planning regulations and apply the procedures anticipated by the law
predominantly in a stylistic manner, thereby rendering the applications different
from the plan decisions. Partial plans may completely change the urban settlement
character as urban sprawl. Since 1980, urban development in metropolitan areas in
Turkey has been primarily incremental rather than holistic. In the process, urban
development planning has tended to be piecemeal, resulting in the fragmentation of
the urban built environment (Balta et al. 2012).
In 1980s, after the legal arrangements, the central government’s role in planning
has diminished, and authority has been decentralized to local governments. How-
ever, in metropolitan areas, the limited capacity and experience of local govern-
ments resulted in urban space to be developed through the private sector. So, urban
fringe faced partial developments. The holes in planning legislation and the popu-
larity of partial plans resulted in a urban sprawl in metropolitan areas.
The rapid growth in metropolitan areas resulted in infrastructure, environment,
and housing problems. In contrast, density increments and land use changes in
urban environment have been realized through plan modifications.
1 Urban Development Policy and Urban Sprawl in Turkey 9
Conclusion
In the twentieth century due to rapid growth, the structure of urban settlements has
changed dramatically. Metropolitan areas were mostly affected by increasing
population. Metropolitan growth will either concentrate within the city boundaries,
increasing the density, but most likely the city will expand on the periphery of the
city through decentralization. The detrimental consequences of urban sprawl can be
solved through planned decentralization. The diverse existing urban systems must
be coordinated with the new development areas in order to establish the integrity of
the macroform.
The new value systems, procedures and concepts brought to the era by global-
ization affected Turkey as well. Turkey is also similar to other developing countries
where metropolitan growth is due to fast population growth and results in urban
sprawl. The multiple plans were not effectively implemented due to lack of policies
because of speculative market forces and their heavy demands in Turkey.
Consequently, partial plans have resulted in uncontrolled development and
metropolitan growth was transformed into an oil-spill form in Turkey. Such devel-
opment increases infrastructure costs and burdens local authorities. Urban sprawl
creates problems, such as incongruity of functions, environmental problems, and
higher of public services cost, increased energy consumption. To overcome these
problems, the uncontrolled growth should be stopped and development policies that
address both public and private sectors should be addressed.
References
Balta, M. Ö., & Eke, F. (2011). Spatial reflection of urban planning in metropolitan areas and
urban rent: A case study of Cayyolu, Ankara. European Planning Studies (SSCI), 19(10), 1817–1838.
Balta, M. Ö., Tekel, A., & Tekel, İ. (2012). Urban development process of built environments in
metropolitan areas in Turkey: A case study of Angora Settlement, Ankara. Journal of Urban Planning and Development-ASCE (SCI), 138(1), 70–77.
Beauregard, R. A. (2006). When America became suburban. Minneapolis: University of Minne- sota Press.
Burchell, R., Shad, N. A., Listokin, D., Phillips, H., Downs, A., Seskin, S., Davis, J. S., Moore, T.,
Helton, D., & Gall, M. (1998). The costs of sprawl, revisited. Transportation research board (pp. 1–40). Washington, DC: National Research Council.
Cox, W., & Utt, J. (2004). The costs of sprawl reconsidered: What the data really show (pp. 1–18). Unpublished paper. The Heritage Foundation. Retrieved May 12, 2009, from http://www.
heritage.org/research/smartgrowth/.
EEA. 2006. Urban sprawl in Europe—The Ignored Challenge EEA Report No.: 10/2006.
Retrieved May 12, 2009, from http://reports.eea.europa.eu/eea_report_2006_10/en/eea_
report_10_2006.pdf.
Erkip, F. (2005). The rise of the shopping mall in Turkey: The use and appeal of a mall in Ankara.
Cities, 22(2), 89–108. Ewing, R.H. (1994). Characteristics, causes and effects of sprawl: A literature review.Environmental
and Urban Studies, 21, 1–15.
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Ewing, R. (1997). Is Los Angeles—Style sprawl desirable? Journal of the American Planning Association, 63(1), 2–4.
Ewing, R., Pendall, R., & Chen, D. (2002). Measuring sprawl and its impact (pp. 1–31). Washington, DC: Smart Growth America.
Gillette, H. (2005). Camden after the fall: Decline and renewal in a post-industrial city. Phila- delphia: University of Pennsylvania Press.
Glicksman, L. R. (2007). Editorial: The energy crisis—The need for more balanced solutions.
HVAC&R Research Journal, 13(4), 521–523. Ozuduru, B. H, & Varol, C. (2009). Global restructuring of the marketplace: Local and regional
impacts on the spatial distribution of retail activity in Turkey. In 23rd congress of the Association of European Schools of Planning (AESOP), Liverpool, İngiltere.
Snyder, K., & Bird, L. (1998). Paying the Costs of Sprawl: Using Fair-Share Costing to Control Sprawl. Washington, DC: U.S. Department of Energy.
Squires, G. D. (2002).Urban sprawl: Causes, consequences & policy responses. Washington, DC: The Urban Institute Press.
Teaford, J. C. (2006). The metropolitan revolution: The rise of post-urban America. New York: Columbia University Press.
Ünlü, T. (2005). Plan modifications within the contexts of planning control mechanisms Mersin case. Unpublished PhD thesis, School of Natural and Applied Sciences of Middle East Technical University, Ankara
1 Urban Development Policy and Urban Sprawl in Turkey 11
Chapter 2
Perspectives on the Implementation of Climate Change Public Policies in Brazil
Rommel de Santana Freire, Monica Carvalho,
Charles Ulises de Montreuil Carmona,
and Alexandre Magno Vieira Gonçalves de Brito
Introduction
As a developing country, Brazil plays an important role in the global scenario for
the reduction of greenhouse gas (GHG) emissions. Several public policies have
been created towards the reduction of pollution levels. Brazil’s participation in international agreements and the creation of a positive agenda for the development
of new regulations for environmental presentation direct the country to the con-
struction of a cleaner scenario.
Brazil participates in the Kyoto Protocol (largest international agreement signed
for the reduction of GHG emissions), but still does not count with established
mandatory reduction levels. However, the country already acts in a pro-active way
through the creation of several sectional plans for mitigation and adaptation
R. de Santana Freire (*) Department of Accountancy and Finances, Center of Applied Social Sciences, Federal
University of Paraı́ba (UFPB), Cidade Universitária, Jo~ao Pessoa, 58051-900 Paraı́ba, Brazil e-mail: [email protected]
M. Carvalho
Department of Renewable Energy Engineering, Center of Alternative and Renewable Energy,
Federal University of Paraı́ba (UFPB), Caixa Postal 5115, Cidade Universitária, Jo~ao Pessoa, 58051-900 Paraı́ba, Brazil
e-mail: [email protected]
C.U. de Montreuil Carmona
Department of Management Science, Center of Applied Social Sciences, Federal University of
Pernambuco (UFPE), Cidade Universitária, Recife, 50670-901 Pernambuco, Brazil
e-mail: [email protected]
A.M.V.G. de Brito
Department of Mechanical Engineering, Center of Technology, Federal University of Paraı́ba
(UFPB), Cidade Universitária, Jo~ao Pessoa, 58051-900 Paraı́ba, Brazil e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_2
13
(Brasil 2011). These plans contemplate strategic areas (forests, energy in agricul-
ture, urban mobility) and industry intensive sectors (metallurgy, mining, transfor-
mation). The focus is to reduce the levels of pollution and at the same time, improve
the performance and competitiveness of companies. The process of implementing
these regulations is slow, as several bureaucratic and cultural barriers still remain,
which hinders the obtainment of better results.
A positive point that helps the country to maintain acceptable levels of pollution
is the constitution of its energy matrix, which is mainly constituted of hydroelectric
plants and therefore presents lower levels of pollution. Incentives to energy gener-
ation utilizing renewable sources is still very limited. In a different direction, in
2013 in the European Union it was observed that the energy generation sector was
responsible for the largest share of CO2 emissions—70% of these companies were
located in Germany and England (Carbon Market Data 2014).
Despite the existence of policies directed to the strengthening of energy gener-
ation from renewable sources, implementation is still expensive and complex,
hindering its application for the majority of the population. Developing countries,
such as China and India, count with greater incentives for the installation of
residential equipment that better utilize renewable energy sources (World Bank
2014). Regarding the logic of reduction of emissions, the European Union created
the European Union Emission Trading Scheme (EU ETS), responsible for regulat-
ing the operation of the market for reduction of carbon emissions, establishing goals
for the reduction of pollution and distributing the allowance quotas for carbon
emissions (European Emission Allowances, EUA) among the members of the
European community (Freire 2014).
Currently, the European Union is the largest negotiator of EUAs in the world,
also gathering the largest number of companies that follow the determinations of
the Kyoto Protocol. Globally, this new active (EUA) has been widely negotiated
since the mid-2000s, mainly in stock markets that deal with energy-related con-
tracts, taking advantage of the already existent structure and know-how (Knox-
Hayes 2009). The EUA market has grown substantially in the recent years, and can
reach the position of being one of the largest commodity markets in the world in the
next decades (Pirrong 2011).
However, after the drop in value of EUA’s during the 2006 and 2007 crisis and re-establishment of carbon markets, similar methodologies to EU ETS have been
applied to several countries, such as Japan, Canada, New Zealand, Australia and
United Kingdom—the U.S.A. (especially the state of California) and China deserve
special mention (Perdan and Azapagic 2011).
The creation of these new markets shows the directions of public policies that
aim at finding a way to reduce levels of emission of pollutants as well as contrib-
uting to energy and operational efficiencies of companies, creating therefore a new
entrepreneurial culture that is directly related to the wellbeing of the society.
A companion paper on the promotion of sustainability by quantifying and reducing
the carbon footprint lays the foundation for environmental awareness in consumers
(Carvalho et al. 2015).
14 R. de Santana Freire et al.
On the basis of an agreement with the United Nations, Brazil established
voluntary actions for the mitigation of GHG, with the objective of reducing
between 36.1% and 38.9% until 2020, fostering national policies on climate
change. Among these actions, the development of a Brazilian Market for Reduction
of Emissions is stimulated. The possibility of creating a nation-wide carbon market,
with its own regulation and interconnection with other markets in the world, can
bring positive contributions from economic and environmental viewpoints. This
manuscript aims to deepen the discussion on the subject, highlighting the benefits
and opportunities than can be generated by the implementation of public policies, as
well as the creation of new supplementary regulations.
Public Policies
The oil crisis, in the beginning of the 1970s, led the Brazilian government to create
its first study group on alternative sources of energy, being the first step towards the
creation of public policies regarding energy efficiency. After crystallization of the
first research efforts on conservation of energy, the first national program on
conservation of energy was launched in 1985. In the early 1990s, the first programs
that aimed at rational production and use of energy were created, along with
programs for better use of oil and natural gas derivatives. These programs
represented a milestone for environmental and energy efficiency policies.
In the following decades, Brazil continued to create and improve its national
policies on climate change, involving different production sectors and governmen-
tal organs. The objective is to create synergy between the involved areas, and the
main expected result is the sustainable development of the country, balancing
economic growth with environmental preservation. The current economic moment
presents low growth, hindering therefore the implementation of environmental
regulations that entail excessive costs. Laws that stimulate investments in new
equipment, processes or green products, through tributary incentives or for the
generation of green revenues, are seen as possible solutions for the mitigation of
climate change.
Politic guidelines lead the path to be followed by companies and society in
general, in the form of incentives such as tax reductions for the companies that
reduce their emissions or apply resources to efficiency energy researches. The
creation of new mechanisms to this kind of development and GHG control,
especially in the most polluting sectors is fundamental to implement a new culture
of environmental preservation. In this new environment, the organizations will be
required to optimize its processes/products in order to mitigate the effects of
pollution generated.
The Brazilian National Policy of Climate Change (PNMC) was established in
2009, through the adoption of Law 12.187 (Lude~na and Netto 2011). PNMC pursues voluntary actions for the mitigation of GHG emissions, including reduction
in deforestation (Amazon and Cerrado), reduction in energy consumption (energy
2 Perspectives on the Implementation of Climate Change Public Policies in Brazil 15
efficiency, alternative energy sources, etc.), stabilization of the share of renewable
energy sources in the energy matrix, and increased use of biofuels, among others.
Brazil’s GHG emissions are calculated every 5 years, and Fig. 2.1 shows the reduction of emissions through the implementation of PNMC, a non-mandatory
policy. These data represent the first results after its implementation.
The Brazilian legislation aims equalize sustainable development with economic
growth, eradicating poverty and reducing social inequalities. This new
interconnected vision drives the country to build a wide platform of emission
reduction alternatives. The Brazilian law also encourages the development of a
national market of reduce emissions, which in practice is not yet operational,
however the main focus is economic and social development compatibility with
the protection of the climate system (Brasil 2009, 2010).
The changes in the carbon market could modify the pollution levels defined by
the legislation (Montgomery 1972), resulting in greater control of the most pollut-
ing activities. The restrictions imposed on companies that exceed the pollution
limits could be seen as barriers to competitiveness, which would affect those that
pollute more (Perdan and Azapagic 2011).
Several countries are adapting theirs energy and climate policies to impose a
new behavior to the companies, one that focuses on cost optimization and reduc-
tions of GHG emissions, representing a new era for sustainable development. This
represents a new view that economy growth is inextricable from environmental
preservation.
The conclusions of the European Council in 2011 (CO EUR 2 CONCL 1 2011)
highlight the direction taken by the European Union regarding much necessary
environmental policies, with emphasis on sustainable growth, energy efficiency and
the necessity of creating policies that are capable of providing more investments in
research, development and innovation (Freire 2014). These three pillars are united
to create a more modern, safe, sustainable and low carbon energy system (European
Council 2011). In 2014, the European Council ratified the relevance to improve the
0
500.000
1.000.000
1.500.000
2.000.000
2.500.000
3.000.000
1990 1995 2.000 2005 2010
Carbon Equivalent Emissions (1000 tonnes)
Carbon Equivalent Emissions (1.000 t)
Fig. 2.1 Overall carbon emissions for Brazil (Brasil 2015)
16 R. de Santana Freire et al.
economic growth through the use of energy efficiency and the improvement of
competitiveness, maintaining the targets of greenhouse gas emission reduction
(CO EUR 2 CONCL 1 2014). Using similar strategy, China has created its own
ETS in seven regions of the country. The system will be in adaptation stage until the
end of 2015, when the emission reduction plan will be in force for the entire country
(Zhang et al. 2014).
Under a regulated market, managers will be enforced to create a new vision of
company, using threats as opportunities in the carbon market, creating competitive
advantage aims to maximize the shareholders’ wealth on behalf of other stake- holders (society and government). Cleary the news ETS needs changes to adapt
local/regional issues, but implementation is the first step for developing countries
and shows the government provides good conditions for the carbon market start up.
Brazil could follow the same path of other countries, but first needs to implement
the existing legislation and adapt/create complementary rules to improve the
creation of its own ETS, to create a positive chain between companies-govern-
ment-society.
Perspectives and Opportunities for Mitigation
Until recently, environment and sustainable development were considered prob-
lems and risk factors: however nowadays, these “problems” are seen as opportuni-
ties, as possibilities for growth and efficiency improvement (Carvalho et al. 2015).
Building upon the work of Carvalho and Freire (2014), mitigation of climate
change involves serious reduction in emissions, which can be achieved through
the better utilization of natural resources (energy efficiency concept). Obviously, if
the same amount of product can be obtained with reduced consumption of
resources, lower production costs are also achieved, which is a win-win situation
for managers and entrepreneurs.
The rise of new technologies and its learning curve costs contributes to a
reduction of transaction costs of organizations (Williamson 1994, 1995), as well
to reductions of pollutants gases (Blyth et al. 2009). R&D investments in produc-
tion models more “clean” and efficient, linked with new environmental policies rise
as option to improve energy efficiency consumption in companies, specially to
pollution reduction (Gans 2012).
Important opportunity for mitigation of climate change in Brazil include defor-
estation (Lude~na and Netto 2011) and energy-related carbon emissions (Melo et al. 2013). These mitigation efforts are translated into challenges at federal,
state and municipal levels, for both public and private sectors in Brazil.
The reduction of GHG emissions from deforestation and forest degradation is
now an important strategy for mitigating climate change, particularly in developing
countries with large forests, such as Brazil (Arima et al. 2014). National forest
policies designed to slow deforestation on public lands in developing countries
have had mixed success. However, there have been successful experiences (IPCC
2 Perspectives on the Implementation of Climate Change Public Policies in Brazil 17
2007): due to severe environmental and public health consequences, China, the
Philippines and Thailand have considerably reduced deforestation rates; in India,
there has been effective partnering with communities to reduce forest degradation.
The implementation of effective public policies needs backup from government
institutions and the general public. Considering the Brazilian scenario of limited
budgets, divergent interests and legal obligations, decision makers in Brazil face
multiple difficulties in the process of searching for adequate and reliable solutions
for the mitigation of GHG emissions (Melo et al. 2013).
In Brazil, buildings were responsible for 48% of the total electricity consumed
in the country in 2010 (Brasil 2011); this important share of electricity consumption
could obviously benefit from energy efficiency and conservation strategies aimed at
the reduction of energy-related GHG emissions. It is expected that the demand for
electricity will increase in Brazil in the next years–there is little wiggle room for
hydroelectric power plants to produce more, and therefore thermoelectric power
plants based on coal and natural gas will have to increase their contributions to the
energy mix. This will lead to higher environmental loads associated with the
consumption of electricity, and more overall environmental loads being disposed
of into the atmosphere—this figure will definitively be higher than what was
predicted in the Brazilian Energy Plan 2030 (Melo et al. 2013). Therefore any
decrease in environmental loads will be the result of dissemination efforts of energy
efficiency technologies, most probably through public policy mechanisms.
According to Lucon et al. (2014), energy efficiency technologies have been
developed at the same time as existing energy efficiency opportunities have been
taken up, and therefore the potential for cost-effective energy efficiency improve-
ment is increasing. However, there are barriers to the market uptake of these
opportunities, and large potentials will remain untapped without appropriate poli-
cies (Lucon et al. 2014): in addition to technologies and architecture, behavior,
lifestyle, and culture have a major effect on energy use.
A very promising energy efficiency scenario is linked to the establishment of
public policies that highlight well-defined priorities, goals and action plans. A
sensitive point involves the education for the development of a collective con-
science towards the preservation of the environment. The responsible agencies
should widen the education, research and development actions for new technolo-
gies and establish partnerships with the private and public sectors. Changes in
energy consumers’ behavior and practices can lead to considerable reductions in energy demands, which present positives effects on climate-change issues (e.g.,
reduction of carbon emissions). Conscious energy behavior can be achieved
through educational interventions, and by combining interventions with incentives,
substantial reductions in energy use can be produced (Kirby et al. 2015).
There is growing acknowledgement on the importance of changing the energy-
related behavior of people. Multiple research efforts have been directed to the
subject of pro-environmental behavior change (of which energy-related behavior
is a component) (Energy Saving Trust 2007). If more consumers agree to a shift
towards a more energy-savvy behavior, important reductions in environmental
loads will be achieved. Energy-education could help change current and future
18 R. de Santana Freire et al.
common routines to save energy, and also encourage consumers to promote similar
behavior. One of the main incentives that propel energy users to adopt energy-
savvy behaviors and practices is the reduction in consumption, accompanied by the
reduction in costs.
Final Remarks
The main conclusion of La Rovere et al. (2014) is that Brazil is in a good position to
meet its mitigation goals until 2020. However, after 2020, Brazil will be challenged
to combine economic development with low carbon energy-related emissions.
The creation of a system for trading GHG emissions in Brazil would encourage
Brazilian companies to reduce their emissions and trade these in a regulated market,
achieving double benefits: reduction of emissions (less consumption of resources,
lower costs) and benefits realized through the trade of emissions. This model is
similar to the model established by the Kyoto Protocol and reproduced internally in
many countries.
New environmental policies combined with financial incentives lead company
managers to promote the reduction of GHG emissions through innovation/adapta-
tion of processes and products. This action would foster economic development that
focuses on environmental preservation, promoting the development of a new
culture, where people would vigorously demand the implementation of green
policies by companies. Brazil has the potential to maintain sustainable economic
growth through the implementation of existing policies and the creation of new
mechanisms, permitting the creation of an internal carbon market, which can also
be connected to other markets already consolidated in the world.
Acknowledgments The authors wish to acknowledge the support of the Institute for the Devel- opment of Paraı́ba (IDEP-UFPB) and of the National Council for Scientific and Technological
Development (CNPq), through project n� 475879/2013-9.
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Chapter 3
30 Years Air Temperature Data Analysis in Athens and Thessaloniki, Greece
T. Slini and K.T. Papakostas
Introduction
The topic of climate change has attracted widespread attention in recent years and is
an issue that numerous scientists study on various time and space scales. The
reasons for climate change are complex and generate extensive discussion and
dispute in the scientific community. The main cause is the greenhouse gas emis-
sions produced by anthropogenic activities, e.g. industry, agriculture, transport. In
all these human activities, energy comes mainly from non-renewable sources
(liquid, gas and solid fuels) producing emissions that trigger the global warming.
It is widely accepted that increasing concentrations of greenhouse gases in the
atmosphere is the dominant driver of global warming and climate change. Climate
change and its impact are met with various ways: increasing temperature, changing
the distribution of rainfall floods, desertification and reduction of water resources,
forest fires, shrinking glaciers, rising sea levels.
Over the past 100 years the increase in global average temperature was about
0.74 �C and 11 out of the 12 years in the period 1995–2006 are listed among the top warmest years with reference to the historic beginning of recorded measurements
by scientific instruments, i.e. 1880 (IPCC 2007). Moreover, according to recent data
(NOAA 2014), on a global scale, the decade 2001–2010 was the warmest ever
recorded. Consequently, global warming is projected to persist, if greenhouse gases
T. Slini (*) Department of Mechanical Engineering, Laboratory of Heat Transfer and Environmental
Engineering, Aristotle University of Thessaloniki, Box 483, 54124 Thessaloniki, Greece
e-mail: [email protected]
K.T. Papakostas
Department of Mechanical Engineering, Laboratory of Process Equipment Design, Aristotle
University of Thessaloniki, 54124 Thessaloniki, Greece
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_3
21
will continue to be emitted at the same rate. It is estimated that surface air warming
in the twenty-first century for a “low emission scenario” will be 1.8 �C, with a likely range of 1.1–2.9 �C, while in a “high emissions scenario”, it will be an increase of 4.0 �C with a likely range from 2.4 to 6.4 �C. A temperature increase of 0.1 �C per decade would be expected for the next two decades, even if concentrations of
greenhouse gases and aerosols were kept at the levels of the year 2000 (IPCC
2013). In particular, the average global temperature increased after 1978 with an
average rate of 0.14 �C per decade, while the average global temperature over land and sea surface reached the record highest temperature (14.47 �C) in April 2010, which is an increase of 0.77 �C as compared to the average of the twentieth century (13.7 �C). This event was characterised as one of the greatest climate anomalies at global scale based on NOAA data (URL 1). According to the same data, the global
average temperature in April 2014 over land was 9.45 �C that is 1.35 �C above the average of the twentieth century (8.1 �C), while the average global temperature of April 2014 in the sea was 16.55 �C that is 0.55 �C above the average of the twentieth century (16 �C).
Regarding Greece, according to a report conducted by the Climate Change
Impacts Study Committee (Climate Change Impacts Study Committee 2011) and
the National Observatory of Athens (WWF 2009), urban centres (e.g., Thessaloniki,
Patras, Larissa and Lamia) are expected to face annually a rise at the number of
days with maximum temperature above 35 �C, and at the number of “hot” nights, during which the temperature is maintained above 20 �C, with the period 1961–1990 as a reference.
In addition, in recent decades the frequency of occurrence of lower temperature
decreases while the frequency of occurrence of higher temperature increases
(Papakostas et al. 2013, 2014) and at the same time, the urban heat island effect
(Urban Heat Island) is observed in several Greek cities (Santamouris et al. 2001;
Kolokotsa et al. 2009; Giannaros and Melas 2012; Vardoulakis et al. 2013;
Giannopoulou et al. 2011; Livada et al. 2002). The effects of climate change are
of particular interest, as even a slight temperature change is reflected directly in
socio-economic sectors such as tourism, agriculture, mining industry, transport,
built environment, quality of life and health (Giannakopoulos et al. 2011) as well as
in energy consumption in buildings (Papakostas et al. 2010, 2013, 2014;
Santamouris et al. 2001).
According to the World Meteorological Organization (WMO) the current offi-
cial baseline for meteorological models is the 30-year time period from 1961 to
1990. At the same time this reference time period is under review for the “adjusted”
evaluation of the latest meteorological data (URL 2). The new proposed baseline is
the period 1981–2010, which is already used by several meteorological organiza-
tions so as to provide more updated and reliable services for both citizens and policy
makers regarding issues such as energy and peak load, civil protection planning and
strategic recommendations.
Based on the above, the purpose of this work is to analyze the ambient air
temperature in Athens and Thessaloniki for 30 years, namely the period 1983–2012,
in order to identify the statistically significant changes and evaluate the current
trends in urban sites in Greece.
22 T. Slini and K.T. Papakostas
Methodology
The hourly time series of outdoor air temperature of three decades (1983–2012) for
the cities of Athens and Thessaloniki are thoroughly analysed in the frame of the
current study. The measurement data are obtained from the meteorological station
of the National Observatory of Athens (NOA) (NOA Climatological Bulletin)
located on a small hill near the Acropolis (with coordinates 37�580N, 23�430E and altitude 107 m), and respectively from the station maintained by the Institute of
Meteorology and Climatology of the Aristotle University of Thessaloniki
(IMC/AUTh) (Department of Meteorology and Climatology) within the university
campus (with coordinates 40�370N, 22�570E and altitude 31 m). The measurements were checked for homogeneity (Founda et al. 2009) and the missing values were
negligible and did not affect the reliability and quality of results. Specifically, for
the Athens area recorded about 1077 out of 263,424 observations (percentage of
0.4%) and Thessaloniki about 567 in total of 263,520 (percentage of 0.2%).
For the need of the study descriptive statistics indicators were estimated such as
the mean, the standard deviation, the frequency, and quartiles in hourly, daily,
monthly, annual and decadal scale. Graphic representation of the data was
performed in order to detect and capture any evident trend, seasonality or outlier.
The average for the period 1961–1990 was employed as a benchmark for the
identification of outliers and deviations from the “normal” values. Furthermore,
according to the Intergovernmental Panel on Climate Change (IPCC), the change in
indicators is mainly expressed as deviations from the average or normal mode. The
current study adopted the indicators used in the reports of IPCC (IPCC 2007) and
the Joint Research Center (2008). In this view, the number of days with daily
average of more than 25 �C and daily maximum temperature above 35 �C were estimated.
Finally statistical tests were carried out in order to identify any statistically
significant changes in temperature at a significance level of 0.05.
Results
The main results of the analysis are presented in the following graphs exhibiting the
average minimum, mean and average maximum monthly values of temperature
(�C), the number of days with daily average temperature above 25 �C, the number of days with a maximum value greater than or equal to 35 �C, and the cumulative frequency curves of temperature per decade for the two areas under study. It is
noteworthy to point out the intense temperature variations between the decades
1983–1992 and 2003–2012 in all graphs especially during the summer months.
More specifically, there is a gradual increase in average minimum, mean and
maximum average monthly values of temperature from decade to decade (Fig. 3.1).
Note that in Athens, the differentiation between the temperature per decade is
3 30 Years Air Temperature Data Analysis in Athens and Thessaloniki, Greece 23
statistically significant both in annual scale and individually throughout the summer
months, based on the non-parametric Kruskal-Wallis (p< 0.05) test, indicating that this variation is not due to a random effect. Respectively the results for Thessaloniki
prove that there is a statistically significant difference to both the minimum and
Fig. 3.1 Average minimum, mean, and average maximum monthly temperatures per decade, in Athens (a, c, e) and Thessaloniki (b, d, f): period 1983–2012
24 T. Slini and K.T. Papakostas
maximum values. In particular regarding the variation between the first decade,
1983–1992, and the third decade, 2003–2012, the average minimum monthly
temperatures in Athens ranged from 0.1 �C (month of January) to 2.94 �C (month of September), the average monthly temperatures range from 0.04 �C (month of January) to 2.25 �C (month of August), while the average maximum temperatures range from 0.15 �C (month of February) to 2.26 �C (month of August). In Thessaloniki, the change in mean minimum monthly temperatures range from
0.24 �C (month of April) to 1.90 �C (month of August), the average monthly temperatures range from 0.13 �C (month of April) to 1.66 �C (month of August), while the average maximum temperatures ranging from 0.16 �C (month of January) to 2.02 �C (month of August). Moreover, it was observed that the major increase occurred in Athens from the first (1983–1992) to the second decade (1993–2002),
while the differentiation of temperatures was much lower from the second to the
third decade. Instead, in Thessaloniki greater changes observed between the second
and third decade, with the exception of mean minimum temperatures in August,
September and October.
Regarding the number of days with daily average temperature above 25 �C, as depicted in the diagrams of Fig. 3.2, a rising trend is exhibited in the number of days
for both areas. In detail, there were 717 days in the first decade, 906 in the second
and 934 in the third decade in Athens (at least in the measuring range). That is the
increase of days with average daily temperature above 25 �C from the first to the third decade was about 30% and from the first to the second about 26%. Similarly,
in Thessaloniki area (at least in the measurement range), there were 494 days during
the first decade, 596 during the second and 748 days in the third decade wherein the
increasing tendency was about 51% from the first to third and 25% from the first to
second decade respectively (Table 3.1).
Higher temperatures increase the amount of moisture that evaporates from land
and water, leading to drought in many areas. Generally, lands and cities are affected
by drought since they become more vulnerable to flooding once rain falls.
Fig. 3.2 Number of days with daily average temperature above 25 �C per decade (a) in Athens and (b) in Thessaloniki: period 1983–2012
3 30 Years Air Temperature Data Analysis in Athens and Thessaloniki, Greece 25
Temperature changes may as well increase the spread of infectious diseases, mainly
because warmer temperatures allow disease-carrying insects. On the other hand
temperature rise favours the touristic attractiveness during spring and autumn,
especially in areas where tourism is an important economic sector.
Regarding the number of the days with a maximum temperature value equal or
exceeding the limit of 35 �C, the analysis of data is presented in the graphs of Fig. 3.3 and the conclusions are similar. In the Athens area, the number of days with
maximum temperature above or equal to 35 �C was estimated at 79, 217 and 287 respectively for each decade (up 175% in the second decade and 263% in
the third, relative to the first), while in Thessaloniki on 56, 70 and 141 (an increase
of 25% in the second decade and 152% in the third, as compared to the first). The
most days with this characteristic were monitored during the third decade
(2003–2012) as presented in Table 3.2, while their distribution is varying signifi-
cantly within the three decades only in the Athens area (non-parametric Kruskal-
Wallis test).
Table 3.1 Number of days with average daily temperature above 25 �C in Athens and Thessaloniki: period 1983–2012
Athens May June July August September October Total
1983–1992 9 126 259 248 71 4 717
1993–2002 24 205 286 279 107 5 906
2003–2012 28 181 300 307 115 3 934
Total 61 512 845 834 293 12 2557
Thessaloniki May June July August September October Total
1983–1992 1 75 211 186 21 0 494
1993–2002 10 107 238 217 24 0 596
2003–2012 11 138 275 273 49 2 748
Total 22 320 724 676 94 2 1838
Fig. 3.3 Number of days with maximum temperature equal or greater than 35 �C per decade (a) in Athens and (b) in Thessaloniki: period 1983–2012
26 T. Slini and K.T. Papakostas
Extreme high temperatures perhaps are the most direct effect of climate change
on humans. High air temperatures in combination with high humidity on a given
day increase the death danger to people with heart and respiratory problems. Higher
air temperature also increases the concentration of ozone at ground level. In the
lower atmosphere, ozone is a harmful pollutant. It damages lung tissues and causes
problems for people with asthma and other lung diseases. Climate change would
increase cardio-respiratory morbidity and mortality associated with ground-level
ozone. Length, frequency and intensity of high temperatures affects also social life,
limits the exposure to open spaces, causes problems to transportation and creates
less favorable conditions for tourism in summer. Hot temperatures and dry condi-
tions also increase the likelihood of forest fires, especially in the conifer forests.
Furthermore based on the cumulative frequency temperature curves in Athens
(Fig. 3.4a) and Thessaloniki (Fig. 3.4b), it is also evident that the frequency of
occurrence of low temperatures decreases, while the frequency of occurrence of
high temperatures increases from decade to decade. This has a positive effect on the
coefficient of performance of heat pumps (with air as the heating source) in winter,
while it has a negative effect on the performance of heat pumps and air-cooled
chillers during the summer. Particular analysis is required in order to investigate
these deviations in efficiency rates (instantaneous and annual) both in winter and in
summer periods. The decrease of low temperatures frequency helps additionally to
reduce the demand of buildings for heating while the rise of high temperature
frequency increase energy demands for cooling, which may further exacerbate
peaks in electricity supply in the summer period. The net local impact of these
two effects depends on the current climate in a particular area. From the temper-
ature frequency curves in Fig. 3.4 it is concluded again that the strongest temper-
ature alterations in Athens are monitored from the first to the second decade while
in Thessaloniki a smoother change from decade to decade was observed.
Table 3.3 shows the number of weeks per decade, in which days with a
maximum temperature value equal or exceeding the limit of 35 �C are observed. The graphs in Fig. 3.5a and b display these weeks during the three decades as well
as the number of days per week, in which the temperature is equal to or greater than
Table 3.2 Number of days with maximum hourly temperature equal or above 35 �C in Athens and Thessaloniki: period 1983–2012
Athens May June July August September October Total
1983–1992 0 3 48 23 4 1 79
1993–2002 3 32 97 77 7 1 217
2003–2012 2 40 125 111 9 0 287
Total 5 75 270 211 20 2 583
Thessaloniki May June July August September October Total
1983–1992 0 5 31 16 4 0 56
1993–2002 0 9 34 25 2 0 70
2003–2012 0 26 50 60 5 0 141
Total 0 40 115 101 11 0 267
3 30 Years Air Temperature Data Analysis in Athens and Thessaloniki, Greece 27
Fig. 3.4 Cumulative frequency curves of the temperature (a) in Athens and (b) in Thessaloniki for the decades 1983–1992, 1993–2002 and 2003–2012
Table 3.3 Number of weeks with daily maximum
temperature equal or above
35 �C in Athens and Thessaloniki for the period
1983–2012
Athens Thessaloniki
1983–1992 79 56
1993–2002 217 70
2003–2012 287 141
Total 583 267
Fig. 3.5 Number of days per week in which the maximum temperature is equal to or exceeds the limit of 35 �C (a) in Athens and (b) in Thessaloniki for the period 1983–2012
3 30 Years Air Temperature Data Analysis in Athens and Thessaloniki, Greece 29
this limit. Obviously, both the number of weeks and the number of days per week
with high temperatures above 35 �C are increasing from decade to decade. The frequency of these events increased in Athens more from the first to the second
decade, while in Thessaloniki mainly from the second to the third decade. The
number of hours with temperature values equal or exceeding the limit of 35 �C are shown in Tables 3.4 and 3.5 and for Athens and Thessaloniki respectively.
Figure 3.6 illustrates the temperature fluctuations on a daily scale, in both cities,
for a winter and a summer month during the three recent decades. The months of
December and July are selected and the average hourly temperature curves are
shown in Fig. 3.6a and b for Athens and in Fig. 3.6c and d for Thessaloniki. It is
apparent that temperature is increasing from decade to decade, with the greater
differences to be observed at lower temperatures of the year, recorded in December.
More specifically in Athens, from the decade 1983–1992 to the decade 2003–2012
the rise monitored in average hourly temperatures ranged from 1.3 �C (16:00) to 1.9 �C (24.00) in December and from 1.6 �C (18:00) to 2.3 �C (11.00) in July. Respectively in Thessaloniki, the rise in the average hourly temperatures ranged
from 1.4 �C (23:00) to 2.0 �C (8:00) in December and from 1.1 �C (at 9:00) to 1.8 �C (17:00) in July. The significant differences in the hour of appearance of maximum temperatures in the two areas are probably due to the urban heat island
effect and the sea breeze, since the monitoring stations are located in different built-
up urban environment. The NOA station is located in a more densely built-up area,
5 m from the sea, while the IMC/AUTh station is in a green area only 1 km from the
sea.
Of particular interest is the fact that the results, the correlations and the varia-
tions of the temperature distribution in the three decades reflected in the graphs are
confirmed by the non-parametric Kruskal-Wallis test, with the only exception of the
number of days with maximum temperature above 35 �C in Thessaloniki area (Table 3.6).
Table 3.4 Number of hours per month, which the temperature is equal to or exceeds the limit of 35 �C. Athens: period 1983–2012
Athens May June July August September October Total
1983–1992 0 9 217 66 15 1 308
1993–2002 5 122 507 362 16 1 1013
2003–2012 5 203 634 529 25 0 1396
Total 10 334 1358 957 56 2 2717
Table 3.5 Number of hours per month, which the temperature is equal to or exceeds the limit of 35 �C. Thessaloniki: period 1983–2012
Thessaloniki May June July August September October Total
1983–1992 0 6 137 61 16 0 220
1993–2002 0 37 139 108 2 0 286
2003–2012 0 105 244 231 10 0 590
Total 0 148 520 400 28 0 1096
30 T. Slini and K.T. Papakostas
Fig. 3.6 Average hourly temperature for December and July for the period 1983–2012 per decade (a, b) in Athens and (c, d) in Thessaloniki respectively
Table 3.6 Results of the Kruskal–Wallis test for the distribution of the studied parameters over the three decades
Athens Thessaloniki
Minimum temperatures ** **
Maximum temperatures ** **
Number of days with daily temperature above 25oC ** **
Number of days with maximum temperature equal or above 35oC ** –
Mean daily temperature of December ** **
Mean daily temperature of July ** **
Statistically significant differences marked with **, at significance level of 0.05
3 30 Years Air Temperature Data Analysis in Athens and Thessaloniki, Greece 31
Conclusions
Climate change is happening and influences life in cities. Current observations as
well as projected changes suggest an increase of the annual mean temperature, a
change of precipitation patterns, a rise of sea level, an increase of the number,
intensity and duration of heatwaves, as well as an increase of extreme precipitation
events and drought. Cities and towns will be affected by the impacts of climate
change. The impacts are direct, such as health problems, damages to infrastructure,
lower crop productivity, fire risks, decrease in water availability, and indirect such
as lower productivity in work, reduction in the use of public spaces, social life
restriction, affection to tourism industry, effects on energy consumption and risks in
energy supplies. All these impacts are extremely important, their analysis is com-
plex and requires different data. In this work, an analysis of the dry-bulb temper-
ature of the ambient air in Athens and Thessaloniki for the 30 years period
1983–2012, based on hourly measurements of meteorological stations of the
National Observatory of Athens and the Aristotle University of Thessaloniki, was
performed. The results show a strong and statistically significant upward trend of
the temperature values in both cities. More specifically, there is a gradual increase
in average minimum, mean and maximum monthly values of air temperature from
decade to decade. The differentiation between the temperatures through the decades
was demonstrated as statistically significant, based on the non-parametric Kruskal-
Wallis test (p< 0.05), suggesting the non-randomness of this variation. The cumu- lative frequency curves of temperature show that the occurrence of low tempera-
tures decreases, whereas the frequency of the high temperatures is increased
through the examined period. Specifically an upward trend is shown in the number
of days with daily mean temperature above 25 �C and the number of days with maximum value equal to or exceeding 35 �C, for both areas, and suggest a slight shift of the warmest days from July to August. In addition, both the number of
weeks and the number of days per week with high temperatures above 35 �C are increasing from decade to decade. Finally, the daily fluctuation in temperature
reveals a distinct temperature rise from decade to decade, throughout the day,
while at the same time the increase was recorded particularly in low temperatures
in winter and in high temperatures in summer. The data that this work presents, may
be helpful to support policy development and decision making in urban and built
environment design.
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3 30 Years Air Temperature Data Analysis in Athens and Thessaloniki, Greece 33
Chapter 4
Mitigation and Adaptation Policies Related to Climate Change in Greece
I. Sebos, A. Progiou, L. Kallinikos, P. Eleni, I. Katsavou, K. Mangouta,
and I. Ziomas
Introduction
In response to the emerging evidence that climate change could have a major global
impact, the United Nations Framework Convention on Climate Change (henceforth
the Convention) was adopted on 9May 1992 and was opened for signature in Rio de
Janeiro in June 1992. Greece signed the Convention in Rio and ratified it in 1994
(Law 2205/94) (Ministry of Environment Energy and Climate Change (MEECC)
2014a).
In that framework, the third meeting of the Conference of the Parties (COP) to
the Convention, held in Kyoto (1–11 December 1997), finalised the negotiations
related to the establishment of a legal instrument; the Kyoto Protocol on Climate
Change. The Kyoto Protocol runs in two commitment periods; the first one started
in 2008 and ended in 2012 (United Nations Framework Convention on Climate
Change (UNFCCC) 1998), whereas the second started in 2013 and will end in 2020
(European Environment Agency (EEA) 2014). The Protocol provides a foundation
upon which future action can be intensified and introduced, for the first time, legally
binding commitments for developed countries to reduce emissions of greenhouse
gases. The Protocol entered into force on 16 February 2005, after its ratification
from 141 Parties (with the exception of USA and Australia—Australia finally
ratified the 1997 Kyoto protocol in 2007) including developed countries with a
contribution of more than 55% to global CO2 emissions in 1990. The detailed rules
for the implementation of the Protocol were adopted at COP 7 in Marrakesh,
Morocco, in 2001, and are referred to as the “Marrakesh Accords.” In Doha,
I. Sebos (*) • A. Progiou • L. Kallinikos • P. Eleni • I. Katsavou • K. Mangouta • I. Ziomas Department of Chemical Engineering, National Technical University of Athens,
Zografou Campus, 9 Heroon Polytechniou Street, 15780 Zografou, Greece
e-mail: [email protected]; [email protected]; [email protected]; peleni@central.
ntua.gr; [email protected]; [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_4
35
Qatar, on 8 December 2012, the “Doha Amendment to the Kyoto Protocol” was
adopted (United Nations Framework Convention on Climate Change (UNFCCC)
1998; United Nations Framework Convention on Climate Change (UNFCCC)
2015), and sets new commitments for Annex I Parties to the Kyoto Protocol who
agreed to take on commitments in a second commitment period from 1 January
2013 to 31 December 2020.
With respect to the EU target under the first commitment period of the Kyoto
Protocol (i.e. reduction of emissions at 8% for the period 2008–2012 comparing to
1990 levels), EU has stated that this will be achieved jointly by EU Member-States
under the provisions of Article 4 of the Protocol. The Burden-Sharing agreement
between all Member States was finalized during the Environment Council in June
1998 and entered into force with Decision 2002/358/EC concerning the approval,
on behalf of the European Community, of the Kyoto Protocol. According to this
agreement, Greece is committed to limit its GHG emissions increase for the period
2008–2012 to þ25% compared to base year emissions (1990 for CO2, CH4 and N2O emissions—1995 for F-gases). Since the base year emissions of Greece were
106,987,169 t CO2 eq. (United Nations Framework Convention on Climate Change
(UNFCCC) 2007), the assigned amount was calculated to be 668,669,806 t CO2 eq. (5 * 1.25 * base year emissions). Greece ratified the Kyoto Protocol in 2002
(Law 3017/2002) and adopted a National Programme for achieving its commitment
by a decision of the Council of Ministers (DCM5/2003).
Concerning the second period of the Kyoto Protocol, legally binding target
trajectories for the period 2013–2020 are enshrined in both the Emissions Trading
System (EU-ETS) Directive (Directive 2003/87/EC and respective amendments)
and the Effort Sharing Decision (Decision No 406/2009/EC). At the same time the
European Union (EU) has set its climate change mitigation objective for 2020,
committing itself to reducing its emissions by at least 20% compared to 1990 levels
(30% subject to the conclusion of a comprehensive international climate change
agreement) (Official Journal of the European Union 2013) in the context of the EU
Climate and Energy Package, which adopted in 2009. These legally binding
trajectories not only result in a 20% GHG reduction in 2020 compared to 1990
but also define the EU’s annual target pathway to reduce EU GHG emissions from 2013 to 2020. The EU has also committed to increase to 20% the share of
renewable energies in the EU final energy consumption (with a minimum 10%
share in the transport sector) and to save 20% of the EU’s energy consumption through increased energy efficiency (“20-20-20” objective) (European Environ-
ment Agency (EEA) 2014; European Commission/DG Climate Action/ European
Environment Agency 2014).
The EU ETS is the key tool for cutting industrial greenhouse gas emissions most
cost-effectively. The climate and energy package includes a comprehensive revi-
sion and strengthening of the legislation which underpins the EU ETS, the Emis-
sions Trading Directive. The revision applies from 2013, the start of the third
trading period of the EU ETS. Major changes include the introduction of a single
36 I. Sebos et al.
EU-wide cap on emission allowances in place of the existing system of national
caps. Thus, the emission reduction to be achieved from the sectors covered by the
EU ETS will be 21% below 2005 emission levels. In specific, the allowed GHG
emissions will start by the mean value of the period 2008–2010 for industries that
are included in the ETS and will be decreased by 1.74% annually until 2020.
The effort to reduce emissions not covered by the EU-ETS, shared between
the EU-28 Member States through differentiated annual national GHG targets
under the Effort Sharing Decision (ESD). The Effort Sharing Decision sets
annual national emission targets for all Member States for the period 2013–2020
for those sectors not covered by the EU-ETS, expressed as percentage changes
from 2005 levels. In March 2013, the Commission formally adopted the national
annual limits throughout the period for each Member State. By 2020, the
national targets will collectively deliver a reduction of around 10% in total
EU emissions from the sectors covered compared with 2005 levels. The national
target of Greece for emissions not included in the ETS (non-ETS) is a 4%
reduction of emissions by 2020 compared to 2005. According to European
Commission Decision 2013/162/EU, 4% reduction of emissions by 2020 for
Greece is account for 63,028,265 t CO2 eq., based on the global warming
potential values from the fourth IPCC assessment report (European Environment
Agency (EEA) 2014).
National Greenhouse Gas Emissions
Figure 4.1 presents the emissions of greenhouse gases (carbon dioxide, methane,
nitrous oxide, HFCs, PFCs), for the years 1990–2012, expressed in carbon dioxide
equivalent (Mt CO2 eq.), while the Land Use, Land Use Change and Forestry
(LULUCF) sector is not included (Ministry of Environment Energy and Climate
Change (MEECC) 2013).
It should be noted that because the sector Land Use, Land Use Change and
Forestry (LULUCF), was a sink of greenhouse gases in 1990 (as in the whole period
from 1990 to 2012), emissions from this sector are not taken into account for the
calculation of emissions base.
Total emissions of greenhouse gases (without LULUCF) in 2012 amounted to
110.98 Mt CO2 eq., showing an increase of 5.77% compared to base year over
emissions. Since the objective of the country for the first commitment period of the
Kyoto Protocol is to limit the increase of GHG emissions at þ25%, it is obvious that the country not only achieves its goal, but also has surplus of emission
allowances (Fig. 4.2).
The contribution of each sector in total emissions is shown in Fig. 4.3. As it is
evident from this figure, emissions from the energy sector (emissions from
4 Mitigation and Adaptation Policies Related to Climate Change in Greece 37
combustion of fossil fuels and fugitive emissions) accounted for 78.61% of the total
emissions for the year 2012.
The key findings are summarized below:
2. Industrial Processes
8.66%
1. Energy 78.61%
3. Solvent and Other Product
Use 0.29%
4. Agriculture 8.18%
5. Waste 4.27%
Fig. 4.2 Contribution of each sector to total GHG emissions for 2012
160
140
140
130
120
110
100
90
80
120
100
80
Mt CO2eq
60
40
20
Total emissions Change to 1990
0
19 90
19 91
19 92
19 93
19 94
19 95
19 96
19 97
19 98
19 99
20 00
20 01
20 02
20 03
20 04
20 05
20 06
20 07
20 08
20 09
20 10
20 11
20 12
Fig. 4.1 Total GHG emissions time series in Greece in Mt CO2 eq
38 I. Sebos et al.
Emissions from Energy in 2012 accounted for 78.61% of total GHG emissions
(without LULUCF) and increased by approximately 13.73% compared to 1990
levels.
The living standards improvement, due to the economic growth, the important
growth of the services sector and the introduction of natural gas in the Greek energy
system represent the basic factors affecting emissions trends from Energy for the
period 1990–2007. The decreasing trend of emissions in all sectors of energy of the
years 2008–2012 is attributed among others (i.e. RES, energy efficiency measures,
road infrastructure and public transportation improvements, etc.) to the economic
recession that the country is facing.
At the same time it should be mentioned that the availability of hydropower has a
significant effect to emissions trends. For instance, the significant increase of
electricity demand in 1999 was not followed by a similar increase of emissions
because of the penetration of natural gas and the high availability of hydropower.
The majority of GHG emissions (64.12%) in 2012 derived from energy indus-
tries, while the contribution of transport, manufacturing industries and construction
and other sectors is estimated at 18.63%, 6.47% and 10.78%, respectively. The
rest 0.01% of total GHG emissions from Energy derived from fugitive emissions
from fuels. Within the fuel combustion activities, the sector with the greatest
increase of emissions for the years 1990–2008 is transport, showing an average
rate of increase of 2.48%. However, for years 2009–2012 a decrease was observed
with an average rate of decrease equal to �6.81%. In addition, energy industries and other sectors (i.e. residential, tertiary and agriculture sectors) presented 1.16%
and 0.94% average annual rate of increase, respectively. Finally, missions from
Fig. 4.3 GHG emissions between 1990 and 2012 by sector
4 Mitigation and Adaptation Policies Related to Climate Change in Greece 39
manufacturing industries and construction emissions had a mean annual rate of
decrease of 1.87%.
Emissions from Industrial Processes in 2012 accounted for 8.66% of the total
emissions (excluding LULUCF) and decreased by 9.42% compared to 1990 levels.
In 2012 mineral products production has continued the decreasing trend of the
previous years, following the decrease of all the subcategories of the sector, mainly
due to the effects of the economic recession. There is an increase in emissions since
2011 (20.07%), which followed the intense decrease of 2011 (�36.74% between 2011 and 2010). Emissions from chemical industry have decreased by 23.67%
since 2011. Emissions from metal production slightly increased with regards to
2011 by 1.05%, due to the increased production of aluminum and nickel. As
regards to fluorinated greenhouse gases (f-gases) emissions, have been increased
compared to 2011 (14.48%). The general increasing trend during the last years of
the time-series depicts the continuous substitution of CFCs in the context of the
protocol of Montreal.
The contribution of the Solvents and other products use sector to total GHG
emissions is minor (0.29% of the total emissions) and has increased by 3.29%
compared to 1990 level of emissions.
Emissions from Agriculture that accounted for 8.18% of total emissions in 2012
(without LULUCF), decreased by approximately 20.44% compared to 1990 levels.
Emissions reduction is mainly due to the reduction of Ν2Ο emissions from agri- cultural soils, because of the reduction in the use of synthetic nitrogen fertilizers.
The decrease in the use of synthetic nitrogen fertilizers is attributed to the increase
of organic farming, the high price of fertilizers and the impact of initiatives to
promote good practice in fertilizer use. The changes of the rest determining
parameters of GHG emissions from the sector (e.g. animal population, crops
production etc.) have a minor effect on GHG emissions trend.
Emissions from the Waste Sector (4.27% of the total emissions, without
LULUCF), decreased by approximately 19.58% from 1990. Living standards
improvement resulted in an increase of the generated waste and thus of emissions.
However, the increase of recycling along with the exploitation of the biogas
produced limits the increase of methane emissions. At the same time, emissions
from wastewater handling have considerably decreased, due to the continuous
increase of the population served by aerobic wastewater handling facilities.
GHG Time Series Trend Assessment
In order to evaluate the trends of GHG emissions time series the indicators
presented in Fig. 4.4 were used. Figures present the variation of the indices
compared to the base year (base year index value¼ 100). The base year is 1990 or 2000, respectively, depending on the availability of data (Project: ODYSSEE-
MURE 2012).
40 I. Sebos et al.
Figure 4.4 presents two indices of GHG emissions in relation to the country’s economic development and population, respectively. As shown in the Figure, both
the total, and the energy related index have decreased significantly compared to
2000 (approximately 17.1% and 14.7%, respectively). Thus, the increase in the
GDP for the period 2000–2008 was not accompanied by a respective increase of
GHG emissions. The entry of natural gas and renewable energy in the energy mix,
and other policies and measures, such as energy saving are significant contributions
to the above reduction. The increase of the indicators in recent years compared to
previous years is probably due to the abrupt decrease in GDP (denominator) due to
the economic crisis of recent years.
Figure 4.5 presents two power generation related indicators. Both indicators
have decreased significantly compared with 1990 (about 27.6% in terms of CO2 specific emissions of public and auto producer power plants and 28.6% for the
electricity carbon intensity of total power generation). The reduction of GHG
emissions compared to the generated electricity is the result of policies and mea-
sures such as the admission of natural gas in the energy mix, the use of renewable
energy sources (RES), the modernization of power plants in combination with
energy saving measures etc. The index of total generation presents a lower value
because it includes the production of electricity from RES.
Figure 4.6 shows the industry assessment index relative to its growth (gross
value added—GVA). The index referring to industry presents a decrement by
27.6% compared to 2000. Thus, the development of industry (the period
2000–2007, as after 2008 GVA reduced) was not accompanied by a corresponding
increase of GHG emissions.
Finally, in Fig. 4.7 the indicators for the residential and tertiary sectors are
presented. For households an increase in GHG emissions per household for the
100
95
90
85
80
75
70
65
60 2000 2005 2010
Total CO2 intensity of GDP
Total CO2 intensity of inhabitant
Energy related CO2 intensity GDP
105
110 Index 2000=100
Fig. 4.4 Carbon intensity of GDP and population
4 Mitigation and Adaptation Policies Related to Climate Change in Greece 41
period 2000–2003 occurs, which is explained by the improvement of living stan-
dards due to the economic growth of the period. Then, the index decreases despite
the continued economic growth, mainly due to the gradual replacement of heating
diesel by natural gas and the implementation of energy saving measures. Respective
conclusions result from the tertiary sector. It should be noted that the above
indicators roughly reflect the GHG emissions from burning fossil fuels for heating
needs for each home or building in the tertiary sector, so they are strongly
influenced by the climatic conditions during winter period of each year (i.e. how
hot or cold the winter was every year).
20001990 2010
Specific CO2 emissions of public and autoproducer power plants
Carbon intensity of total power generation
100
95
90
85
80
75
70
65
60
105 Index 1990=100
Fig. 4.5 Carbon intensity of power generation
2000 2005 2010
Specific CO2 emissions of households
CO2 intensity of the commercial and institutional sector
180
160
140
120
100
80
60
Index 2000=100
Fig. 4.6 Evaluation indicator of industry (based on gross value added)
42 I. Sebos et al.
Level of Achievement of the National Commitment Under the KP
The GHG emission projections presented in this paper are based on the latest
official energy projection scenarios approved by the Ministry of Environment,
Energy and Climate Change. In Fig. 4.8 the evolution of GHG emissions and
their projections till year 2020, along with the assigned amount of Greece for the
first commitment period of Kyoto Protocol are presented.
The fulfillment of the Kyoto Protocol target (first commitment period) is eval-
uated through a comparison between the total GHG emissions of the years
2008–2012, and the Assigned Amount of Greece for the same period
(668,669,806 t CO2 eq). As it is obvious (Fig. 4.8), Greece achieves Kyoto Protocol
target for the first commitment period, on the basis of the domestic policies and
measures implemented; and there was a surplus of allowances of GHG emissions of
approximately 44 million AAUs.
The presented progress of the country in achieving the emission reduction
targets for the period 2013–2020, concerns only the case of non-ETS sectors,
since the emissions of sectors covered by the ETS will be regulated by the
Emissions Trading System (ETS). Thus, projected emissions from non-ETS sectors
and annual emissions allocation for the years 2013–2020, are presented in Fig. 4.9.
Comparing the annual emissions allocation for the years 2013–2020 (Annex 1 of
2013/634/EU), which reflect the non-ETS target of Greece pursuant to European
legislation (2013/162/EU and its amendment 2013/634/EU), with the projected
emissions from non-ETS sectors, it is concluded that Greece will meet this target,
on the basis of the domestic policies and measures. It should be mentioned that this
conclusion is based on the comparison of projections and annual emissions
Energy related CO2 intensity of gross value added of industry
2000 2005 2010
100
90
80
70
50
60
110
Index 2000=100
Fig. 4.7 Evaluation indicators of the residential and commercial sectors
4 Mitigation and Adaptation Policies Related to Climate Change in Greece 43
allocation calculated by applying global warming potential values from the second
IPCC assessment report. However, the same conclusion would result if global
warming potential values from the fourth IPCC assessment report were considered
(Ministry of Environment Energy and Climate Change (MEECC) 2014a; European
Commission 2014).
1985 1990
140,000.00
130,000.00
120,000.00
110,000.00
100,000.00
90,000.00
80,000.00 1995 2000 2005 2010 2015 2020 2025
Fig. 4.8 GHG emissions projections
2013
65000
Kt CO2 eq. Assigned Amount Units (AAUs) for
non-ETS sectors
Level of achievement of the national
commitment for the years 2013-2020 for
non-ETS sectors 60000
55000
50000
45000
40000 2014 2015 2016 2017 2018 2019 2020 2013 2014 2015 2016 2017 2018 2019 2020
Fig. 4.9 Projected emissions from non-ETS sectors and annual emissions allocation for the years 2013–2020—level of achievement of the national commitment for the period 2013–2020
44 I. Sebos et al.
Effect of GHG Mitigation Policies
The most important policies related with the implementation of measures for the
mitigation of GHG emissions in Greece are (Ministry of Environment Energy and
Climate Change (MEECC) 2014a):
• The National Renewable Energy Action Plan, which sets out Greece’ national targets for the share of energy from renewable sources consumed in transport,
electricity and heating and cooling in 2020, taking into account the effects of
other policy measures relating to energy efficiency on final consumption of
energy, and adequate measures to be taken to achieve those national overall
targets (raising the share of EU energy consumption produced from renewable
resources to 20%).
• The National Energy Efficiency Action Plans, which covers significant energy
efficiency improvement measures and expected and/ or achieved energy savings,
including those in the supply, transmission and distribution of energy as well as
energy end-use. (Measures for the improvement of energy efficiency.)
• The continuous development of the transmission and distribution network of
natural gas, and the promotion of its use.
• The European emissions trading scheme (Directive 2003/87/EC) the operation
of which started in 2005. In Greece, the trading system for the period 2008–2012
comprises 140 industrial installations (power plants, refineries, cement plants,
etc.). An allowance reserve is also created which is intended to cover possible
unknown new entrants in the period. In 2013, the EU ETS is now in its third
phase, running from 2013 to 2020. A major revision in order to strengthen the
system means the third phase is significantly different from phases one and two
and is based on rules which are far more harmonized across EU than before.
• The fiscal measures that support policies and measures that reduce GHG
emissions, such as the tax regime of energy products, the registration tax of
vehicles, the Motor vehicle circulation fee (road tax), the income taxation—
relief and exemptions.
The total realistic GHG emissions reduction potential from the
implemented and adopted policies and measures was estimated to be 33.3 Mt CO2 eq. for 2015 and 41.0 Mt CO2 eq. for 2020. The possible interferences
between these implemented/adopted measures, which may restrict the estimated
GHG emissions reduction potential, were taken into account. Thus, it is obvious
that the application of the already implemented and adopted measures for
the mitigation of GHG emissions contributes considerably in the restriction of the
augmentative trend of emissions (besides the economic recession), leading to the
achievement of the 2020 target, exclusively with domestic measures and actions.
4 Mitigation and Adaptation Policies Related to Climate Change in Greece 45
Adaptation Measures for Climate Change
Adaptation may include both national and regional strategies as well as measures
at community level or by individuals. Although an over-arching adaptation strategy
is not yet available in Greece, adaptation measures are currently under implemen-
tation as part of a broader network of measures that apply to the specific areas of
identified vulnerabilities. It is worth noting that the Overall National Strategy for
Adaptation is ongoing and is a key priority of the country (Ministry of Environment
Energy and Climate Change (MEECC) 2014a; Bank of Greece 2013).
Greece already has a National Biodiversity Strategy and Action Plan for its
implementation, based on a project that started in 1999 and was completed in 2014
(Ministry of Environment Energy and Climate Change (MEECC) 2014b). The aim
of the strategy is to stop the loss of biodiversity and degradation of the ecosystems
in Greece until 2026, as well as the promotion of biodiversity as a national issue.
Aiming to the adaptation of the country concerning the agricultural sector
Greece is participated in the Project ADAGIO—ADAptation of AGriculture in
European RegIOns at Environmental Risk under Climate Change. The project is
focusing on improving awareness and user-orientation of adaptation strategies,
improving local representation and considering the main vulnerable regions to
Climate Change in Europe. In addition, the National Action Plan for Combating
Desertification (2001) sets as an objective to combat efficiently the desertification
trends in the 35% of the whole Greek territory that is under direct threat and to
prevent the desertification process elsewhere. The main issues in relation to agri-
culture are erosion of soils and drought problems.
The national strategy concerning forest ecosystems is implemented via the
Program of Rural Development (RDP) 2007–2013 “Aleksandros Mpaltatzis”
(MRDF), under which 69 projects have been implemented by the Forestry Services,
aiming at the enhancement of forest fires prevention and restoring of forest burnt
area, along with anti-erosion, anti-flood works for prevention of flooding in the
lowlands and for restoration of forest burnt areas. In addition, a Lifeþ project “Adaptation of forest management to climate change in Greece (AdaptFor)” was
implemented, aiming at enhancing the capacity of forest services to adapt forest
management to climate change and to disseminate the need for adaptation of forest
management to other stakeholders and to the general public. Natura 2000 network
has also a key role in protecting and enhancing our natural capital. In addition to
safeguarding nature’s intrinsic value, investing in Natura 2000 provides multiple benefits to society and the economy at the local, regional, national and EU level.
Finally, The National Action Plan for Combating Desertification was approved
in 2001 and includes measures to reduce the frequency and decrease the spread of
forest fires.
The Greek Operational Programme “FISHERIES 2007–2013” was approved by the European Commission, with a strategic objective focusing on
“Measures for the adaptation of the fishing fleet”. Concerning aquacultures,
46 I. Sebos et al.
possible adaptation measures to climate change include institutional measures,
policy measures and action planning which are summarized as follows:
(a) Insurance aquaculture, (b) Technology transfer and research,
(c) Diversification of crop species, (d) Adoption of selection systems for the
installation and monitoring of aquacultures.
In the water resources sector, according to the National Action Plan for
Combating Desertification, the suggested measures include: reduction of water
loss through the improvement of irrigation efficiency, reduction of water losses and
demand in urban and industrial use and increase of water supply through funding of
programs for water recycling and reuse, etc. In addition, the MEDROPLAN
Project: “Mediterranean Drought Preparedness and Mitigation Planning” focuses
on developing Guidelines for drought preparedness plans and to setting up a
Network for drought preparedness in Mediterranean countries. The Guidelines
provide an integrated approach to face droughts from a risk management perspec-
tive and therefore minimizing the impacts of drought in the population and
resources.
Concerning coastal zones the General National Framework for Spatial
Planning and Sustainable Development includes priorities that avoid the expan-
sion of existing settlements, especially along the coast; encourage expansion in the
areas where population density permits it; protect beaches and natural coastal areas,
assure public access etc.
The following measures promoted by the tourism sector and especially the
Greek National Tourism Organization include adaptation of an appropriate mar-
keting strategy aiming at diversification through the development of new tourism
product and distinctive destination brands, promotion of sustainable tourism (eco-
tourism, nature based tourism, rural tourism), promotion of Green Destinations,
encouragement of sustainable business practices, providing tools and guidance to
the tourism industry and investors and new technologies to improve energy
efficiency.
The National Action Plan for the ‘Response of Environmental Hazards Threatening Health’ for 2008–2012 included a special action dedicated to the ‘Exploring of Climate Change Impacts on Health’, primarily referring to the identification, research and documentation of the impacts. At the national level,
the governments of Europe have been developing actions to address the impacts of
climate change: (1) The national health ministries have launched actions to ensure
equal access to health services and social justice for all victims of climate change.
(2) The national health ministries will also need to design special action plans to
address the public health problems. (3) Hospitals will also need proper infrastruc-
ture and equipment. (4) Healthcare personnel will need to receive training in
environmental epidemiology and the health implications of climate change, etc.
In addition the General Framework of Spatial Planning and Sustainable
Development has the following specific objectives:
• Constant care for energy-saving;
• Promotion of alternative, and in particular renewable, energy sources;
4 Mitigation and Adaptation Policies Related to Climate Change in Greece 47
• Protection and enhancement of natural processes;
• Adaptation to new climate change conditions and mitigation of their conse-
quences (fires, floods, erosion, drought, water salinization, desertification etc.),
by putting in place mitigation mechanisms, appropriate infrastructures and plans
for action.
The proposed policies and specific policy measures for coping with the impacts
on the transport system include:
• Development of monitoring systems for crucial infrastructure and use of ‘smart’ decision-making, risk management and disaster management systems, etc.
• Use of new materials, more resilient to extreme weather conditions.
• Policy measures aimed at reducing transport demand, e.g. carpooling, mobility
management, school transport, etc.
• Promotion and support of eco-driving.
• Use of ‘smart’ technologies and systems with a view to improving freight transport and maximizing capacity use of all means of transport (target: zero
empty routes), etc.
References
Bank of Greece. (2013). Environmental, economic and social impacts of climate change in Greece.
European Commission. (2014). European Union transaction log. http://ec.europa.eu/environment/ ets/.
European Commission/DG Climate Action/ European Environment Agency. (2014). The 2020 climate and energy package. http://ec.europa.eu/clima/policies/package/index_en.htm.
European Environment Agency (EEA). (2014). Total greenhouse gas (GHG) emission trends and projections (CSI 010/CLIM 050). Assessment published November 2014.
European Environment Information and Observation Network (EIONET). (2014). Central data repository. http://cdr.eionet.europa.eu/gr.
Ministry of Environment Energy and Climate Change (MEECC). (2013). Annual inventory submission of Greece under the convention and the Kyoto protocol for greenhouse and other gases for the years 1990–2012.
Ministry of Environment Energy and Climate Change (MEECC). (2014a). Sixth national commu- nication and 1st biennial report under the United Nations framework convention on climate change.
Ministry of Environment Energy and Climate Change (MEECC). (2014b). National strategy & action plan for biodiversity.
Official Journal of the European Union. (2013). COMMISSION IMPLEMENTING DECISION of 31 October 2013 on the adjustments to Member States’ annual emission allocations for the period from 2013 to 2020 pursuant to Decision No. 406/2009/EC of the European Parliament and of the Council (2013/634/EU).
Project: ODYSSEE-MURE. (2012). Key indicators, final energy intensity. http://www.indicators. odyssee-mure.eu/online-indicators.html.
United Nations Framework Convention on Climate Change (UNFCCC). (1998). Kyoto protocol to the United Nations framework convention on climate change.
48 I. Sebos et al.
United Nations Framework Convention on Climate Change (UNFCCC). (2007). Report of the review of the initial report of Greece.
United Nations Framework Convention on Climate Change (UNFCCC). (2015). Doha amendment to the Kyoto protocol.
4 Mitigation and Adaptation Policies Related to Climate Change in Greece 49
Chapter 5
Assessing Air Quality in the Urban Environment: the Gender Gap
Theodora Slini and Fotini-Niovi Pavlidou
Introduction
Gender Priorities in the European Union
Climate change affects both women’s and men’s living conditions, welfare and wellbeing, however due to gender roles, women do not affect the environment in
the same way as men, and in many countries women’s access to resources, and hence their opportunities to manage conditions and adapt are quite limited
(IPCC 2014).
At the same time, environmental policies are characterized by lack of sensitivity
to women’s different economic and social status and needs, having as a result women to be directly and disproportionally affected from environmental degrada-
tion. While consumption and lifestyle patterns still differ between two genders,
with women to consume less and being more environmentally conscious, “women
are clearly under-represented in environmental negotiations, budget deliberations
and decisions on achieving a green, sustainable economy” (EC 2012). According to
‘Gender aspects of the economic downturn and financial crisis European Parliament resolution of 17 June 2010 on gender aspects of the economic downturn and
financial crisis (2009/2204(INI))’, the European Parliament “urges the need to
T. Slini (*) Laboratory of Heat Transfer and Environmental Engineering, Centre of Space, Technology
and Gender, School of Engineering, Aristotle University of Thessaloniki, Box 483, 54124
Thessaloniki, Greece
e-mail: [email protected]
F.-N. Pavlidou
Department of Electrical and Computer Engineering, Centre of Space, Technology and
Gender, School of Engineering, Aristotle University of Thessaloniki, Box 489, 54124
Thessaloniki, Greece
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_5
51
encourage women in local entrepreneurial initiatives in green economy”. The
European Parliament (2012) resolution of 11 September 2012 ‘on the role of women in the green economy (2012/2035(INI))’ “calls on the Commission and the Member State to introduce gender equality into all environmental policy areas”
and introduce gender equality into all environmental policy areas, and at all levels
of economic decision-making. On 14 November 2012 the European Commission
published its proposal for a Gender Diversity Directive for improving gender
balance on company boards, obliging companies with less than 40% of women
non-executive directors to make significant efforts to make appointments in the
next 7 years to reach this target.
Furthermore, the Opinion of the European Economic and Social Committee on
‘The gender dimension in the Europe 2020 Strategy’ 2013/C 76/02 (EU Legislation 2013), the Commission is “highlighting the essential role played by women in
sustainable development”, while “women can have a key influence on decision-
making concerning the environment, particularly with regard to climate change
policy. This is a new opportunity for women, who can play a key role and improve
their personal and financial situation by getting involved with the new and emerging
green economy, which is a crucial sector for development and job creation”. After
all “women’s activism was critical in getting the conversation started,” according to historian David Stradling, author of “Smokestacks and Progressives: Environmen-
talists, Engineers and Air Quality in America, 1881–1951.”
In response to these requirements a gender perspective is a critical assumption
towards a sustainable environment and a green economy in terms of the ecosystem,
consumption, food, growth, transport, energy and citizen welfare.
Gender Priorities in Greece
According to the National Strategic Reference Framework (NSRF) for 2014–2020,
the main tools for the implementation of gender policy will be integration of equal
opportunities between men and women in all institutions, policies and actions
(gender mainstreaming) and the assumption of certain specific activities in the
following areas:
• equal participation women in the labor market,
• the participation of women outdoor activities aimed at local development,
• promotion of inclusion of women, prevention and control of female poverty and
all forms of gender-based violence,
• mainstreaming of gender issues in social protection and health,
• support family,
• equal participation of women in public life and processes of political, social and
economic decisions,
• combat discrimination based on sex and gender stereotypes and
• the integration of gender equality in public policies, monitoring and evaluation.
52 T. Slini and F.-N. Pavlidou
However, the Greek Legislation does not include the gender perspective as a
critical parameter through its development and implementation and in many cases it
is characterized as neutral or negative, according to a report by the General
Secretariat for Gender Equality (2013). For example,
1. The Law 4067/2012 (OG A79/9-3-2012) the “New Construction Regulation”
that includes a number of provisions on accessibility of buildings and built
environment. Regarding the motivation for environmental enhancement and
the improvement of quality of life in densely populated urban areas, which
gender neutral with no comment on specific needs.
2. The master plan for urban planning and environmental protection of the greater
Thessaloniki area (L. 1561/1985) refers to the daily needs of citizens ignoring
the gender matters. Special requirements due to diverse living habits and rou-
tines as well as the different ways in which environment is perceived and used
between men and women should be considered for the optimum urban planning
and city upgrading.
The most recent L. 3653/2008 on Research and Technology establishes the
minimum proportion of male/female participation in national committees of
research and development, that is at least 1/3 of each gender, as long the candidates
are equally qualified.
Results and Discussion
Gender, Air Quality and Global Warming
Despite it is widely accepted that balanced participation of men and women in
decision-making is a prerequisite for improving the operation of democracy and
society, the ongoing under-representation of women in political and economic
decision-making reflects a basic democratic deficit in Europe and the broader
international context. At the same time it is important to highlight that the female
population is more vulnerable in effects of environmental degradetation and poor
air quality (UN 2014; Fouillet et al. 2007). Furthermore, as suggested by Druckman
(2012), the investigation of the concept of carbon footprint as a potential marker for
social justice, a higher proportion of an average man’s carbon footprint is due to leisure than an average woman’s.
There are several studies that prove that poor air pollution conditions can
generate negative effects in the female population in both rural and urban sites
(Xu et al. 2013; Huisman et al. 2005; Oiamo and Luginaah 2013; Künzli
et al. 2010). The proportion of women and young children is mainly affected as
these groups of population spend most of their time indoors where solid fuels, fire
places and cooking stoves are in extensive use. According to WHO (2014), around
three billion people cook and heat their homes using open fireplaces and stoves
5 Assessing Air Quality in the Urban Environment: the Gender Gap 53
using various burning materials. These materials are not always the appropriate
ones, causing the death of over four million people prematurely from illness due to
the poor indoor air quality. The mortality of premature deaths among children under
5 attributed to household air pollution is also extremely high.
Additionally according to The European environment—state and outlook 2010
(EEA 2010), vulnerable population groups (e.g. pregnant women) are more threat-
ened by the bio-accumulation of organic persistent pollutants such as mercury.
Chen et al. (2005) and Miller et al. (2007), the associations of PM2.5 and cardio-
vascular morbidity and mortality were greater in women above 60 and at the same
time Xu et al. (2013) states that air pollution (referring to air pollutants such as NO2,
SO2, PM2.5, O3 and CO) increases risk for hypertension in pregnant women during
early pregnancy and the full gestational period.
Ambient air pollution has stronger effects on females partly due to autoimmune
disorders. Females were more likely to report cardinal symptoms after controlling
for income, age and chronic diseases (Oiamo and Luginaah 2013). As Bakke
et al. (2007) suggests female gender has reported health symptoms more often
than did men and complained more about physical but not psychosocial factors
gender, psychosocial, and physical environment factors were related to symptoms
and perceived indoor climate. Female gender seems to be highly associated with the
sick building syndrome and the symptom of atopia (Magnavita 2015).
Several studies have linked air pollution exposure to autism, including the Volk
et al. (2011) study in Environmental Health Perspectives that looked at children in Los
Angeles who lived near freeways and the Hallmayer et al. (2011) study that analysed
traffic-related air pollution exposure data among pregnant women. The main conclu-
sion of the studies was that a large proportion of the variance in liability can be
explained by shared environmental factors in addition to moderate genetic heritability.
In general, studies suggest that health responses to air pollutionmay differ between
women and men, however it is still unclear, whether observed modification is a result
of sex-linked biological differences or gender differences in activity patterns or
exposure measurement accuracy (Clougherty 2010). Cautious consideration of gen-
der effects and examination in environmental epidemiology may provide critical
information on other social factors that can affect population response to air pollution.
In addition, in countries that face the severity of current financial crisis, struc-
tural changes occur in European members states as well, including migration and
changing of household structures due to energy poverty. For example, in Greece, an
exponential increase of wood and pellet employment is monitored primarily for
heating purposes (Slini et al. 2014; Santamouris et al. 2013), posing major concern
especially for women health (Fig. 5.1), based on the results of a survey conducted in
Northern Greece by the Department of Mechanical Engineering, Aristotle Univer-
sity of Thessaloniki (AUTh).
In Greece, due to the economic situation the consumption of oil products, which
are the main fuel that is used by the household sector, decreased already by 25.7%
between 2007 and 2010. What is impressive is the exponential increase in the use of
wood and pellets, a trend that has begun to have its first implications in matters of
air quality, both indoor and outdoor, but also in an enhanced deforestation, with
54 T. Slini and F.-N. Pavlidou
major field studies being currently carried out on those matters (Slini et al. 2014).
Towards this direction many countries in Europe are adopting policies and effective
precautionary measures in order to reduce the exposure of vulnerable population
groups in toxic environments (EEA—European Environment Agency 2015).
At the same time, research on gender-related disparities are mainly focused on
energy consumption profiles and transport use. As pointed out at the Report on
Gender Equality and Climate Change (EIGE 2012a), the most significant gendered
differences in energy consumption were monitored in Greece and Sweden, with
men energy consumption reaching a proportion of 39% and 22% more than
women, respectively. Moreover, it is suggested that women use the public transport
or other sustainable means of travel more often than men.
Gender Balance in Environmental Decision Making
As global warming is a multi-fold issue and the abatement policy (e.g. GHG
emissions, legislation, and limit values) requires an interdisciplinary approach
conducted within environmental authorities. Thus, the gender distribution in
authorities responsible for climate change adaptation/mitigation measures is sub-
stantial (genderSTE 2014).
According to EU data, concerning environmental governing positions in
European States, such as senior and junior ministers in environment, energy and
transport at national governments, the women participation was slightly increased
Electricity Woodc d
2000
1500
1000
500
0 2011 2012
−31.5%
Oila lt
3000
2000
1000
0 2011 2012
−2.5%
kW h
1000 800 600 400 200
0 2011 2012
+325%
kg
b
N m
3
−21%
2011 2012
Natural gas
800
600
400
200
0
Fig. 5.1 The average annual fuel and electricity consumption for the years 2011–2012 by type: (a) oil in litres, (b) natural gas in N m3, (c) electricity in kilowatt-hours and (d) wood in kilograms
5 Assessing Air Quality in the Urban Environment: the Gender Gap 55
from 20% to 27% during the last 3 years (2012–2014), a proportion that is still
significantly lower than male proportion (Fig. 5.2). In Greece during the same
period there was no female representation.
However, the national administration positions show a slightly improved distri-
bution with the female proportion increasing from 33% to 36% between 2012 and
2014. In Greece the data are considerably more balanced compared to the European
figures, though decreased from 48% to 45% from 2012 to 2014 (Fig. 5.3).
It is noteworthy to mention that in a broader approach the representation of
women in boards of large listed companies is also discouraging, with major gaps
and little progress on women representation and career evolution, as presented in
Fig. 5.4, in both the European Member States and Greece. More recently, and
specifically in October 2014, Greece stands for the proportion of 8.9% of women in
highly ranked position with a European average of 20.2% (EC 2015).
Having the aforementioned facts under consideration, the European Commis-
sion has established a set of indicators in order to determine and evaluate the
women’s participation in decision making on climate change (EIGE 2012b), that is the following:
• Proportion of women in climate change decision-making bodies at the national
level in EU Member State.
• Proportion of women in climate change decision-making bodies at the EU level.
• Proportion of women in climate change decision-making bodies at the interna-
tional level.
• Proportion of women tertiary graduates of total graduates in natural sciences and
technologies at the EU and Member State level.
Fig. 5.2 The proportion of men and women in environmental ministers (senior and junior) in European Member States for the period 2012–2014
56 T. Slini and F.-N. Pavlidou
The development and collection of such data will support the study of gender-
climate change issues and may provide the benchmark for the development of new
indicators about the correlation between gender, environment and social welfare
and justice.
Conclusions
The current study unveil the relations and links between gender and global warming
at national and European level. It is proven that there are dissimilarities between
males and females regarding global warming attitudes, contributions and capabil-
ities of adaptation in the mitigation measures and the socio-economic impacts of
climate change policies. As little progress is achieved, it comes without saying that
gender perspective is a critical assumption towards a sustainable environment and a
green economy in terms of the ecosystem, consumption, food, growth, transport,
Fig. 5.3 The gender distribution of environmental national administrators (a) in the European Member States and (b) in Greece for the period 2012–2014
Fig. 5.4 Representation of women and men (absolute numbers) on boards of high listed compa- nies (a) in the European Member States and (b) in Greece for the period 2003–2010
5 Assessing Air Quality in the Urban Environment: the Gender Gap 57
energy and citizen welfare. As the engendering of decision making on climate
change will reinforce and will improve the efficiency of the suggested policies, the
systematic research and monitoring of gender equality data and development of
awareness initiatives are on the top of the agenda of policy recommendations.
Quantitative targets and strong commitment on gender equality on environment
and global warming by national governments, international institutes and authori-
ties are critical areas of concern towards sustainable social development.
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5 Assessing Air Quality in the Urban Environment: the Gender Gap 59
Chapter 6
Promotion of Sustainability by Quantifying and Reducing the Carbon Footprint: New Practices for Organizations
Monica Carvalho, Rommel de Santana Freire, and Alexandre Magno Vieira Gonçalves de Brito
Introduction
Until recently, companies and organizations had the opinion that the environment
and sustainable development were problems and risk factors. However, the pro-
gressive development of a generalized, global environmental conscience created a
demand for products (processes, services) that are more environmentally-friendly
(with less associated impacts), for which there are great advances and developments
in the application of eco-efficiency principles by industries and designers.
Nowadays, these “problems” are seen as opportunities, as possibilities for
growth and efficiency improvement. According to the World Business Council
for Sustainable Development (WBCSD 2000), eco-efficiency is basically the art of
doing more with less: better production, with the consumption of less resources. But
eco-efficiency is not only defined as the search for energy efficiency, it also
stimulates creativity and innovation in the search for the best way to do things
(WBCSD 2000). Achieving eco-efficiency does not mean the complete elimination
of environmental impacts caused by man, rather lowering these impacts to levels
M. Carvalho (*) Department of Renewable Energy Engineering, Center of Alternative and Renewable Energy,
Federal University of Paraı́ba, Caixa Postal 5115, Cidade Universitária, Jo~ao Pessoa 58051- 900, Paraı́ba, Brazil
e-mail: [email protected]
R. de Santana Freire
Department of Accountancy and Finances, Center of Applied Social Sciences, Federal
University of Paraı́ba, Cidade Universitária, Jo~ao Pessoa 58051-900, Paraı́ba, Brazil e-mail: [email protected]
A.M.V.G. de Brito
Department of Mechanical Engineering, Center of Technology, Federal University of Paraı́ba,
Cidade Universitária, Jo~ao Pessoa 58051-900, Paraı́ba, Brazil e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_6
61
that are more compatible to the current degree of environmental conscience.
According to Silva (2010), the environmental impacts caused by human activities
are also studied in parallel with the development of solutions to increase
eco-efficiency, to allow for the perception of solutions.
According to Ribeiro (2011), the oil crisis in the 1970s sparked the concern of
society with the depletion of fossil fuel reserves, and as a consequence, the first
environmental analyses were carried out. The interest in these analyses was not
constant throughout the years, and was rekindled in the 1990s with the creation of
the ISO 14040 norms and increase in environmental discussions. In 2006, Lima
et al. (2006) mentioned that there was a progressive interest of industry, as well as
of environmental specialists, authorities, consumer associations, environmental
associations and general public, in the environmental quality of production pro-
cesses and products.
In this current scenario where emphasis is on the minimization of dependency in
fossil fuels along with the integration of alternative energies (progressively increas-
ing participation of renewable energies), quantification of environmental impacts
has been established as a powerful tool that creates awareness. Some studies go a
step further by searching not only for the optimal solution from an environmental
viewpoint (Carvalho et al. 2011a, b), but for a balance or equilibrium between
different points of view (environmental and economic perspectives: Carvalho
et al. 2011a, b; Buoro et al. 2013). Quantification of environmental impacts have
been utilized by developed countries for many years, and the European Union
(EU) has even declared Life Cycle Assessment to be a state-of-the-art methodology
and included related aspects in the 6th Environmental Action Programme, to assure
that environmental legislation is adopted to attack most of the environmental
challenges in the EU (EIONET 2003).
Modern companies and institutions have aimed at a balance situation between
the expansion of businesses and preservation of the environment, where sustainable
growth is the fundamental point for the efficient management of resources. Accu-
rate knowledge on productive processes is essential for the organizations to mea-
sure costs and risks; when not measured or correctly controlled, revenue can be
significantly decreased to the point of non-viable business in some cases. Correct
quantification of the environmental loads of a specific process, or sector, helps the
company optimize costs and reduce risks, avoiding future liabilities in function of
environmental damages caused. In this way, from the a priori knowledge on the
amount of environmental loads generated, companies can establish targets for
reduction/mitigation of pollution levels and promote the results to society in a
clear manner. The company will publicize the reduction in the pollution generated
by its activities as a contribution to the sustainable development of its surroundings.
The reduction in environmental loads can be achieved through improvements in
processes and products, installation of new equipment, capture and treatment of
generated residues for posterior discharge or even sale. Companies can generate
non-operational revenues, which can add up to relevant volumes, from the negoti-
ation of processed/treated residues and also from the sale of carbon credits, gener-
ated from the elaboration of Clean Development Mechanism (CDM) projects. In
62 M. Carvalho et al.
these projects, the volume of reduced emissions can be converted into a commodity,
and negotiated in the financial market, which has been increasing substantially in
recent years (Pirrong 2011). Therefore, the reduction in the levels of emissions
brings, besides the environmental benefits, also financial benefits, allowing for the
sustainable growth of organizations.
Brazil should, as always, accompany the global trends of environmental con-
science. The objective of this manuscript is to explore the relationship between the
environmental loads generated by companies, with society and governments. This
relationship is based on the tripod QUANTIFY-REDUCE-PROMOTE and can be
extended to assess what society itself emits. The idea supporting this project is that
the social perception of companies developing studies for the quantification of
environmental impacts will be improved. It is important to highlight that the
quantification study is the first step: then, points are identified where improvements
can be introduced for posterior reduction of emissions. The next step is to promote,
disseminate these results, which returns to the initial idea: improvement of social
perception and popularity of the company. If the consumers or clients perceive that
the company is concerned with the environment, they are more inclined to be loyal
to the brand.
Diagnosis and Analysis of the Situation
Due to the progressive development of environmental conscience by the society,
along with ever-increasing pressure to reduce environmental loads, emerges the
necessity of considering the environment as an additional criterion at the time of
designing or building products and processes (Carvalho et al. 2012). Therefore, the
evaluation of the performance of products, processes or services depends less on
economic criteria and starts to include, progressively, environmental components.
Developed countries committed to reducing their greenhouse gas (GHG) emis-
sions through the Kyoto Protocol, at the end of the 1990s. This commitment is
mandatory only for developed countries, reflecting the international consensus that
industrialized countries must lead the process of mitigation of climate change (Baer
et al. 2000). Developed countries should not only reduce their emissions, but also
produce technology and means to help developing countries (Baer et al. 2000;
Ashton and Wang 2003). Developing countries insist that the solution for climate
change cannot be achieved at the expense of their development (Yale 2014).
According to Yale (2014), it is obvious that a reduction in emissions should also
be the goal of developing countries, but economic growth and decrease of poverty
are connected to the lack of access to energy services. Development seems to be
linked, therefore, to an unavoidable increase in the use of fossil fuels and conse-
quently, of GHG emissions. Apart from the multiple schemes for allocation of
emissions, the United Nations Framework Convention on Climate Change has
already recognized that the global nature of climate change requires the broadest
collaboration possible from all countries, and their united participation in an
6 Promotion of Sustainability by Quantifying and Reducing the Carbon Footprint. . . 63
adequate international response, following a common but differentiated responsi-
bility according to the capacity of each country (UNFCCC 2014).
There are also technical-operational arrangements, regulated by the Kyoto
Protocol, that can be utilized by companies or countries. These arrangements
offer different routes for the countries to achieve emission reduction limits and
goals. There are three “flexibilization” mechanisms (United Nations 2014): emis-
sion trading (countries that have reduced emissions even beyond the established
limit can transfer their reduction excess to another country that has not achieved its
limit); CDM, and joint implementation (GHG emission reduction projects in
countries that have set goals in the ambit of the Protocol). Only CDM is currently
applicable to Brazil. The regulation concerning CDM and carbon credits remains
underexplored in Brazil, but even without adequate regulation, in 2007 the first
auction sale of carbon credits took place in S~ao Paulo, corresponding to a volume of more than 800 thousand tonners of CO2-equivalent (CDM from a landfill project)
(Perera 2010).
Although GHG emissions are part of the development process of countries, the
increasing current environmental conscience demands that environmental impacts
are at least diminished (since they cannot be completely eliminated) in the search
for eco-efficiency (Carvalho and Freire 2014). During the 2009 United Nations
Climate Change Conference, Brazil voluntarily committed to reduce its GHG
emissions between 36.1% and 38.9% until 2020 (Marques et al. 2010). More
recently, in December 2014, during the Conference of the United Nations in
Peru, the text “The Lima call for Climate Action” (UNFCCC Newsroom 2014)
was announced. Countries can establish their own goals for the reduction of
emissions (Intended Nationally Determined Contributions), which, according to
Brasil (2014) represent the intended contribution of each country to the global effort
of mitigating climate change.
However these reduction efforts should not be limited to mitigation only,
including also efforts for adaptation, funding, technology transfer and training
(Brasil 2014). Although the word “intended” appears to indicate a non-binding
connotation, Brazil defends that the reduction targets should be juridically binding
(Brasil 2014). The Lima Call maintains the line that there is differentiated content
for developed and developing countries, according to the aforementioned principle
of common, but differentiated responsibilities.
Following the idea of sustainable development, consumers can already choose
which product to purchase based on the information shown on ecological tags or
labels. Ecological labels provide a measure of the environmental performance of
the product, informing the consumer about the environmental impacts. The con-
sumer is therefore enpowered, and this action reverberates in the market, as other
similar products will suffer pressure to adopt ecological labels; those that already
count with this label will also suffer pressure to minimize even more their impacts.
In a study carried out in France between 2004 and 2006, it was concluded that the
percentage of more selective consumers increased from 15% to 32% (Perera 2010).
64 M. Carvalho et al.
Still according to Perera (2010), more than 85% of French citizens believe they
play a crucial role in environmental matters, almost 90% prefer products and
brands that are environmentally correct, and 95% intended to research more on
the environmental impacts of consumer products. Ecological labels build on the
added value of environmental quality to the consumer (Csutora and Zs�oka 2012). The importance of providing environmental information to support more sustain-
able consumption has been repeatedly highlighted in policy reports and declarations
such as UN Agenda 21 United Nations, the EU Sustainable Consumption and
Production Action Plan and the UK Sustainable Development Report (Upham
et al. 2011).
The Blue Angel (Blaue Engel) was the pioneer in the labeling of products and
services, and was instituted in Germany in 1977 (Blaue Engel 2014). The European
Ecological Label was created in 1992, and has been raining awareness in companies
and consumers ever since (Spain 2014). In a parallel line of thinking, since 1993
Brazil counts with a seal from the National Program for the Conservation of
Electrical Energy, which is a simple way of informing the consumer on the
efficiency level and consumption of electricity of domestic appliances and equip-
ment (CBIEE 2006). This program was created by the Brazilian Government and
although limited, it is evident that Brazil attempts to follow the efforts of other
countries.
Entrepreneurship, which can be translated into the search for business opportu-
nities, might appear to be in the opposite direction of sustainability perspectives at
the long term—however, maybe because entrepreneurs present the unique ability to
combine, in an innovative manner, the individual viewpoint and the circumstances,
researchers already start to explore entrepreneurship as a potential mechanism for
sustainable development (Kosgaard and Anderson 2010). Despite the increasing
interest in this connection between sustainability and entrepreneurship, this rela-
tionship is still young but, according to York and Venkataraman (2010), entrepre-
neurs can contribute to the solution of environmental issues through the creation of
more sustainable products or services. From the moment a company or institution
manages to concentrate efforts to decrease consumption of energy or increase the
efficiency of a process, it provides some “relief” to the environment. The perception
of the consumer is positive, returning to the aforementioned environmental con-
science process. By giving preference to this product or service, the consumer
encourages the competition to decrease their own environmental impacts, closing
the cycle: less consumption of resources; less cost with resources; less environ-
mental impact. Gaining commitment and buy-in from the company is crucial. It is
also important to highlight the reductions achieved to promote the company as an
environmentally-friendly organization. This vision embraces the entrepreneur’s potential to supplement: (1) legislation; (2) social corporative responsibility; and
(3) activism in the solution of environmental issues (York and Venkataraman
2010).
6 Promotion of Sustainability by Quantifying and Reducing the Carbon Footprint. . . 65
The Quantify-Reduce-Promote (QRP) Proposal
The overarching intention of the proposal is to implement the concept of
eco-efficiency, which involves the extraction of the maximum potential of materials
and energy (efficient use), with the consequent minimization of environmental
loads and monetary costs (better use of resources means to use less and emit less,
with lower costs). International concern about climate change is beginning to
positively influence Brazilians, leading to evergrowing interest in the greenhouse
gas emissions involved in products, processes and services. The calculation of these
emissions is starting to become common in academic environments, however
actions directed to reduction and mitigation actions are still in an initial stage.
The reduction of environmental loads can only be confirmed after adequate
quantification, and in recent decades, different techniques for global environmental
assessment have been developed (e.g., ecological footprint, water footprint, carbon
footprint, Life Cycle Assessment—LCA, LEED-NH, to name a few). According to
Curran (1999), LCA is one of the most adequate tools to reach objectives directed
towards sustainability and is already an internationally accepted and recognized
tool, that evaluates the consequences of building and utilizing products and ser-
vices, through the identification and accounting of material used and disposal of
residues into the environment. However, sometimes due to limited resources and
data, companies carry out analysis based on simplified LCA approaches or apply
the general principals of Life Cycle Thinking (LCT) to specific aspects of the
productive system (De Benedetto and Klemeš 2009). LCT takes into consideration
all environmental and toxicological impacts associated with a product, process or
service, throughout its lifetime.
The first step in the proposal presented herein is to solidify LCT as a method-
ology applied not only to the quantification of environmental impacts of a product,
process or service, but also for the comparison of different alternatives, helping
decide on which option is better from an environmental viewpoint. In the light of
the above, the necessity of carrying out this project is justified, to pursue
eco-efficiency with support from the LCT/LCA methodology, which will help
decision makers make informed decisions from an environmental perspective, or
even find a commitment between economic and environmental perspectives. With
the information generated, it will be possible to establish internal environmental
policies that enable maximization of economic-financial results in equilibrium with
the preservation of the environment.
Along with the improvement of operational and economic results, there is a
concomitant improvement in the image of the company to society, created in
function of the reduction in the pollution/emissions generated. This type of public-
ity (promotion) is already utilized by large companies, especially those that have
titles being negotiated in the stock market. In Brazil, the Efficient Carbon Index
(ICO2) has sparked the interest of investors worried with environmental issues as
well as with revenue expectancy (BM&FBOVESPA 2011). The companies that
participate in this index are obligated to publish, in annual reports, the emission of
66 M. Carvalho et al.
GHG. However, small and medium sized enterprises do not present any interaction
with society, and therefore the existence of a great niche is confirmed for the
implementation of this project, especially in energy-intensive industries. In a
proactive and positive manner, good practices in environmental education will be
stimulated at the same time that environmental conscience is built in a responsible
way. Investments in green, positive marketing are important to increase market
share.
The traditional saying ‘what gets measured gets managed’ launches Phase 1, which starts with the QUANTIFICATION of environmental impacts through a
comprehensive, detailed environmental analysis. This analysis will allows for the
identification of the products, processes and services that are least aggressive to the
environment and will help quantify (and identify) critical aspects and even those
deserving special attention. This assessment can be extended to comprehend dif-
ferent products, processes or services. Another target for this Phase is the identifi-
cation of the configurations/options that are most adequate, through the
introduction of the environmental component as explicit decision element in syn-
thesis, design or operation stages.
Phase 2 of this project is the REDUCTION of environmental impacts, which
occurs after exhaustive analysis of the results of the QUANTIFICATION Phase.
This could lead to the formulation of an environmental strategy that could signal a
step change in environmental management for the studied company. Opportunities
for the REDUCTION of environmental loads can be identified, a priori, in energy
efficiency, introduction of renewable energy sources, and minimization of waste
(maximization of reuse and recycle). REDUCTION can be extended (but not
limited) to supplies and contracts (procurement), transport, construction and tem-
porary activities, and use of water. According to the Ministry for the Environment
of New Zealand (2015), these aspects are initially selected because they likely to
have the highest environmental impacts, are the most commonly addressed by other
major international organisms, and addressing them is consistent with international
government environmental policy priorities.
Phase 3 of this project is the PROMOTE, the dissemination of the results. The
dissemination, the advertising of the results is essential and therefore a specific
Phase of the project is dedicated to this activity, which includes analysis of results,
synthesis, conclusions, publicity and dissemination of results. The integration of the
previous results will provide a panoramic vision, much more complex and rich than
the simple addition of results: environmental evaluation, identification of opportu-
nities and innovative aspects to which R&D efforts must be directed, and recom-
mendations. Due to the high volume of information and data presented in Phases
1 and 2, a great effort of synthesis and creation will be necessary. Phase 3 will
influence consumers even when the cost of products is higher (in comparison with
competition or similar products). For example, Csutora and Zs�oka (2012) remark that hybrid cars are expensive (when the energy saved is accounted for, no cost
payback can be expected) but these vehicles still represent prestige or environmen-
tal value for some environmentally-conscious consumers and have achieved pre-
mium price position and small, but considerable market share.
6 Promotion of Sustainability by Quantifying and Reducing the Carbon Footprint. . . 67
The company involved in the project will be analyzed from different perspec-
tives, integrating, within an environmental focus, the productive sector with the
economic-financial management of the organization. A new focus will be therefore
created, generating wealth with an environmentally-responsible basis. Phase 1 is
not a simple activity, as it requires the mobilization of a significant amount of data
as well as a high consumption of time and computational effort. The product
(process, or service) must be described in detail, including inputs (material, energy)
and outputs (product, service, residues).
Special care is necessary to avoid any comparisons or relationships with green-
washing claims. Greenwashing is a type of deceptive marketing, used to provide the
image that a product is “green”. When combined with inexistent or ineffective
legislation, greenwashing could decrease the potential of the consumer to drive
companies in the direction of better solutions (Dahl 2010). The idea defended
herein is that good eco-labeling helps prevent greenwashing, and reduces consumer
skepticism.
Opportunities and Advantages
Some of the opportunities identified for the company that adopts the QRP proposal
are the development of a more strategic environmental approach, which will
position the company to better respond to customer needs, legislative requirements,
market changes and stakeholder expectations. Businesses and institutions aim at
respectability and need to build a good image, a good reputation and there are two
route to achieve these aspects: (1) lead the way, being the pioneer in building this
positive, environmentally-conscious image; or (2) be close to whom is a reference,
and follow their steps into achieving a good consumer perception.
Regarding the technological-social contribution of the project, it satisfies the
priorities of research, development and demonstration of new concepts and tech-
nologies to improve energy efficiency and reduce the final consumption of primary
energy. The minimization of environmental impacts is a benefit for all Brazilian
citizens. This project also presents a strong social bias, as the information on the
environmental loads embedded in a product, process or service provides decision
power to the consumer, who will be able to choose the least aggressive option,
forcing other manufacturers or suppliers to search for more “ecological” ways to
maintain competitiveness. The generation of economic-financial benefits represents
an extra advantage for the adoption of this project, enabling the company to recover
the investments made for its implementation. Already in 2006, Tachizawa predicted
that Brazilian consumers would start to give preference to products that were
environmentally responsible (Tachizawa 2006; Perera 2010). According to Tan
et al. (2014), voluntary carbon labeling schemes have been introduced in several
countries, with significant participation from companies that do not want to be seen
as lagging behind rivals in cornering the green market.
68 M. Carvalho et al.
There are also opportunities for carbon offsetting, where emissions can be
mitigated by investing in projects that avoid the production of emissions or remove
them from the atmosphere. According to the Ministry for the Environment of
New Zealand (2015), commitments to reduce emissions should always be accom-
panied by offsetting measures in order to be worthy of belief or confidence, as it is
more effective to avoid creating the emissions than elaborating strategies for
offsetting. Both emission reduction and offsetting can be integrated into an envi-
ronmental responsibility plan, and it is important to obtain the advice of experts. In
Brazil, during the 2014 Soccer World Cup, the Fédération Internationale de Foot-
ball Association (FIFA) announced a set of carbon offsetting projects in Brazil that
were selected to reduce the overall emissions of the tournament, which included
emissions from staff travel and accommodation, and extended to officials, teams,
volunteers and guests—four certified low-carbon development projects helped
achieve the goal (Fédération Internationale de Football Association 2014).
In recent years, the carbon market has progressively expanded and has become a
lucrative business for businesses. This market can also include stock market actions
and voluntary markets, where a business that reduces pollution generates compen-
sation credits and can sell them. In 2012, Brazil occupied the third position among
the countries that participated in the global carbon market, with approximately 5%
of the world total and 268 projects—however, initial estimates indicated that Brazil
would absorb 20% of the carbon credits (Brasil 2012). The CDM is a flexible tool
that allows the participation of developing countries (or countries with no reduction
commitments) in the carbon market, and has incentivized the creation of new
technologies for reduction of GHG gases in Brazil. There is a series of criteria for
recognizing carbon credit projects, such as alignment with the sustainable devel-
opment premises of the host country, defined by a Designated National Authority
(DNA)—in Brazil, this authority if the Interministerial Commission of Climate
Change, and only after approval of the Commission the project can be submitted to
the United Nations for evaluation and registry.
According to Perera (2010), paradoxically, the Brazilian clean energy matrix
could hinder CDM mechanisms in Brazil, but the country could become the largest
exporter of carbon credits—therefore it is important to be the first in this market to
reach leadership in the ability of recruiting international resources for sustainable
development.
Final Remarks
Encouraging consumers to make more informed choices requires access to envi-
ronmental performance information of products. The QRP project presented herein
has the ultimate goal of informing consumers about how the purchase of different
products within a substitutable range would have differing impacts on the environ-
ment. Since Brazilian consumers are starting to demand more data on how their
consumption patterns affect the environment, the adoption of the QRP proposal
6 Promotion of Sustainability by Quantifying and Reducing the Carbon Footprint. . . 69
helps businesses and institutions keep up with the competition through the provi-
sion of guidance to consumers on the impact of purchases on GHG emissions.
According to Tan et al. (2014), the implementation of carbon labeling is likely to
have positive effects on the environment.
Transfer of know-how from this project will increase the interest of Brazilian
industry and help the sector perceive the effect and importance of quantifying and
reducing the GHG emissions, with posterior transference (promotion) of results to
the general public as well as other sectors. Technology transfer can be achieved
through this proposal, and gaining commitment and buy-in from the company is
crucial. Highlighting the reductions achieved has a twofold goal: promote the
company as an environmentally-friendly organization and improve its reputation.
The QRP project explained herein brings opportunity, innovation and compet-
itive advantage to the companies and institutions that decide to be on-board. The
project will improve the image of the company, even if the initial commitment is
only to achieve reduction goals or profit.
Regional integration and articulation with other sectors can be achieved through
this project, which will provide specialized services and suggest better technologies
or processes, which can be available locally. Integration and articulation will be
promoted through the Life Cycle Thinking approach, propelling local and regional
economy, and positively influencing the region involved in the project.
The implementation of the activities contained in this project guarantees the
rational use of natural resources, decreases social and environmental impacts
deriving from their utilization and impels regional economy, resulting in the
increase of life quality standards and social standards for local communities.
Additionally, the QRP project contributes to sustainable development and improve-
ment of environmental quality.
Acknowledgments The authors wish to acknowledge the support of the Institute for the Devel- opment of Paraı́ba (IDEP-PB) and of the National Council for Scientific and Technological
Development (CNPq), through project n� 475879/2013-9.
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Part II
Global Warming and Climate Change: General Issues and Challenges
Climate Change Mitigation Measures and Prospects
Chapter 7
Group Comparison, Trends and Cluster Analysis to Understand Historical Precipitation
Raphael Abrah~ao
Introduction
In recent years, much research has been carried out regarding climate change and its
consequences. The current concentrations of greenhouse gases are already a con-
cern and several scientists predict that the average temperature of the planet can
increase between 1.8 and 4.0 �C until the end of this century, which may cause dramatic environmental impacts (IPCC 2007; Malhi et al. 2009; Davidson
et al. 2012). According to the IPCC (2014), warming of the climate system is
unequivocal, and since the 1950s, many of the observed changes are unprecedented
over decades to millennia.
This scenario of increasing temperatures is only one facet of climate change.
Shifting in precipitation patterns (frequency and intensity) is another important
change that needs to be deeper understood. Such changes in climate may impact
ecosystems, trigger plagues and epidemics, threaten urban infrastructure, water and
energy supply, as well as agriculture, especially in regions where shortage of water
is already an issue (Knapp et al. 2002; Disch et al. 2012; Davidson et al. 2012;
Durack et al. 2012; IPCC 2014).
Understanding the nature and extent of these impacts is crucial for the determi-
nation of adaptation policies towards avoiding or diminishing the negative impacts
of climate change, as well as taking advantage of the positive impacts. However, to
understand the potential impacts and plan adequately, we first need to understand
how climate is changing.
R. Abrah~ao (*) Department of Renewable Energy Engineering (DEER), Center of Alternative and Renewable
Energy (CEAR), Federal University of Paraı́ba (UFPB), Caixa Postal 5115, Cidade
Universitária, Jo~ao Pessoa 58051-970, PB, Brazil e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_7
77
Climate models are useful tools to project climate change scenarios. Although
nowadays they are very comprehensive and can take into consideration several
parameters and relationships, there is still a high level of uncertainty in the studies
using these projections, especially for precipitation (Von Storch et al. 1993;
Grillakis et al. 2011; Zhang et al. 2011).
In addition, in many parts of the world, relatively long historical climate datasets
are available and little (and in many cases, none) use of this information is made
towards a better understanding of climate change impacts. The high costs associ-
ated with installation and maintenance of these monitoring stations throughout
decades could be better spent and deeper information about the dynamics of
regional and local climate change could be obtained from the datasets.
A number of studies used historical data, confirming that climate change is not
something that will happen in the future but is a current reality (Magnuson
et al. 1997; Vincent and Gullett 1999; Alexander et al. 2006; Wang and Ding
2006). These studies are good examples of how deeper information about climate
change can be obtained from real historical data. Furthermore, confidence in the
projections from climate models is higher for temperature than for other climate
elements such as precipitation; confidence is also higher at global and continental
scales than for regional and local scales (AMS 2012).
Thus, can historical data provide sufficient information about climate change in
order to understand the potential impacts and develop adaptation strategies? And,
more importantly, are the methodologies effective to provide this information? The
objective of this paper is to assess the use of cluster analysis, together with other
more traditional methodologies such as group comparison and trend analysis, to
expand knowledge about climate change on local and regional scales from histor-
ical data of precipitation.
Methodology
The methodology was based on three different approaches: (1) a general assessment
of annual totals with comparison of past and recent periods, (2) trend analysis, and
(3) the application of cluster analysis to analyse monthly and seasonal changes. The
intention was not compare these approaches, but evidence the importance of using
different approaches, instead of a single one, to assess climate changes that will
affect the water cycle and others factors regionally.
Monthly rainfall and snowfall data were obtained from the Sudbury airport
station (Canada), from January 1956 to December 2010 (55 complete years).
Data was obtained from Environment Canada (Canadian National Climate Data
and Information Archive, www.climate.weatheroffice.gc.ca) and it was subjected to
a process of quality control before becoming available. The city of Sudbury is part
of the province of Ontario and is located at 46�290N and 81�000W. The climate of the area is classified as humid continental (Dfb according to the K€oppen-Geiger classification).
78 R. Abrah~ao
The 20 first years (1956–1975) and 20 last years of the dataset (1991–2010) were
selected for evaluation of annual changes. Since the annual data presented normal
distribution, the t-test was applied to compare both periods. The t-test performed a
comparison of means to determine whether the means of the two periods where
significantly different. A probability of less than a 5% error (p< 0.05) was considered.
The Mann-Kendall test was used for trend analysis. A non-parametric test was
selected because the monthly and seasonal data did not present normal distribution
(Mann 1945; Kendall 1975). The trend estimation was performed applying the
Sen’s slope calculation (Sen 1968) and error probabilities between 0.1% and 10% were used.
Cluster analysis was carried out to analyze changes in the distribution of rainfall
and snowfall throughout the year. The purpose was to place the objects (month-year
combinations) into groups (or clusters) suggested by the data, not defined a priori.
Thus, data was organized monthly, and each month was considered as a different
variable, thereby obtaining data from 660 month-year combinations (12 months in
55 years). Years with similar precipitation distribution were placed into the same
cluster. The cluster analysis was performed by standardizing the variables and using
the Euclidean square distance as similarity measure (Hair et al. 1998). Due to its
simplicity and computational efficiency, the Ward method was used to obtain
hierarchical clustering (Hair et al. 1998).
In hierarchical cluster techniques, the objects are progressively aggregated until
they form a single cluster. Each object begins in a cluster itself and then the closest
clusters are merged to form a new cluster that replaces the two previous clusters.
Merging of the two closest clusters is repeated until only one cluster is left (Ramos
2001; Munoz-Dı́az and Rodrigo 2004). In some studies, similar results were
obtained by applying cluster techniques and principal component analysis
(Munoz-Dı́az and Rodrigo 2004; Yin et al. 2011).
The “median year” of the objects (month-year combinations) was used as an
indicator to compare recent and past periods. All statistical procedures were carried
out with Statgraphics 15 and Makesens 1.0 softwares.
Results and Discussion
Changes in Annual Rainfall and Snowfall
The dataset suggests that annual rainfall is increasing in the Sudbury site. Even with
the expected variability of rainfall between years, an increasing trend during recent
years could be observed (Fig. 7.1). Significant statistical differences (p< 0.05) were observed when comparing the 1956–1975 period versus the 1991–2010 period,
with average values of 608 and 680 mm/year respectively, which represents a 12%
increase in rainfall.
7 Group Comparison, Trends and Cluster Analysis to Understand Historical. . . 79
Regarding snowfall, the trend was not that clear. Although a slight increase in
snowfall could be observed (Fig. 7.2), there was no statistically significant differ-
ence between the means of the two periods (p< 0.05).
Changes in Monthly and Seasonal Distribution of Rainfall and Snowfall—Trend Analysis
Trend analysis also detected the annual changes presented in the previous section.
A significant increasing trend in rainfall (p< 0.10) was quantified by the Sen’s slope through a rate of 1.74 mm/year and no significant trend was detected for
annual snowfall (Table 7.1).
Fig. 7.1 Annual rainfall
Fig. 7.2 Snowfall in the Sudbury site during the 1956–2010 period
80 R. Abrah~ao
The trend analysis could be considered more comprehensive for evaluation of
annual changes than the t-test group comparison, because all years of the dataset are
included in the analysis and not only the 20 first and 20 last years. However, the
expected variability of precipitation could hinder the detection of trends, which was
not the case for the Sudbury site during the 1956–2010 period.
Changes in the distribution of precipitation throughout the year were also noted
during the studied period. It means that the annual increasing trends observed for
rainfall volumes were not uniform over the year. March and May presented
significant (p< 0.10) positive trends with Sen’s slopes of 0.28 and 0.58 mm/year respectively. October presented a more significant (p< 0.05) positive trend and a Sen’s slope of 0.49 mm/year. The remaining months did not present significant trends.
Seasonally, significant increasing trends were observed in winter (p< 0.10) and spring (p< 0.05) through Sen’s slopes of 0.32 and 1.04 mm/year respectively. The Mann-Kendall test did not detect significant trends in rainfall during summer and
fall. Regarding snowfall, no significant trends were detected for any month or
season.
Table 7.1 Rainfall and snowfall trends detected by
the Mann-Kendall test and
quantified by the Sen’s slope for the Sudbury site during the
1956–2010 period
Period
Rainfall
(mm/year)
Snowfall
(cm/year)
January 0.05 ns 0.20 ns
February – 0.17 ns
March 0.28a �0.07 ns April 0.22 ns 0.07 ns
May 0.58a –
June �0.13 ns – July 0.13 ns –
August 0.36 ns –
September �0.18 ns – October 0.49b –
November 0.15 ns �0.10 ns December 0.07 ns 0.17 ns
Winter 0.32a 0.67 ns
Spring 1.04b 0.06 ns
Summer 0.08 ns –
Fall 0.35 ns �0.15 ns Annual 1.74a 0.60 ns
ns non significant ap< 0.10 bp< 0.05 cp< 0.01 dp< 0.001
7 Group Comparison, Trends and Cluster Analysis to Understand Historical. . . 81
Changes in Monthly and Seasonal Distribution of Rainfall and Snowfall—Cluster Analysis
For the monthly rainfall data from the Sudbury site, the cluster analysis applied
separated the 55 years into three clusters (Table 7.2). Cluster 1 consisted of years
1956, 1959, 1960, 1961, 1962, 1964, 1970, 1972, 1976, 1978, 1987, 1992, 1997 and
2010. Cluster 2 consisted of years 1957, 1958, 1963, 1965, 1966, 1967, 1968, 1969,
1971, 1973, 1974, 1975, 1977, 1979, 1981, 1982, 1984, 1985, 1986, 1989, 1990,
1991, 1994, 1998, 1999, 2000, 2001, 2002, 2003, 2004, 2005, 2006, 2007 and 2009.
Finally, cluster 3 included years 1980, 1983, 1988, 1993, 1995, 1996 and 2008.
Each cluster included similar years regarding precipitation distribution over the
year. It is important to note that the median year in Table 7.2 does not necessarily
have to be included in the years within the cluster, since it is just an indicator for
comparison between clusters representative of past and recent periods.
As the interannual variability of rainfall is often high, there were past and recent
years within the three clusters. However, cluster 1 presented a greater concentration
of earlier years (median year¼ 1971), while cluster 2 (median year¼ 1985) and cluster 3 (median year¼ 1993) gradually corresponded to more recent years.
The separation into three clusters highlighted the temporal increase in annual
rainfall, with cluster 1 adding up to 611 mm/year; cluster 2 to 656 mm/year and
cluster 3, representing the most recent years, adding up to 701 mm/year. These
results of increased rainfall over time had been indicated by the methods applied
previously, however, through cluster analysis, changes in the seasonal distribution
of rainfall could also be observed, with little interference from the interannual
variability of the data. Thereby, the most interesting result from the cluster analysis
was the observation of changes in the distribution of rainfall throughout the year.
Increases were observed in most months, but at different scales (Table 7.2).
Decreases were observed during the months of June, July and September despite
the annual increases. Since these months belong to the rainy period of the site
(May–October), the shift may have consequences on local water and agricultural
management.
Observing these changes through the seasons, it is easier to verify the gradual
influence of climate changes on the annual variability of rainfall (Fig. 7.3). Changes
were very important during winter and spring, with increases of 309% and 65%
respectively, when comparing clusters 1 and 3. During the fall, increases were not
very important (6%), while in summer, which is the most important rainy season in
Sudbury, the 15% reduction represented a decrease of 41 mm in rainfall.
For snowfall, cluster analysis separated the 55 years into two clusters. Cluster
1 comprised years 1956, 1957, 1958, 1959, 1960, 1961, 1963, 1964, 1966, 1968,
1969, 1970, 1973, 1977, 1980, 1984, 1986, 1987, 1991, 1993, 1994, 1995, 1998,
2003, 2005, 2007 and 2010, and cluster 2 consisted of years 1962, 1965, 1967,
1971, 1972, 1974, 1975, 1976, 1978, 1979, 1981, 1982, 1983, 1985, 1988, 1989,
1990, 1992, 1996, 1997, 1999, 2000, 2001, 2002, 2004, 2006, 2008 and 2009. The
median years of the two clusters were close (1977 and 1987), implying in that the
82 R. Abrah~ao
T a b le
7 .2
T h re e cl u st er s d is cr im
in at ed
b y th e cl u st er
an al y si s b as ed
o n m o n th ly
ra in fa ll d at a in
S u d b u ry
si te
fr o m
1 9 5 6 to
2 0 1 0
C lu st er
M ed ia n
Y ea r
Ja n u ar y
(m m )
F eb ru ar y
(m m )
M ar ch
(m m )
A p ri l
(m m )
M ay
(m m )
Ju n e
(m m )
Ju ly
(m m )
A u g u st
(m m )
S ep te m b er
(m m )
O ct o b er
(m m )
N o v em
b er
(m m )
D ec em
b er
(m m )
S u m
(m m )
1 1 9 7 1
6 0
1 1
3 7
6 7
8 6
8 6
9 5
1 2 9
5 1
3 5
7 6 1 1
2 1 9 8 5
7 9
3 0
4 7
7 2
8 6
7 9
7 5
9 4
8 1
5 7
1 9
6 5 6
3 1 9 9 3
3 6
5 2 5
6 9
9 7
5 0
7 0
1 0 6
1 0 4
8 2
4 1
1 6
7 0 1
M ed ia n y ea r an d an n u al
su m
co rr es p o n d en t o f ea ch
cl u st er
ar e al so
p ro v id ed
7 Group Comparison, Trends and Cluster Analysis to Understand Historical. . . 83
trends of change in snowfall distribution over the year were not as clear as for
rainfall.
Nevertheless, changes in snowfall distribution could be observed for December,
January and February, the 3 months of higher snowfall values in Sudbury. Although
the annual sum of snowfall did not change significantly, more recent years
presented lower values in December (13%), and higher values in January (38%)
and especially in February (116%), when values more than doubled (Fig. 7.4).
The application of cluster and trend analysis evidenced that the increasing
annual trends for rainfall volumes in the Sudbury area were not uniform over the
year. This annual increase was mainly in winter and spring. Decreases in summer
rainfall were detected only through cluster analysis. According to cluster analysis,
although years are currently more humid, summers are becoming drier in the
location. Previous studies have detected and/or projected changes in rainfall in
Sudbury and nearby sites (Magnuson et al. 1997; OCCIAR 2010; IEESC 2012;
Charron 2014), however, the changes in seasonality were not considered in depth.
Regarding snow precipitation, while group comparison and trend analysis did
not indicate any significant trends, cluster analysis showed clear changes for the
months of greatest snowfall (December, January and February). Reductions in
December and increases in January and February were observed. This means that
the climate of the site is changing towards later winters regarding snowfall, which
may also be related to changes in other variables (e.g., temperature).
Although it was not the focus of this study, changes in extreme events should
also be investigated. According to Folland et al. (2002), in regions where annual
rainfall has increased it is very likely that there have been even more pronounced
increases in heavy and extreme rainfall events. And the converse is also true.
Fig. 7.3 Trends of changes in rainfall distribution throughout the seasons in the Sudbury site from 1956 to 2010, represented by the three clusters discriminated by cluster analysis
84 R. Abrah~ao
In some regions, heavy and extreme precipitation events have increased, despite the
fact that total precipitation has decreased or remained constant.
Conclusions
The methodologies used in this study demonstrated that the detection of annual
changes is only the initial step in a more comprehensive understanding of climate
change, which also includes complex seasonal and monthly changes. In many areas
of the world, the absence of detected changes or significant trends from annual data
may give a false idea of the absence of climate change in the location (e.g., snowfall
in the site of this study). However, the results presented herein indicate that the
inclusion of simple methods, such as cluster analysis, can contribute to a better
understanding of seasonal and monthly climate changes.
Acknowledgement This work was supported by the Ontario Centre for Climate Impacts and Adaptation Resources (OCCIAR) and Environment Canada.
Fig. 7.4 Trends of changes in snowfall distribution
throughout December,
January and February in the
Sudbury site from 1956 to
2010, represented by the
two clusters discriminated
by cluster analysis
7 Group Comparison, Trends and Cluster Analysis to Understand Historical. . . 85
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Charron, I. (2014). A guidebook on climate scenarios: Using climate information to guide adaptation research and decisions. Montreal: Ouranos.
Davidson, E. A., de Araújo, A. C., Artaxo, P., Balch, J. K., Brown, I. F., Bustamante, M. C.,
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IEESC, Institute for Energy, Environment and Sustainable Communities. (2012). Producing high- resolution (25 km� 25 km) probabilistic climate change projections over Ontario using UK PRECIS. Regina: University of Regina.
IPCC, Intergovernmental Panel on Climate Change. (2007). Climate change 2007: The physical science basis. Contribution of working group I to the fourth assessment report of the Inter- governmental Panel on Climate Change. Cambridge/New York: Cambridge University Press.
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7 Group Comparison, Trends and Cluster Analysis to Understand Historical. . . 87
Chapter 8
Ground Response to Global Warming
Mohamad Kharseh and Mohammed Al-Khawaja
Introduction
Over the period 1880–1985 the mean global temperature increased by 0.5–0.7 �C (Hansen and Lebedeff 1987), bearing in mind that the warming rate at high latitudes
of the northern hemisphere during recent past decades was greater (Lachenbruch
and Marshall 1986; Peterson et al. 2009). Certainly, the change in surface air
temperature (SAT) is more than the change of mean global temperature. A com-
parison of the averages anomalies of SAT between 1880–1890 and 2000–2010
shows that the SAT has increased 1.2 �C above the preindustrial level (NCDC and NOAA 2010). Figure 8.1 and the meteorological data presented by Hansen and
Lebedeff (1987) clearly show that the recorded meteorological data of air temper-
ature varies greatly over time, which might lead to a miscalculation of the warming
level (Lachenbruch and Marshall 1986). In other words, the warming that was
calculated above might be different if different periods were compared.
The analysis of borehole temperature depth profile (BTDP) has therefore
recently become an accepted method for inferring recent climatic changes, rather
than measuring the SAT (Deming 1995; Ferguson 2006; Goto 2010; Harris and
Chapman 1997). Although in some cases, e.g. in North America, it was shown that
warming estimated from the analysis of BTDP is consistent with warming esti-
mated from the analysis of meteorological data over the period 1880–1987 (Hansen
and Lebedeff 1987).
Measurements of BTDP evidently show that there are temperature deviations
from the linear steady-state ground temperature in the upper sections of boreholes
M. Kharseh (*) • M. Al-Khawaja Mechanical & Industrial Engineering Department, Qatar University,
Al Dafna, Jamaa Street, Doha, Qatar
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_8
89
(Lachenbruch and Marshall 1986; Goto 2010; Harris and Chapman 1997; Guillou-
Frottier et al. 1998).
This deviation in temperature might be theoretically attributed to many different
sources (Harris and Chapman 1997):
• There is a disturbance in the energy balance at the Earth’s surface on a multi- decade scale. This disturbance might be interpreted by a continental-scale
change in the SAT, i.e. recent warming of the mean annual SAT (Deming
1995; Harris and Chapman 1997).
• Change in land use such as more buildings (Lachenbruch and Marshall 1986;
Ferguson 2006). Yoshikawa et al. attributed this temperature deviation to
increase in albedo and reduction of the leaf area involved in transpiration
following deforestation or wildfire (Yoshikawa et al. 2002). It was shown that
a recent change in vegetation cover and increased surface temperature over the
past century result in a similar shape of BTDP (Nitoiu and Beltrami 2005).
• Changes in thermal conductivity might lead to this temperature departure, that
is, “a systematic upward increase in conductivity might cause a systematic
upward decrease in gradient and simulate the transient warming” (Lachenbruch
and Marshall 1986; Deming 1995).
Thus, using the borehole temperature to analyze the warming is not always easy
(Deming 1995). However, in general, the departure of BTDP from the steady state
line is considered a direct consequence of a change in SAT (Lachenbruch and
Marshall 1986; Deming 1995). Moreover, the effects of other non-climatic sources
(e.g. change in land use, variability of thermal conductivity, groundwater move-
ment and so forth) have been shown to be negligible at the noise level of data
(Chisholm and Chapman 1992).
Fig. 8.1 Global mean surface air temperature anomalies (NCDC and NOAA 2010)
90 M. Kharseh and M. Al-Khawaja
It is important to mention that there are temperature measurements of boreholes
that show recent cooling trends at the surface which started in the 1970s
(Lachenbruch and Marshall 1986; Deming 1995).
However, measurements of borehole temperature generally show smooth
enough curves to permit us to approximate it to a mathematical formula
(Lachenbruch and Marshall 1986). The current study mainly aims to derive an
equation that expresses ground temperature deviation from the steady-state line as a
result of warming at ground surface. The derived equation was used to determine
the average change of ground temperature over a certain depth and therefore the
heat retained by a column of earth during the warming period. This average change
of ground temperature is of great importance in the borehole system.
Methodology
Dominating Equation
In order to obtain an equation that expresses the ground temperature change from its
linear steady-state profile, the heat conduction equation needs to be solved. For this
purpose the transient ground temperature θ(z,t) at depth z and time t is given as follows:
θ z; tð Þ ¼ Ts þ γ � zþ T z; tð Þ ð8:1Þ
where Ts is the air temperature at the surface level; γ is the temperature gradient due to geothermal heat flux; z is the depth below the ground surface; t is the time
elapsed since the warming started; and T(z,t) is ground temperature deviation from
the steady-state profile, i.e. the response of the ground to recent warming of the
mean annual surface temperature.
It is worth mentioning that in current study and for the sake of simplicity some
assumptions were made as follows. It is well established that urban areas can be
3–6 �C warmer than their surrounding rural areas (Kolokotroni 2009; EPA 2013- 01-15) . Certainly, such local temperature changes affect the ground temperature.
However, due to the insulating effect of the ground itself (i.e., low thermal
conductivity and big heat capacity), it was shown that the effect of change in land
use will only extend 50 m beyond the affected area at the surface (Ferguson 2006).
In the shallow subsurface, the transfer of heat can have an advection component
owing to the transfer of water between the different compartments, but this com-
ponent might be compensated by phase changes (evaporation). In addition the
thermal diffusivity of the ground is assumed to be constant and evaluated at the
average over value (Guillou-Frottier et al. 1998; Chisholm and Chapman 1992).
In nutshell, the effect of lateral heat flow and the advection component of heat
transfer are neglected and one dimensional heat flow is considered. This
8 Ground Response to Global Warming 91
simplification of the analysis provides insight into time scales of ground tempera-
ture deviation. Thus, in the case with absence of any internal heat generation, the
governing equation is:
∂θ z; tð Þ ∂t
¼ α∂ 2θ z; tð Þ ∂z2
ð8:2Þ
Substitution Eq. (8.1) in Eq. (8.2) yields
∂T z; tð Þ ∂t
¼ α∂ 2 T z; tð Þ ∂z2
ð8:3Þ
This way, any factor that might affect thermal exchanges at the air-ground interface
was removed. Thus the subsequent analysis will lead to the best estimate of ground
temperature deviation (Harris and Chapman 1997).
Another important assumption is that the ground surface temperature has line-
arly changed over time τ (i.e. it was assumed that the warming began τ years ago), see Eq. (8.5) (Lachenbruch and Marshall 1986; Winterberg 1991). Indeed, assum-
ing nonlinear form of surface warming leads to a more complex solution.
Reference Depth
Because the ground has a relatively low thermal diffusivity, changes in temperature
at the Earth’s surface propagate slowly into the ground and diminish with depth. The reference depth (hereafter referred to as H) is defined as the depth beyond
which, for practical purposes, the effect of warming at surface becomes difficult to
observe. This depth depends on both the time elapsed since the start of warming at
the surface and thermal diffusivity of the ground. In the current study, Laplace
transformation technique was used to give an acceptable approximation to the
reference depth, see Eq. (8.4):
H ¼ π � ffiffiffiffiffiffiffiffiα � tp ð8:4Þ Note that the temperature change at the depth given by above equation is less than
2.6% of the surface temperature change. The measurements made by Lachenbruch
and Marshall (1986), Goto (2010), Harris and Chapman (1997), Williams and Gold
(1976) show no change in ground temperature beyond the depth given by Eq. (8.4).
It is good to mention that, Lachenbruch and Marshall defined this depth as the depth
beneath where the changes in the ground temperature becomes <5% of the surface temperature change. Consequently, the reference depth in their study is H¼ 2.07 √α.t. However, in this study Eq. (8.4) will be used, and it can be shown that it is more accurate. For alternative approximations it is recommended to consult Chap. 9
given by Özişik (1980).
92 M. Kharseh and M. Al-Khawaja
This way, the boundary conditions for Eq. (8.3):
T 0; tð Þ ¼ δ τ � t ¼ ε � t ð8:5Þ
T H; tð Þ ¼ 0 ð8:6Þ
While the initial condition is
T z; 0ð Þ ¼ 0 ð8:7Þ
where τ is the time during which the surface temperature increased by δ �C; ε¼ δ/τ is the warming rate; and H is the reference depth (Eq. 8.4).
Results
To obtain the equation that gives the change in ground temperature due to linear
increase of surface air temperature, Eq. (8.3) that is subject to the boundary
conditions and initial condition are given by Eqs. (8.5), (8.6) and (8.7), respectively.
Using Fourier’s theory technique for solving partial deferential equation, the temperature change in ground temperature is:
if z � π ffiffiffiffiffiffiffiffiα � tp then T z; tð Þ ¼ ε
α
z2
2 � z
3
6π ffiffiffiffiffiffiffiffi α � tp �
π ffiffiffiffiffiffiffiffi α � tp � z 3
� � þ ε � t � 1� z
π ffiffiffiffiffiffiffiffi α � tp þ
2
π
X1 n¼1
e�n 2 � sin n � zffiffiffiffiffiffiffiffi
α � tp � � n3
0 BB@
1 CCA
if z > π ffiffiffiffiffiffiffiffi α � tp then
T z; tð Þ ¼ 0 ð8:8Þ
This equation represents the ground temperature deviation at depth z and time t
elapsed since the start of linear warming at the surface.
Figure 8.2 illustrates some of the partial sums (containing only a finite number of
terms) for T(z,t¼ τ), Eq. (8.8), where terms up to n¼ 4 were considered. The same ground thermal properties assumed by (Lachenbruch and Marshall 1986) were used
in the current example, i.e. thermal conductivity λ and thermal diffusivity α are 2.1 W/m K, and 1.10–6 m2/s, respectively. The ground surface temperature was
linearly increased to δ¼ 2.5 �C over time τ¼ 130 years. For other assumptions, the curve can be easily adjusted using Eq. (8.8).
To examine the accuracy of the derived equation, Eq. (21) given by (Winterberg
1991) and Eq. (10) given by (Lachenbruch and Marshall 1986) (for n¼ 2) were also illustrated in Fig. 8.2 using the same assumptions made above. As it is shown, the
8 Ground Response to Global Warming 93
suggested equation (i.e., Eq. 8.8 in the current study) is consistent with the solutions
proposed in other studies using other techniques.
Application of Derived Equation
The total heat absorption Q as a result of increased air temperature is about the same
for all forms of warming curve at the surface (linear, step, accelerating as the square
of time and so forth) (Lachenbruch and Marshall 1986). The knowledge of this heat
is of significant importance in analyzing global warming’s sources (Nordell 2003). The heat retained by a column of earth surface due to increasing the air can now be
Fig. 8.2 Comparison between our suggested equation and equations derived by Lachenbruch and Marshall (1986) and Winterberg (1991) of the response of the ground to recent warming of the
mean annual surface temperature of 2.5 �C started in 1880. The following assumptions were made: Ground thermal conductivity λ¼ 2.1 W/m K, thermal diffusivity α¼ 1.10–6 m2/s and warming rate of ambient air ε¼ 0.0192 �C/year
94 M. Kharseh and M. Al-Khawaja
calculated by integrating the result of Eq. (8.8) and volumetric heat capacity of the
ground during the warming event (i.e., t)
Q tð Þ ¼ ðH 0
C � T z; tð Þdz ¼ K � C � ε � t � ffiffiffiffiffiffiffiffiα � tp ð8:9Þ where K is a constant (K¼ 0.74727) given by Eq. (8.10); C is volumetric heat capacity of the ground that is in the range of 2 MJ/m3 K.
K ¼ π 2 � π
3
24 þ 4 π
X1 n¼0
e� 2nþ1ð Þ 2
2nþ 1ð Þ4 � π
2 � π
3
24 þ 4 π � e ð8:10Þ
Thus, for the same warming rate and thermal properties assumed above, the total
heat absorption by 1 m2 of ground is 251 MJ/m2 (about 0.06 W/m2).
Calculating the mean change in ground temperature over a particular depth,
say L, (ΔTm(L,t)) is of great importance for ground source heat pump system design (Kharseh et al. 2011; Kharseh and Altorkmany 2012; Fontaine et al. 2011) .
This mean change ΔTm(L,t) is given by integrating Eq. (8.8) from zero to the concerned depth (L) and dividing the result by L as follows:
if L � π ffiffiffiffiffiffiffiffiα � tp ΔTm L; tð Þ ¼ ε
6α L2 � L
3
4π � ffiffiffiffiffiffiffiffiα � tp � π ffiffiffiffiffiffiffiffi α � tp � L
� � þ
þ ε � t � 1� L 2π � ffiffiffiffiffiffiffiffiα � tp � 4 �
ffiffiffiffiffiffiffiffi α � tp
π � L X1 n¼1
e�n 2 � sin 2 n � L
2 � ffiffiffiffiffiffiffiffiα � tp � � n4
0 BB@
1 CCA
if L > π ffiffiffiffiffiffiffiffi α � tp
ΔTm L; tð Þ ¼ ε � π � t � ffiffiffiffiffiffiffiffi α � tp
2L 1� π
2
12 þ 8 π2
X1 n¼0
e� 2nþ1ð Þ 2
2nþ 1ð Þ4 !
ð8:11Þ
Conclusions
The aim of this study was to find an equation relating ground temperature change
with global warming. To achieve this goal, a heat conduction equation was solved
using Fourier’s theory. The derived equation in the current study and the equations established in other studies are in excellent agreement. The suggested equation is
more user-friendly than other equations that are published in previous publications.
Because of its simplicity, the suggested equation was used to state the mean change
8 Ground Response to Global Warming 95
in ground temperature and the heat retained by a column of earth surface due to the
increasing surface air temperature. These equations are expected to be useful in
situations where the ground temperature is of importance; e.g. design of under-
ground thermal energy storage systems, ground source heat pump, studies of
microbiological systems in the ground, plant growth, frost heave, in addition to
the understanding of the effect of global warming. Although the study is based on
large uncertainties (a fact typical of this subject), the derived equation provides
insight into time scales of ground temperature anomalies.
Acknowledgements This work was made possible by an NPRP 7-725-2-270 a grant from the Qatar National Research Fund (a member of The Qatar Foundation). The statements made herein
are solely the responsibility of the authors.
Nomenclature
C Volumetric heat capacity (J/m3 k)
H Reference depth (m)
L A certain depth that is of interest to calculate the ΔTave (m) Q(t) Heat retained by a column of earth surface due to the climatic changes
(J/m2)
t Time elapsed since start-up warming (s)
T(z,t) Ground temperature anomaly (�C) Ts Air temperature at the surface level (
�C) z Depth below ground surface (m)
α¼ λ/C Thermal diffusivity (m2/s) γ Temperature gradient due to geothermal heat flux (�C/m) δ Temperature change at the ground surface (�C) ΔTm(L,t) Average change of ground temperature over a certain depth L (�C) ε Warming rate of air (assumed to be constant over time) (�C/s) θ(z,t) The transient ground temperature at depth z and time t λ Thermal conductivity (W/m K)
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Peterson, T. C., Baringer, M. O., Thorne, P. W., Menne, M. J., Kennedy, J. J., Christy, J.,
et al. (2009). Bulletin of the American Meteorological Society, 90, S13. Williams, G. P., & Gold, L. W. (1976). Canadian Building Digest.
Winterberg, F. (1991). Detection of global warming through spatial temperature-variations below
the earth surface. Kerntechnik, 56, 143–146. Yoshikawa, K., Bolton, W. R., Romanovsky, V. E., Fukuda, M., & Hinzman, L. D. (2002).
Impacts of wildfire on the permafrost in the boreal forests of Interior Alaska. Journal of Geophysical Research-Atmospheres, 108, FFR 4-1–FFR 4-14.
8 Ground Response to Global Warming 97
Chapter 9
Specific Case: Regional Estimates of Global Climate Change: A Dynamical Downscaling Approach to Southeast Europe
Rafaella-Eleni P. Sotiropoulou, Efthimios Tagaris, Andreas Sotiropoulos, Ioannis Spanos, Panagiotis Milonas, and Antonios Michaelakis
Introduction
Climate change is a major environmental problem that will affect future weather
and will modify the meteorological data, locally. General Circulation Models
(GCMs) estimate that the global mean surface temperature change for the near
future (i.e., for the period 2046–2065 relative to 1986–2005) will likely be in the
range of 0.4–2.6 �C while globally-averaged precipitation increases with global mean surface temperature at about 1–3% �C-1 are projected. However, the mini- mum and the maximum estimated changes cover a wide range of values for all
geographical regions (IPCC 2013). For example, under the RCP4.5 experiments,
annual temperatures for northern, central, and southern Europe are estimated to be
modified in the range of �0.5 �C to 3.8 �C, 0.4 �C to 3.2 �C and 0.7 �C to 3.1 �C, respectively, while annual precipitation rates are estimated to be modified in the
R.-E.P. Sotiropoulou (*) Department of Mechanical Engineering, University of Western Macedonia, 50100 Kozani,
Greece
Environmental Research Laboratory, NCSR Demokritos, 15310 Athens, Greece
e-mail: [email protected]
E. Tagaris
Environmental Research Laboratory, NCSR Demokritos, 15310 Athens, Greece
e-mail: [email protected]
A. Sotiropoulos • I. Spanos
Environmental Engineering Consultancy, Terra Nova Ltd., 11527 Athens, Greece
e-mail: [email protected]; [email protected]
P. Milonas • A. Michaelakis
Department of Entomology and Agricultural Zoology, Benaki Phytopathological Institute,
14561 Kifisia, Greece
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_9
99
range of �5% to 17%, �6% to 9%, and �14% to 3%, respectively for the period 2046–2065 relative to 1986–2005. However, the outputs from the GCM are rela-
tively coarse for applications to regional scales. To increase their spatial resolution,
the coarse resolution data of the GCM are used as initial and boundary conditions
by a regional climate model (RCM) (dynamical downscaling). The purpose of
doing this is to add-up more detail from local topography, coastline and land
use/land cover to obtain high resolution data, with the greatest possible accuracy
for the area of interest.
During the last years there is an increasing interest related to the climate change
over Mediterranean as it is one of the most vulnerable regions of the globe given
that large climate shifts have been observed in the past (Luterbacher et al. 2006). As
a result, Mediterranean has been identified as one of the most prominent “Hot-
Spots” in future climate change projections (Giorgi 2006). It is located in a
transition zone between the arid climate of northern Africa and the wet climate of
central Europe and even a minor change in large scale climatic factors might
impose large impacts on the climatic conditions of different Mediterranean areas.
The objective of this study is to estimate the changes in temperature and
precipitation over southeast Europe in the near future at a very fine resolution
since the topography and the coastlines of the region suggest a fine scale spatial
variability of the climatic conditions (Gao and Giorgi 2008).
Methods
General Circulation Model
The NASA GISS GCM ModelE (Goddard Institute for Space Studies General
Circulation Model) (Schmidt et al. 2006) is used to simulate current and future
climate. The GISS model has been chosen for simulations since it is a state-of-
the-art and widely used global climate model. The version of the NASA GISS GCM
ModelE used here has horizontal resolution 2� � 2.5� latitude by longitude and 20 vertical layers (from surface to 0.1 hPa). The model accounts for both the
seasonal and diurnal solar cycles in its temperature calculations. It simulates the
emissions, transport, chemical transformation and deposition of several chemical
tracers. Sea surface temperatures (SST) are calculated using model-derived surface
energy fluxes and specified ocean heat transports. In the present study the IPCC-
A1B emissions scenario (IPCC 2000) is used. This scenario describes alternative
directions of technological change in the energy system suggesting balance across
all sources, where balanced is defined as not relying too heavily on one particular
energy source, on the assumption that similar improvement rates apply to all energy
supply and end-use technologies. The simulations cover the period from 1880 to
2061. The beginning of the simulations is chosen prior to significant anthropogenic
forcing and climate change, but sufficiently recent to contain observations that
100 R.-E.P. Sotiropoulou et al.
allow extensive evaluation of the model. The main perturbation to climate over the
historic period (up to 2008) is the change in atmospheric composition: primarily the
increasing concentration of greenhouse gases and aerosols. Greenhouse gas con-
centrations up to 2008 are prescribed using ice-core measurements (Schmidt
et al. 2011). For the period 2009–2061 the GHG levels are supplied from the
IPCC A1B emissions scenario (IPCC 2000).
Regional Climate Downscaling
The outputs from the GCM are relatively coarse (i.e., 2� � 2.5�) for applications to regional and local scales. The need for regional climate projections in a finer grid
size is assessed, here, using the Weather Research and Forecasting (WRF version
3.4.1) model to dynamically downscale GCM simulations. WRF is a next genera-
tion limited area, non hydrostatic, terrain following model designed to serve both
research and operational applications (http://www.wrf-model.org/index.php). The
domain covers the south—southeast Europe in 273� 161 horizontal grids of 9 km� 9 km, with 28 vertical layers (Fig. 9.1).
For the set of physics options we used the following modules: the WRF Single-
Moment 3-class scheme for microphysics, the Rapid radiative transfer model
(RRTM) for long-wave radiation, the Dudhia scheme for short-wave radiation,
the Monin-Obukhov with Carslon-Boland viscous sub-layer for surface layer
options, the five-layer thermal diffusion for land surface options, the Yonsei
University scheme for the planetary boundary layer and the Kain-Fritsch scheme
for the cumulus cloud option. Due to the time needed for the downscaling procedure
meteorological conditions are simulated for five current (i.e., 2008–2012) and five
future (i.e., 2058–2062) years.
151
136
121
106
91
76
61
46
31
16
1 46 91 136 181 226
1
Fig. 9.1 Modeling domain
9 Specific Case: Regional Estimates of Global Climate Change: A Dynamical. . . 101
Results and Discussion
The temperature trend suggests an overall increase in the future, as a result of the
reduction of the low temperatures and the increase of the high temperatures for all
seasons (Table 9.1). A reduction in the number of days for which the daily average
temperature is below 10 �C for both winter and spring is estimated, with a consequent increase in the number of days with daily average temperature above
10 �C. These changes suggest milder winters and warmer springs in the future. During summer and autumn, a reduction is estimated in the number of days for
which the daily average temperature is below 20 �C, leading to an increase in the number of days above 20 �C. The number of days with daily average temperature above 30 �C is estimated to be ten times higher in the future summers and eight times higher in the future springs. Daily average temperatures above 30 �C start to appear in the future autumns too. What is interesting to point out here is that, the
increase in the number of days characterized by high temperatures during future
springs and autumns suggests an extension of the future summer period beyond the
traditional summer months.
Analysis of the spatial distribution plots suggests that annual average tempera-
ture is estimated to be higher in the future all over the domain (Fig. 9.2), while
increases in the range of 1.0–1.5� cover the major part of it. A maximum increase of up to 2.0� is estimated in the eastern and southeastern parts of the domain, while a minimum increase in the range of 0.5–1.0� is estimated in the western and south- western parts of the domain, as well as in the eastern Mediterranean Sea. During
winter, an increase up to 1.5� is estimated in the Tyrrhenian Sea, most of Italy, central Mediterranean Sea, Adriatic Sea, Ionian Sea and the western part of the
Balkan Peninsula; a smaller increase of up to 1.0� is estimated in north Balkan Peninsula, north Italy and the Ligurian and Balearic Seas. Central Greece, the
Aegean Sea and the eastern Mediterranean face temperature increases in the
order of 0.5�. The maximum increase is simulated in the greater Venice area (i.e., up to 2.0�). During spring, an increase of up to 1.0� is estimated in the major part of the domain. A higher increase (i.e., up to 1.5�) is found over the east land of the domain, central Mediterranean, north Italy and at the central and north Greece
while a milder increase (i.e., up to 0.5�) is found locally over Mediterranean Sea. During summer, an increase of up to 2.0� is estimated in Balkan Peninsula, most of Italy, southeastern France and central Mediterranean Sea, while temperature
increases up to 2.5� are found over the east land of the domain. For the rest of the domain an increase of up to 1.5� is found. During autumn a gradual increase from 0.5 to 3� from the west to the east, respectively, is found. An increase of up to 2.5� is estimated in a major part of Greece and Bulgaria, while the rest part of the Balkan
Peninsula is estimated to be warmer more than 2.0�. Temperature change over Italy is found to cover a range between 0.5 to 2.0�.
Precipitation trend suggests an increase of the dry days (i.e., precipitation rate
less than 1 mm/day) and a decrease of the days with precipitation rate in the range
of 1–10 mm/day for future winter, spring and autumn (Table 9.2) over the domain.
102 R.-E.P. Sotiropoulou et al.
T a b le
9 .1
N u m b er
o f d ay s p er
te m p er at u re
ra n g e o f th e d ai ly
av er ag e te m p er at u re
fo r cu rr en t an d fu tu re
se as o n s (%
)
W in te r
S p ri n g
S u m m er
A u tu m n
C u rr en t
F u tu re
C u rr en t
F u tu re
C u rr en t
F u tu re
C u rr en t
F u tu re
T em
p er at u re
ra n g es
N u m b er
o f d ay s (%
)
T < 0
� C 1 8 .4 2 7
1 5 .6 7
4 .1 6 9
2 .9 0 9
0 .0 3 8
0 .0 1 4
5 .7 2 1
1 .8 7 4
0 � C
< T < 1 0
� C 3 9 .0 1 9
3 8 .2 1 6
2 7 .0 1 1
2 4 .5 1 2
1 .8 2 0
1 .2 8 9
2 3 .8 4 7
2 3 .7 1 5
1 0
� C < T < 2 0
� C 4 2 .5 4 7
4 5 .9 8 4
6 6 .9 9 7
6 8 .5 6 7
3 6 .3 7 2
2 3 .4 4 8
4 6 .5 9 0
4 4 .9 5 8
2 0
� C < T < 3 0
� C 0 .0 0 7
0 .1 3 0
1 .8 1 7
3 .9 6 6
6 1 .7 3 2
7 4 .8 1 8
2 3 .8 4 2
2 9 .4 3 1
T > 3 0
� C 0 .0 0 0
0 .0 0 0
0 .0 0 6
0 .0 4 6
0 .0 3 9
0 .4 3 1
0 .0 0 0
0 .0 2 2
9 Specific Case: Regional Estimates of Global Climate Change: A Dynamical. . . 103
The changes are much higher during winter compared to spring and autumn. More
days with precipitation rates in the range of 10–200 mm/day are estimated for future
winters and less for future springs. Fewer days with precipitation rates in the range
of 10 mm/day up to 100 mm/day are estimated for future autumns, while a small
increase is found for precipitation rates in the range of 100–200 mm/day. Future
summer is estimated to be slightly wetter than the present; however around 90% of
the days are dry. Extreme precipitation rates (i.e., greater than 200 mm/day) are
more frequent during all future seasons; especially for future winter and spring, a
doubling in the number of days characterised by extreme rates is fund.
Analysis of the spatial distribution plots, suggests that precipitation change is
very location dependent, presenting a mixed trend. Given that, the fine resolution
151 136 121 106 91 76 61 46 31 16 1
1 46
Winter Spring
Summer Autumn
Annual
91 136 181 226 1 46 91 136 181 226
1 46 91 136 181 226
1 46 91 136 181 226
3.0
2.5
2.0
1.5K
1.0
0.5
0.0
1 46 91 136 181 226
151 136 121 106 91 76 61 46 31 16 1
151 136 121 106 91 76 61 46 31 16 1
151 136 121 106 91 76 61 46 31 16 1
151 136 121 106 91 76 61 46 31 16 1
Fig. 9.2 Seasonal and annual temperature change between future and current years
104 R.-E.P. Sotiropoulou et al.
T a b le
9 .2
N u m b er
o f d ay s p er
p re ci p it at io n ra n g e o f th e d ai ly
av er ag e p re ci p it at io n fo r cu rr en t an d fu tu re
se as o n s (%
)
W in te r
S p ri n g
S u m m er
A u tu m n
C u rr en t
F u tu re
C u rr en t
F u tu re
C u rr en t
F u tu re
C u rr en t
F u tu re
P re ci p it at io n ra n g es
N u m b er
o f d ay s (%
)
R < 1 m m /d ay
7 2 .2 3 9
7 4 .0 0 9
8 3 .6 3 3
8 4 .2 3 3
8 9 .6 4 3
8 9 .0 6 1
7 7 .5 8 7
7 8 .4 7 8
1 m m /d ay
< R < 1 0 m m /d ay
2 1 .9 2 4
2 0 .0 4 0
1 2 .7 5 7
1 2 .2 6 7
6 .9 0 4
7 .2 0 0
1 6 .0 6 0
1 5 .3 9 9
1 0 m m /d ay
< R < 1 0 0 m m /d ay
5 .7 7 1
5 .8 5 8
3 .5 2 1
3 .4 0 6
3 .1 5 5
3 .3 6 1
6 .0 2 9
5 .7 8 8
1 0 0 m m /d ay
< R < 2 0 0 m m /d ay
0 .0 6 1
0 .0 8 3
0 .0 7 5
0 .0 6 9
0 .2 2 9
0 .2 9 0
0 .2 6 4
0 .2 6 6
R > 2 0 0 m m /d ay
0 .0 0 5
0 .0 1 1
0 .0 1 4
0 .0 2 5
0 .0 6 9
0 .0 8 8
0 .0 6 0
0 .0 7 0
9 Specific Case: Regional Estimates of Global Climate Change: A Dynamical. . . 105
grid size used in our analysis (i.e., 9 km) provides a detailed insight of the localised
precipitation changes (e.g., over islands) happening in the future (Fig. 9.3).
Annual precipitation is estimated to be lower up to 40% in the major part of the
southeast land (i.e., Balkan Peninsula and Turkey) and the west part of the domain,
while an increase of up to 60% is found over central Mediterranean, northern Italy
and the central European countries belonging to the domain. A higher increase is
simulated at the south of the domain. Seasonally, various changes take place.
During winter a decrease of more than 20% is estimated over the land at the
southeast and the north parts of the domain. A decrease is also found over the
Balkan Peninsula, except for central Greece. Precipitation is estimated to increase
over most of Italy. High precipitation increase (i.e., more than 100%) is found over
northern Italy and Sicily. Precipitation increase is dominant over sea also (i.e.,
central Mediterranean and Aegean Sea), however, a decrease is found at the east
and the west Mediterranean regions of the domain. During spring, an increase at the
154 137 120 103
86 69 52 35 18
1
1 46 91 136 181 226 1 46 91 136 181 226
1 46 91 136 181 226
1 46 91 136 181 226
1 46 91 136 181 226
154
137
120
103
86
69
52
35
18
1
154
137
120
103
86
69
52
35
18
1
154 137 120 103
86 69 52 35 18
1
154
137
120
103
86
69
52
35
18
1
120.0 100.0
80.0 60.0 40.0%
20.0 0.0
-20.0 -40.0 -60.0
Winter Spring
Summer Autumn
Annual
Fig. 9.3 Seasonal and annual precipitation change between future and current years
106 R.-E.P. Sotiropoulou et al.
northern and a decrease at the southern parts of the land of the domain dominate.
The major parts of Italy and Greece are found to face less precipitation (up to 60%)
in the future, with some local exceptions. Reduction is also found above sea except
for parts of the central Mediterranean and the Aegean Sea. During summer, higher
precipitation rates (i.e., more than 100%) are found mainly at northern Italy,
Tyrrhenian Sea, Adriatic Sea, western Greece and at the south—southeast borders
of the domain, while lower precipitation rates up to 60% are found over sea,
locally. During autumn, a decrease is found for the west part of the Mediterranean
Sea and an increase for the southern and southeast regions of the domain. An
increase is also dominant for the central European countries of our domain.
Precipitation is projected to be lower in the future over south and north Italy in
contrast to the central part of the country. A decrease of up to 60% is found over
Greece, except for the southwest part of the country.
A direct comparison of our results with the results of other researchers (e.g.,
Christensen et al., 2012; Dubrovsky et al., 2014; Garcı́a-Ruiz et al., 2011; Gao and
Giorgi, 2008) focusing in the area of our interest is not possible due to the different
spatiotemporal scales and emissions projection used. However, the following
conclusions can be extracted: All the models point to a warmer future. Domain’s temperature is projected to increase for all seasons. All models project a homoge-
nous increase which depends on the season. There is less agreement among the
models about future precipitation change with differences in regions for increasing,
decreasing, or similar-to-current precipitation rates. The general trend is a reduction
at the south—southeast part of the domain which turns to an increase at the north
with a transition zone between them. Due to the largest grid size used in the other
studies, precipitation presents a more homogenous change compared to our results,
where seasonal trends are available in a very fine scale providing detailed infor-
mation for the continental regions and the islands.
Conclusions
Future temperature is estimated to be higher over southeast Europe. The increase
depends on both the season and the location, with higher increases during spring
and autumn at the south and southeast of the domain. More days with high
temperatures and fewer days with low temperatures are estimated in the future,
suggesting an extended future warmer period. Precipitation change is very location
dependent, presenting a mixed trend for all seasons. A large part of the land at the
southeast is estimated to have less annual precipitation in the future, however,
seasonal analysis suggests a wetter summer and an increase in the extreme precip-
itation rates during all future seasons.
Acknowledgement This work was supported by the EU co-funded LIFE-CONOPS project through grand agreement LIFE12 ENV/GR/000466.
9 Specific Case: Regional Estimates of Global Climate Change: A Dynamical. . . 107
References
Christensen, O. B., Goodess, C. M., & Ciscar, J.-C. (2012). Methodological framework of the
PESETA project on the impacts of climate change in Europe. Climatic Change, 112, 7–28. Dubrovsky, M., Hayes, M., Duce, P., Trnka, M., Svoboda, M., & Zara, P. (2014). Multi-GCM
projections of future drought and climate variability indicators for the Mediterranean region.
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Garcı́a-Ruiz, J. M., L�opez-Moreno, J. I., Vicente-Serrano, S. M., Lasanta–Martı́nez, T., & Beguerı́a, S. (2011). Mediterranean water resources in a global change scenario. Earth-Science Reviews, 105, 121–139.
Giorgi, F. (2006). Climate change hot-spots. Geophysical Research Letters, 33, L08707. Intergovernmental Panel on Climate Change (IPCC). (2000). In N. Nakicenovic, & R. Swart
(Eds.), Emissions scenarios. Cambridge: Cambridge University Press. Intergovernmental Panel on Climate Change (IPCC). 2013. In T. F. Stocker, D. Qin, G.-K.
Plattner, M. Tignor, S. K. Allen, J. Boschung, et al. (Eds.), Climate change 2013: The physical science basis. Contribution of working group I to the fifth assessment report of the intergov- ernmental panel on climate change. Cambridge/New York, NY: Cambridge University Press.
Luterbacher, J., Xoplaki, E., Casty, C., Wanner, H., Pauling, A., Küttel, M., and 43 co-authors,
2006. Mediterranean climate variability over the last centuries: a review. Edited by Lionello, P., Malanotte-Rizzoli, P., Boscolo, R., The Mediterannean Climate: An overview of the main
characteristics and issues, Amsterdam, Elsevier, pp. 27–148
Schmidt, G. A., Jungclaus, J. H., Ammann, C. M., Bard, E., Braconnot, P., Crowley, T. J.,
et al. (2011). Climate forcing reconstructions for use in PMIP simulations of the last millen-
nium (v1.0). Geoscientific Model Development, 4, 33–45. Schmidt, G. A., Ruedy, R., Hansen, J. E., Aleinov, I., Bell, N., Bauer, M., et al. (2006). Present day
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108 R.-E.P. Sotiropoulou et al.
Part III
Global Warming and Climate Change: General Issues and Challenges
Climate Change Observatory
Worldwide climate change observations, specific cases
Chapter 10
Drought Conditions in Turkey Between 2004 and 2013 Via Drought Indices Derived from Remotely Sensed Data
Nazila Molavizadeh, Elif Sertel, and Hande Demirel
Introduction
Drought is one of the major hazards that has a significant adverse effect on the
socio-economy, agriculture, and ecosystem. According to the United Nations
Convention to Combat Desertification, drought is defined as “the naturally occur-
ring phenomenon that exists when precipitation has been significantly below
normal recorded levels, causing serious hydrological imbalances that adversely
affect land resource production systems” (UN 2014). Evaporation (affected by
temperature and wind), soil types and their ability to store water, the depth and
presence of ground water supplies and vegetation are among the most important
parameters that influences occurrence of drought. Each drought year is unique in its
climatic characteristics and impacts, because drought is related to the timing and
the effectiveness of the precipitation. Therefore, it is impossible to make a defini-
tion of drought that can be universally accepted (Li and Xiao 1992; Wilhite 1993).
Drought can be described by three characteristics: spatial coverage, duration and
N. Molavizadeh (*) Satellite Communication & Remote Sensing Program, Department of Advanced Technology,
Informatics Institute, Istanbul Technical University, Maslak, 34469 Istanbul, Turkey
e-mail: [email protected]
E. Sertel
Geomatics Engineering Department, Istanbul Technical University, Maslak, 34469 Istanbul,
Turkey
Center for Satellite Communications and Remote Sensing, Istanbul Technical University,
Ground Receiving Station, Maslak, 34469 Istanbul, Turkey
e-mail: [email protected]
H. Demirel
Geomatics Engineering Department, Istanbul Technical University, Maslak, 34469 Istanbul,
Turkey
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_10
113
intensity (Wilhite and Glantz 1985). Briefly, according to (Heim 2002; Keyantash
and Dracup 2002), meteorological drought is a precipitation deficit, agricultural
drought is a total soil moisture deficit, hydrological drought is a shortage of stream
flow, and socioeconomic drought is associated with the shortage of any economic
goods affected by the drought process. The relationship between meteorological,
agricultural and hydrological drought is illustrated in Fig. 10.1 (NDMC 2014).
According to climate change scenarios such adverse impacts will gain speed in
the near future especially for certain locations of the world, including Turkey and
its neighborhood. Hence, monitoring its severity has a vital importance. This
requires understanding historical droughts in the region as well as impacts of
droughts during their occurrences. However, monitoring drought presents various
challenges such as inadequate data collection networks with respect to density of
stations, high cost of data and insufficient data sharing, difficulties in forecasting,
insufficiencies of drought indices for detecting the early beginning and end of the
drought, data integration problems such as soil parameters and socioeconomic
indicators, mitigation and response programs needs to be regional, therefore
regional assessments are required and data sharing and dissemination is limited
(WMO 2006). Several of these challenges could be eased by means of spatial
information technologies. Remote sensing based drought indices are becoming
more popular, since it is possible to determine spatio-temporal distribution of
Decreasing emphasis on the natural event (precipitation deficiencies)
Increasing emphasis on water/natural resource management Increasing complexity of impacts and conflicts
Meteorological Agricultural
Time/duration of the event
Hydrological
Socio-economic and political
Fig. 10.1 Interrelationships between meteorological, agricultural, hydrological and socioeco- nomic drought (NDMC 2014)
114 N. Molavizadeh et al.
droughts. Remote sensing satellites could monitor large areas rapidly, accurately,
periodically, economically and have been widely used to examine drought impacts.
In order to analyze the possibilities of remote sensing based drought indices,
three different indices namely Temperature Condition Index (TCI), Vegetation
Condition Index (VCI) and Vegetation Health Index (VHI) were generated to
determine drought conditions in Turkey for the last decade. MODIS-derived Nor-
malized Difference Vegetation Index (NDVI) and Land Surface Temperature
(LST) values were used to derive these indexes. NDVI values could be used to
identify healthy and unhealthy vegetation, where LST values derived from thermal
bands indicates the variations in temperature. Since, LST and NDVI are negatively
correlated; drought areas and periods could be investigated for the research area.
The paper is set out as follows: Section “Introduction”, introduces the problem and
the aim of the study. Section “Data and Methodology” covers case study area, the
data and methodology used. In Section “Results and Conclusion”, the achieved
results, problems encountered, major findings and conclusions from the study is
presented.
Data and Methodology
The development of remote sensing, spatial drought monitoring and assessment has
become possible in the last decades (Kanellou et al. 2008). Remote Sensing data
presents significant advantages and is the integral part of monitoring drought,
especially for the spatial and temporal evolution. A number of satellite drought-
monitoring indices are developed based on the Advanced Very High Resolution
Radiometer (AVHRR) of National Oceanic and Atmospheric Administration
(NOAA) polar-orbiting satellite series, MODIS (Moderate Resolution Imaging
Spectroradiometer) and others. Historically, the most commonly used remote
sensing tool for large-area drought monitoring has been the daily orbiting National
Oceanic and Atmospheric Administration (NOAA) Advanced Very High Resolu-
tion Radiometer (AVHRR), partially because there is now a sufficiently long time
series to let for the identification of anomalies to compare to “normal” conditions.
MODIS is superior to AVHRR because it provides higher spatial and spectral
resolutions, improved atmospheric corrections and more precise geolocation.
When compare the MODIS and AVHRR data sets such as NDVIAVHRR with
NDVIMODIS atmospherically corrected MODIS NDVI generally displays a higher
dynamic range than atmospherically corrected AVHRR NDVI. This is attributed to
the small bandwidth of MODIS (Huete et al. 2002; IWMI 2014). Within this study,
The Moderate-resolution Imaging Spectroradiometer (MODIS) data is used.
MODIS sensor was launched into Earth orbit by NASA in 1999 on board the
Terra (EOS AM) Satellite, and in 2002 on board the Aqua (EOS PM) satellite.
The MODIS has 36 spectral bands ranging in wavelength from 0.4 μm to 14.4 μm and at varying spatial resolutions (two bands at 250 m, five bands at 500 m and
29 bands at 1 km). Together the instruments image the entire Earth every 1–2 days.
10 Drought Conditions in Turkey Between 2004 and 2013 Via Drought Indices. . . 115
They are designed to supply measurements in large-scale global dynamics, includ-
ing changes in Earth’s cloud cover, radiation budget and processes occurring in the oceans, on land, and in the lower atmosphere. More information on MODIS data
could be obtained from NASA web-page (NASA 2014). Products of one of the well
known satellite system, MODIS, have been used for numerous research applica-
tions including mapping deforestation, identifying desertification and crop yield
estimation, natural and non-natural disasters—such as floods and droughts—in
many areas due to the its high temporal resolution and coverage. Terra MODIS
monthly composite NDVI images of 1 km resolution and Terra MODIS 8-day
composite LST of 1 km resolution were used in this research for the period
2004–2013.
The three remote sensing based drought indices, Vegetation Condition Index
(VCI), Temperature Condition Index (TCI) and Vegetation Health Index (VHI)
were generated and analyzed to determine drought conditions in Turkey for the last
decade.
Vegetation Condition Index (VCI): Kogan (1987) proposed a vegetation condi-
tion index based on the relative NDVI change with respect to minimum historical
NDVI value. VCI is pixel based normalization of NDVI values. The basic assump-
tion is that drought conditions will weaken the growth of vegetation resulting in
lower NDVI values in multiyear NDVI values (Du et al. 2013; Kogan 1995). VCI is
a good indicator of drought stress and its values scaled between 0 and 1. In case of
very dry month, vegetation conditions will be weakened and the value will close to
zero whereas a VCI value of 0.5 reflects fair vegetation conditions (Du et al. 2013).
It is defined as following:
VCI ¼ NDVI � NDVImin NDVImax � NDVImin ð10:1Þ
where NDVI, NDVImax, and NDVImin the smoothed monthly NDVI, multi-year
maximum NDVI and multi-year minimum NDVI, respectively, for each grid cell.
Temperature Condition Index (TCI): is a remote sensing based thermal stress
indicator that is used to quantify temperature component of droughts. There is a
higher LST in the drought year than the same month of normal years and this index
assumes that drought event will decrease soil moisture and cause land surface
thermal stress (Du et al. 2013; Kogan 1995). TCI is used to find out thermal stressed
regions by using the maximum/minimum temperature in a given time series. Since
drought is expected to decrease soil moisture and increase LST values, higher LST
values are signal for drought conditions and lower LST values indicates favorable
conditions, opposite to the NDVI (Du et al. 2013). Thus, the TCI formula was
modified as the following expression 10.2.
TCI ¼ LSTmax � LST LSTmax � LSTmin ð10:2Þ
116 N. Molavizadeh et al.
where LST, LSTmax and LSTmin are the values of LST, maximum LST and
minimum LST of each pixel respectively in the same month during the study period
of January 2004–December 2013. The is a good indicator to determine drought and
to find out its beginning time, intensity, duration and dynamics. The VCI could be
successfully used to define both prolonged and short-term droughts either global or
localized (Kogan 1995).
Vegetation Health Index (VHI): is calculated from an empirical formula by
giving equal weights to Vegetation Condition Index (VCI) and the Temperature
Condition Index (TCI) to reflect the impacts of both temperature and vegetation
components. The equation of VHI is below:
VHI ¼ 0:5 VCI þ TCIð Þ ð10:3Þ
The TCI indicates areas that are hotter than usual and the VCI’s normalized NDVI anomalies identify areas where vegetation is more or less dense than usual.
VHI reflects both vegetation cover and temperature anomalies and also it has been
widely applied for the early drought warning, monitoring of crop yield and pro-
duction, and assessment of irrigated areas and extreme wetness (Karnieli
et al. 2006) The classification of indices for drought conditions are presented in
Table 10.1 (Kogan 2001).
Results and Conclusion
Turkey is located in Anatolia and the Balkans, bordering the Black Sea, between
Bulgaria and Georgia, and bordering the Aegean Sea and the Mediterranean Sea,
between Greece and Syria. The total land area is about 783,562 km2, of which
756,816 km2 are in West Asia (Anatolia) and 23,764 km2 are in Southeastern
Europe (Thrace). Climatic conditions of Turkey vary significantly from one region
to another, due to topography and the geo-location of the country. While the coastal
regions have milder climates, extreme hot summers with limited rain fall and cold
winters are generally experienced at the inner Anatolian plateau (Sensoy
et al. 2008). The Aegean and Mediterranean coasts have cool, rainy winters and
hot, moderately dry summers. Annual precipitation in those areas varies from
580 to 1300 mm, depending on location. The Black Sea coast receives the greatest
amount of rainfall. The eastern part of that receives 2200 mm annually and is the
only region of Turkey that receives rainfall throughout the year. Climate types of
Turkey are presented in Fig. 10.2 (Atalay and Efe 2012).
In order to automate the process of generating indices and data handling, codes
were written in Interactive Data Language programming language and all indices
Table 10.1 Classification of VCI, TCI and VHI drought conditions (Kogan 2001)
VCI, TCI, VHI values * 100 <10 10–20 20–30 30–40 40–60 >60
Drought conditions Extreme Severe Moderate Mild Normal Wet
10 Drought Conditions in Turkey Between 2004 and 2013 Via Drought Indices. . . 117
were generated automatically. In the last 10 years, Turkey observes two drought
periods, the first one start from 2006. This drought period, is observed from
November and December of 2006 until December of 2008. This long period
between 2007 and 2008 clearly can be observed by analyzing the VCI and
VHI maps.
Drought is a slow occurring process starts with precipitation deficits, then
causing soil moisture deficits resulted in higher Land Surface Temperature (LST)
values. Finally, vegetation growth is affected because of water deficits and temper-
ature increases (Du et al. 2013). In this research LST and NDVI data were used to
monitor LST and NDVI anomalies during 10 year period using TCI and VCI
indexes. In order to represent both soil moisture deficit and vegetation growth,
VHI was calculated using TCI and VCI. VHI values between 40–60% represent
normal conditions whereas VHI values lower than 0.4 represents drought higher
than 0.6 represents wet climatic conditions.
TCI is based on LST values and could be used to identify regions that are hotter
or colder than usual values. For drought affected regions, higher temperature values
resulted in lower TCI values than normal conditions. TCI values lower than 30%
might give the signal of extreme, severe and/or moderate drought conditions. In
drought conditions, land surface will have thermal stress and TCI could be used to
determine temperature-related drought conditions (Du et al. 2013; Kogan 1995).
VCI is based on NDVI anomaly values and could be used to identify areas where
vegetation is more or less than usual values. In normal/usual conditions VCI pre-
sents same seasonal pattern and presents higher values in May-September period
and lower values in October-April period. Figure 10.3 shows an example of VCI for
2004 a normal year in terms of climatic conditions. As can be seen from the figure
VCI values are comparatively higher between May and September. Vegetation
response in the May–September period is related to the very wet period from
November–April (months where most of the geographic regions receive most of
Fig. 10.2 Climate types of Turkey (Atalay and Efe 2012)
118 N. Molavizadeh et al.
Fig. 10.3 VCI maps for the year 2004
10 Drought Conditions in Turkey Between 2004 and 2013 Via Drought Indices. . . 119
the precipitation). For drought occurring years such as 2007, VCI presents lower
values in May–September period as well unlike the normal conditions mentioned.
Turkey has different climatic regions as shown in Fig. 10.2. Black Sea Region
having coastal (humid-temperate) climate has vegetation throughout the year
resulting in higher VCI values as can be seen in Fig. 10.3. This region is highly
vegetated with mostly evergreen forests causing higher NDVI values. Considering
Turkey boundaries, during the winter months, most of the country has lower NDVI
values due to the fact that there are not planted agricultural areas and deciduous
plants.
Analysis of TCI, VCI and VHI maps illustrated that 2007, 2008 and 2013 were
drought impacted years in Turkey. In order to consider for temperature and vege-
tation growth, VHI maps were extensively analyzed. Figure 10.4 illustrates the
comparison of a normal (2004) and drought (2007) years. After comparing
12 months of each year, it was found that impact of drought is more detectable
between July and September. As can be seen from Fig. 10.4, during the drought
year 2007 most of the country has VHI values lower than 0.2 indicating the excess
or very excess drought conditions.
Fig. 10.4 Comparison of VHI maps between 2004–2007 for July, August and September
120 N. Molavizadeh et al.
Droughts can lead significant environmental, social, and economic conse-
quences by impacting agriculture, ecology and socio-economy. Therefore, it is
important to monitor droughts and their impacts in local, regional and global scales.
Meteorological data and drought indices derived from these data could be used to
monitor drought conditions however their spatial and temporal availability are
limited. To this end, remotely sensed data derived indices could be an important
asset to monitor drought conditions globally and timely.
References
Atalay, I., & Efe, R. (2012). Ecology of Scots pine (Pinus sylvestris var. sylvestris) forests and their dividing into regions in terms of seed transfer. Ministry of Environment and Forestry Publ. 45, Ankara. ISBN 975-605-4610-11-2.
Du, H. Y., Shen, Y. Z., & Huang, Z. J. (2013). Function of the wheat TaSIP gene in enhancing
drought and salt tolerance in transgenic Arabidopsis and rice. Plant Molecular Biology, 81, 417–429.
Heim, R. (2002). A review of twentieth-century drought indices used in the United States. Bulletin of the American Meteorological Society, 83, 1149–1165.
Huete, A., Didan, K., Miura, T., Rodriguez, E. P., Gao, X., & Ferreira, L. G. (2002). Overview of
the radiometric and biophysical performance of the MODIS vegetation indices. Remote Sensing of Environment, 83, 195–213.
IWMI. Retrieved February, 6, 2014, from http://www.iwmi.cgiar.org/.
Kanellou, E., Domenikiotis, C., Tsiros, E., & Dalezios, N. R. (2008). Satellite-based drought
estimation in Thessaly. European Water Publications, 23(24), 111–122. Karnieli, A., Bayasgalan, M., Bayarjargal, Y., Agam, N., Khudulmur, S., & Tucker, C. J. (2006).
Comments on the use of the Vegetation Health Index over Mongolia. International Journal of Remote Sensing, 27(10), 2017–2024.
Keyantash, J., & Dracup, J. (2002). The quantification of drought: An evaluation of drought
indices. Bulletin of the American Meteorological Society, 83, 1167–1180. Kogan, F. N. (1987). Vegetation index for areal analysis of crop conditions. In Proceedings of 18th
conference on agricultural and forest meteorology, September 15–18 (pp. 103–106). W. Lafayette, Indiana: AMS.
Kogan, F. N. (1995). Droughts of the late 1980s in the United States as derived from NOAA polar-
orbiting satellite data. Bulletin of the American Meteorological Society, 76(5), 655–668. Kogan, F. N. (2001). Operational space technology for global vegetation assessment. Bulletin of
the American Meteorological Society, 82(9), 1949–1964. Li, S.-X., & Xiao, L. (1992). Distribution and management of dryland in the People’s Republic of
China. Advances in Soil Science, 18, 148–278. NASA. Retrieved February 6, 2014, from http://modis.gsfc.nasa.gov/.
NDMC. Retrieved February 6, 2014, from http://drought.unl.edu/.
Sensoy, S., Demircan, M., Ulupınar, U., & Balta, İ. (2008). Türkiye İklimi, DMİ. http://www.dmi.
gov.tr/iklim/iklim.aspx.
UN. Retrieved February 6, 2014, from http://www.unccd.int/en/Pages/default.aspx.
Wilhite, D. A. (1993). Drought assessment, management, and planning: Theory and case study. Boston: Kluwer.
Wilhite, D. A., & Glantz, M. H. (1985). Understanding the drought phenomenon: The role of
definitions. Water International, 10, 111–120. World Meteorological Organization. (2006). Drought monitoring and early warning: Concepts,
progress and future challenges. WMO-No. 1006. ISBN 92-63-11006-9.
10 Drought Conditions in Turkey Between 2004 and 2013 Via Drought Indices. . . 121
Chapter 11
Carbon Foot Print of a Passanger Aircraft Engine at Landing and Take-Off Cycle
Yasin Ş€ohret and T. Hikmet Karakoç
Introduction
In last decade, rapid civilization forces us to develop more eco-friendly systems
with respect to the environmental issues. Mankind population growth on the earth
and utilization of the sources callously leads to consider sustainable development.
On the other hand, environmental impact reduction is as important as sustainability
at the present time. Especially damage and impact of the energy industry on the
environment become more of an issue for the future of the mankind. In this case,
transportation industry, which is an ever-growing and consuming energy sources
more and more, should be evaluated in terms of environmental issues (Winter 2014;
Lee et al. 2009). Under consideration of the aviation transportation growth in
Turkey, environmental impact of the aircrafts plays a key role for understanding
slice of this industry within the contribution of Turkey to the global warming and
climate change. As mentioned in a previous study (Ekici et al. 2013), number of
aircrafts in aviation fleet enormously increases day by day.
Many researcher studied on exhaust emission related issues of the aviation with
concern of environmental issues. Beck et al. (1992) presented the impact of the
aircraft emissions on atmosphere’s tropospheric layer by a two-dimensional model. Authors especially focused on ozone formation as a result of aircraft exhaust
emissions in the paper. Role of the nitrogen oxides within the global warming
was highlighted by authors. In another text, international airports in Korea was
Y. ހohret (*) Aircraft Technology Program, Keciborlu Vocational School,
Suleyman Demirel University, 32700 Isparta, Turkey
e-mail: [email protected]
T.H. Karakoç
Faculty of Aeronautics and Astronautics, Anadolu University, 26470 Eskisehir, Turkey
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_11
123
handled and dependence among the air pollution and the greenhouse gases emitted
from commercial aircrafts was investigated. Fan et al. (2012) calculated fuel
consumption and aircraft emissions from domestic flights for China in 2010. As a
result of their study, an airline emitting excessive emissions is selected in China. Hu
et al. (2009) evaluated air pollutants near an airport depending on real-time
measurements. Aircraft engine exhaust emissions, exhaust gases emitted from
other vehicles in the airport were discussed in the paper. Yilmaz and Ilbas (2012),
presented the emission parameters of various aircraft engine in service. Conse-
quently, the necessity of alternative fuel utilization in aircraft engines is empha-
sized by the authors. Aircraft engine emissions over the course of landing and take-
off cycle are investigated by Ekici et al. (2013) for the busiest airports in Turkey. In
another study, it is aimed to develop a model for nitrogen oxide emissions of a
turbofan engine for determining environmental impact of aircraft engine emissions
on the basis of the operational and meteorological conditions. In another text
(Naugle and Fox 2014), contribution of the emitted gases from aircrafts to air
pollution was discussed. Also, aircraft emissions caused health issues were
highlighted by the authors. Exhaust emissions of an aircraft engine which is fed
with both an alternative fuel and kerosene were evaluated by Santoni et al. (2011).
Especially unburned hydrocarbon and nitrogen oxide emissions were given in
details by authors. It is reported that, unburned hydrocarbon concentrations in
engine exhaust were lower than ambient concentrations at higher thrust levels.
Mazaheri et al. (2011) evaluated exhaust emissions of large aircrafts at an airport.
Authors presented emission rates depending on aircrafts operating in the airport.
Additionally, particulate matter emissions were discussed in details by researchers.
Synylo and Duchêne (2014) modelled nitrogen oxide emissions of a turbofan
engine to evaluate the impact of operational and meteorological conditions on
nitrogen oxide formation. Additionally the environmental sustainability of the
engine was discussed in the paper.
In the present paper, a turbofan engine of a commercial aircraft in service is
investigated. Carbon footprint of the examined engine is intended to present with
the aid of ICAO aircraft engine emissions inventory. The main goal and differences
of the current paper from previous studies may be listed as follows:
• Introducing the correlation between emission index and carbon footprint.
• Revealing the carbon footprint of an aircraft engine for the first time.,
• Presenting a different perspective to understand environmental impact of the
aviation.
Turbofan Engine and Evaluation Methodology
In this study, a mixed turbofan type aircraft engine is evaluated. The engine which
is named as JT8D is operated on many aircraft such as Boeing 727 and 737 series,
McDonnell Douglas DC-9 and MD-80. The JT8D serves the industry by providing
124 Y. Ş€ohret and T.H. Karakoç
power to more than 2400 aircraft. The sectional view of the engine is shown in
Fig. 11.1 (Pratt & Whitney 2014). For evaluation of the engine, data is provided
from the ICAO aircraft engine emissions inventory (EASA 2014).
The ICAO aircraft engine emissions inventory (EASA 2014) contains emission
data for the ICAO landing and take-off flight envelope. A typical flight envelope is
demonstrated in Fig. 11.2. ICAO landing and take-off flight cycle is the part of this
envelope which is under the 3000 feet altitude. In the course of emission measure-
ment, engine was operated under the relevant flight settings. That is to say, engine
was operated at 100%, 85%, 30% loads for 0.7, 2.2, 4.0 min at take-off, climb-out
and approach flight phases respectively (ICAO 1993).
Carbon footprint is the total sets of greenhouse gas emissions caused by an
organization, event, product or person and a useful parameter to understand con-
tribution to the climate change. The calculation of the carbon footprint is performed
by finding carbon dioxide equivalent for 100-year time horizon of the greenhouse
gases emitted by an organization, event, product or person. In this framework,
carbon footprint of the examined turbofan engine can be found as following
(Schimel et al. 1996; Wright et al. 2011):
C ¼ X
CO2eð Þi ¼ X
EIimfGWP 100ð Þi ð11:1Þ
Here, C notates carbon footprint whereas CO2e, EI, mf, GWP(100) and i
represents carbon dioxide equivalent, emission index, fuel mass flow rate, global
warming potential for 100-year time horizon and ith greenhouse gas emitted from
the engine. Carbon dioxide equivalent of any gas means global warming potential
of the gas for 100-year time horizon. Emission index indicates emitted gas amount
per consumed fuel amount within the combustion chamber. In Table 11.1, global
warming potentials of emitted gases for 100-year time horizon are given.
Fig. 11.1 The sectional view of the JT8D engine (Pratt & Whitney 2014)
11 Carbon Foot Print of a Passanger Aircraft Engine at Landing and Take-Off Cycle 125
Results and Discussion
In this study, carbon footprint of emitted greenhouse gases from JT8D engine which
is still operated on many commercial passenger aircraft. During a typical landing
and take-off flight cycle, exhaust gas emissions of the engine are given in
Table 11.2.
Calculations based upon data given in Table 11.2, are performed with the aid of
Eq. (11.1). Herein, unburned hydrocarbon (UHC) emission was assumed to be
Fig. 11.2 A typical flight envelope for a commercial aircraft (adopted from ICAO 1993)
Table 11.1 Global warming potential values of greenhouse gases emitted from an aircraft engine for 100-year time horizon (Altuntas 2014; Schimel et al. 1996)
Greenhouse gas GWP(100)
CO2 1
CO 1
NOx 310
CH4 21
Table 11.2 Exhaust gas emissions of the JT8D engine
at landing and take-off flight
cycle (EASA 2014)
Flight phase EICO EINOx EIUHC
Take-off 0.74 19.20 0.69
Climb-out 1.00 15.23 0.79
Approach 8.54 6.10 1.96
Idle 31.00 3.30 0.00
Total 41.28 43.83 3.44
126 Y. Ş€ohret and T.H. Karakoç
methane (CH4). As a result of the study, obtained carbon footprint equivalent of
each emission gas was summarized in Table 11.3 on the basis of flight phases.
For better comprehension of the situation, Figs. 11.3 and 11.4 are plotted. As
indicated in Fig. 11.3, unburned hydrocarbon emission index of the engine is
approximately same at take-off and climb-out phases of flight. However, emitted
unburned hydrocarbon per consumed fuel increases at approach phase and dramat-
ically decreases at idle. Additionally, reverse proportion among carbon monoxide
and nitrogen oxide emission index is clarified in the graph. So, it can be asserted
that, while amount of emitted carbon monoxide per consumed fuel raises, nitrogen
oxide emission descents over through the landing and take-off flight cycle.
Figure 11.4 reveals the carbon footprint of the engine during landing and take-
off flight cycle in simple terms. Herein, carbon footprint values of carbon monoxide
and unburned hydrocarbon are approximate to zero in comparison with nitrogen
oxide emission. However, carbon footprint of emitted nitrogen oxide decreases
from 7410.24 g to 150.381 g. So, impact of nitrogen oxides emitted from aircraft
engines on global warming is clearly proven.
Table 11.3 Carbon footprint equivalents of emitted
greenhouse gases from JT8D
engine at landing and take-off
flight cycle
Flight phase C(CO) C(NOx) C(UHC)
Take-off 0.921 7410.240 18.040
Climb-out 0.997 4707.136 16.540
Approach 3.023 669.414 14.570
Idle 4.557 150.381 0
Total 9.498 12937.170 49.150
Fig. 11.3 Emission index variation of JT8D engine greenhouse gases with flight phases
11 Carbon Foot Print of a Passanger Aircraft Engine at Landing and Take-Off Cycle 127
Conclusions
As a result of the study, following statements are concluded by authors:
• With regard to emission measurement, emitted greenhouse gases from the
engine are concern. On the other, in terms of carbon footprint calculation carbon
monoxide and unburned hydrocarbons can be disregarded in future studies. But
it is not possible to assert for nitrogen oxide emission.
• Conducting similar study for various engine types can be beneficial as a com-
parison. So that, contribution of aircraft engine exhaust emissions to global
warming and carbon cycle can be revealed in details.
• If the flights all around the world are considered, obtained results can be more
meaningful. However, from this point of view, impact of aircraft transportation
on the environment may be more comprehensible.
In a future study, it is planned to cover that issue from perspective of aviation
fleet and comparison of different aircraft engine types.
Acknowledgements Authors gladly thank to Anadolu and Suleyman Demirel Universities of Turkey.
Fig. 11.4 Carbon footprint variation of JT8D engine greenhouse gases with flight phases
128 Y. Ş€ohret and T.H. Karakoç
Nomenclature
C Carbon footprint CO2e Carbon dioxide equivalent EI Emission index (g kg�1) GWP Global warming potential m Mass flow rate (kg s�1)
Subscripts
f Fuel i ith greenhouse gas emitted from the engine
References
Altuntas, O. (2014). Calculation of domestic flight-caused global warming potential from aircraft
emissions in Turkish airports. International Journal of Global Warming, 1, 367–379. Beck, J. P., Reeves, C. E., De Leeuw, F. A., & Penkett, S. A. (1992). The effect of aircraft
emissions on tropospheric ozone in the northern hemisphere. Atmospheric Environment. Part
A. General Topics, 26(1), 17–29. EASA. (2014). ICAO Aircraft engine emissions databank. Retrieved December 15, 2014, from
http://easa.europa.eu/document-library/icao-aircraft-engine-emissions-databank#1.
Ekici, S., Yalin, G., Altuntas, O., & Karakoc, T. H. (2013). Calculation of HC, CO and NOx from
civil aviation in Turkey in 2012. International Journal of Environment and Pollution, 53, 232–244.
Fan, W., Sun, Y., Zhu, T., &Wen, Y. (2012). Emissions of HC, CO, NOx, CO2, and SO2 from civil
aviation in China in 2010. Atmospheric Environment, 56, 52–57. Hu, S., Fruin, S., Kozawa, K., Mara, S., Winer, A., & Paulson, S. (2009). Aircraft emission impacts
in a neighborhood adjacent to a general aviation airport in southern California. Environmental Science & Technology, 43, 8039–8045.
ICAO. (1993). Annex 16. In Aircraft engine emissions (2nd ed.). Lee, D. S., Fahey, D. W., Forster, P. M., Newton, P. J., Wit, R. C. N., Lim, L. L., et al. (2009).
Aviation and global climate change in 21st century. Atmospheric Environment, 43, 3520–3537. Mazaheri, M., Johnson, G. R., & Morawska, L. (2011). An inventory of particle and gaseous
emissions from large aircraft thrust engine operations at an airport. Atmospheric Environment, 45, 3500–3507.
Naugle, D., & Fox, D. (2014). Aircraft and air pollution. Environmental Science and Technology, 15, 391–395.
Pratt & Whitney, JT8D engine. Retrieved December 15, 2014, from http://www.pw.utc.com/
JT8D_Engine.
Santoni, G., Lee, B., Wood, E., Herndon, S., Miake-Lye, R., Wofsy, S., et al. (2011). Aircraft
emissions of methane and nitrous oxide during the alternative aviation fuel experiment.
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Synylo, K., & Duchêne, N. (2014). NOx emission model of turbofan engine. International Journal of Sustainable Aviation, 1, 72–84.
Winter, R. A. (2014). Innovation and the dynamics of global warming. Journal of Environmental Economics and Management, 68, 124–140.
Wright, L. A., Kemp, S., & Williams, I. (2011). ‘Carbon footprinting’: towards a universally accepted definition. Carbon Management, 2, 61–72.
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130 Y. Ş€ohret and T.H. Karakoç
Chapter 12
Greenhouse Gas Emissions Trends from Waste in Greece
L. Kallinikos, I. Sebos, A. Progiou, P. Eleni, I. Katsavou, K. Mangouta,
and I. Ziomas
Introduction
United Nations Framework Convention on Climate Change (henceforth the Con-
vention) was adopted on 9May 1992 and was opened for signature in Rio de Janeiro
in June 1992 in response to the emerging evidence that climate change could have a
major global impact. Greece signed the Convention in Rio and ratified it in 1994.
The Conference of the Parties (COP) in 2007, by its decision 1/CP.13 (the Bali
Action Plan) launched a comprehensive process to enable the full, effective and
sustained implementation of the Convention through long-term cooperative action,
now, up to and beyond 2012, to be conducted under a subsidiary body of the
Convention, the Ad Hoc Working Group on Long-term Cooperative Action under
the Convention (AWG-LCA).
The Protocol entered into force on 16 February 2005, after its ratification from
141 Parties (with the exception of USA and Australia) including developed coun-
tries with a contribution of more than 55% to global CO2 emissions in 1990.
With respect to the EU target under the Kyoto Protocol (i.e. reduction of
emissions by 8% for the period 2008–2012), EU has stated that this will be
achieved jointly by EU Member-States under the provisions of Article 4 of the
Protocol. The Burden-Sharing agreement between all Member States was finalized
during the Environment Council in June 1998 and entered into force with Decision
2002/358/EC concerning the approval, on behalf of the European Community, of
the Kyoto Protocol. According to this agreement, Greece is committed to limit its
L. Kallinikos • I. Sebos (*) • A. Progiou • P. Eleni • I. Katsavou • K. Mangouta • I. Ziomas Department of Chemical Engineering, National Technical University of Athens, Zografou
Campus, 9 Heroon Polytechniou Street, 15780 Zografou, Greece
e-mail: [email protected]; [email protected]; [email protected]; peleni@central.
ntua.gr; [email protected]; [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_12
131
GHG emissions increase for the period 2008–2012 toþ25% compared to base year emissions.
For the period 2013–2020 EU adopted the climate and energy package which is a
set of binding legislation aiming in ensuring of the European Union meets its
ambitious climate and energy targets for 2020. These targets, known as the “20-
20-20” targets, set three key objectives for 2020 (http://ec.europa.eu/clima/policies/
ets/index_en.htm):
• A 20% reduction in EU greenhouse gas emissions from 1990 levels.
• Raising the share of EU energy consumption produced from renewable
resources to 20%.
• A 20% improvement in the EU’s energy efficiency.
Finally, EU leaders agreed on 23 October 2014 the domestic 2030 greenhouse
gas reduction target of at least 40% compared to 1990 together with the other main
building blocks of the 2030 policy framework for climate and energy, as proposed
by the European Commission in January 2014. This 2030 policy framework aims to
make the European Union’s economy and energy system more competitive, secure
and sustainable and also sets a target of at least 27% for renewable energy and
energy savings by 2030.
Regarding Greek contribution in the first commitment period, 2008–2012, the
country ratified the Kyoto Protocol in 2002 (Law 3017/2002) and adopted a
National Programme for achieving its commitment by a decision of the Council
of Ministers (DCM5/2003).
Annual inventories of greenhouse and other gases emissions form an essential
element of each national environmental policy-making process. They can be used
to derive information on emissions trends, with reference to a pre-selected base
year, and can assist in monitoring the progress of existing abatement measures for
the reduction of greenhouse gases emissions and the fulfillment of the KP target
(MRPEE 2014b).
According to UNFCCC structure for the first commitment period, 2008–2012,
annual inventories regarding emissions sources could be categorized to the follow-
ing sectors (IPCC 1997, 2002):
Energy sector
Industrial processes
Solvents and other products
Agriculture
Waste
Land Use, Land Use Change and Forestry (LULUCF)
Waste sector consists one of the sectors as they are categorized by IPCC
Guidelines and it is recognized that the waste management industry plays an
increasing role in climate change mitigation (Ragossnig and Hilger 2008).
The definition of ‘waste management’ adopted here covers four basic divisions (UN 1998; Bogner et al. 2008; Braschel and Posch 2013):
132 L. Kallinikos et al.
• Solid waste disposal on land
• Wastewater handling
• Waste incineration
• Other (Biological treatment)
Solid Waste Disposal on Land
Solid waste disposal on land is responsible for methane emissions. Methane is
emitted during the anaerobic decomposition of organic waste disposed in various
solid waste disposal sites (SWDS). The main characteristic of this process is that
organic waste decomposes at a diminishing rate over time and takes many years to
decompose completely. Moreover, other factors such as the type of waste disposed,
the characteristics of the disposal sites and the climate conditions, affect the
decomposition rate.
Carbon dioxide emissions occur during the flaring of biogas released from the
decomposition of waste. However, these emissions should not be included in the
total GHG emissions of the sector as they are of biogenic origin. Recovery and
flaring of biogas constitute a waste management practice in the major
managed SWDS.
Methane emissions from solid waste disposal on land consist of emissions from
municipal solid waste disposal on sites, emissions from sewage sludge (generated
during municipal wastewater handling) landfilled and emissions from industrial
solid waste and construction and demolition solid waste disposal in managed and
unmanaged sites (MRPEE 2014b; IPCC 1997, 2002).
The estimation of methane emissions from solid waste disposal on land could be
based on default emission factors or more detailed methodologies. IPCC Guidelines
provide three accounting methods; Tier 1, Tier 2 and Tier 3. Tier 1 provides IPCC
default data to countries with little data available (Braschel and Posch 2013). Tier
2 includes first-order decay (FOD) equations with some default parameters defined
by the IPCC, while Tier 3 is based on FOD equations with nationally developed
parameters, such as the degradable organic content of the waste (Gentil et al. 2009).
The method is applied separately for the managed and unmanaged waste disposal,
taking account of the different conditions in those sites and the detailed information
available regarding the opening and closure years of the operation of the managed
sites (MRPEE 2014b; IPCC 1997, 2002, 2006).
Wastewater Handling
Domestic and industrial wastewater handling under anaerobic conditions produces
CH4 while under aerobic treatment they result in sewage sludge production, the
disposal of which produces also CH4. Moreover, from both sub sectors N2O
12 Greenhouse Gas Emissions Trends from Waste in Greece 133
emissions are released (MRPEE 2014b; IPCC 1997, 2002). For the estimation of
the emissions from waste water handling default methodologies are provided by
IPCC (1997), IPCC (2002) and IPCC (2006).
Waste Incineration
Carbon dioxide, Methane and Nitrous oxide emissions produced from the inciner-
ation of waste such as clinical waste, biogenic agricultural residues produced in
slaughterhouses and from the incineration of small amounts of industrial chemical
waste are being estimated (MRPEE 2014b; IPCC 1997, 2002). For the estimation of
the emissions from this sector default methodologies are provided by IPCC (1997),
IPCC (2002) and IPCC (2006).
Emissions Trend
Total Emissions
Information regarding the methodologies utilized on the estimation of emissions
from the different sectors and the data collection are provided by the annual
emissions inventory submission of Greece (MRPEE 2014b).
According to these estimations in 2012, GHG emissions (without LULUCF)
amounted to 110.78 Mt CO2 eq showing an increase of 3.63% compared to base
year emissions and of 5.86% compared to 1990 levels.
Carbon dioxide emissions accounted for 81.67% of total GHG emissions in
2012 (without LULUCF) and increased by approximately 9.11% from 1990.
Methane emissions accounted for 8.57% of total GHG emissions in 2012 and
decreased by 8.77% from 1990, while nitrous oxide emissions accounted for
6.15% of the total GHG emissions in 2012 and decreased by 33.39% from 1990.
Finally, f-gases emissions (from production and consumption) that accounted for
3.95% of total GHG emissions in 2012, and 41.16% of the IP sector, has an average
increase of 33.19% from 1995 (base year for F-gases).
In Fig. 12.1, the evolution of the emissions for the period 1990–2012 are
provided. In the same figure the evolution of the Gross Domestic Product (GDP)
is provided. As it is observed GHG emissions follow the trend of GDP. Over the last
5 years Greek economy faced its most-severe crisis since it experienced a signif-
icant recession having recorded a cumulative decline in real terms exceeding 20%
(by the end of 2012 compared to GDP at the end of 2007).
The repercussions from the international financial crisis are unavoidable felt also
in Greece especially through the negative impact in the two significant exporting
sectors (tourism and ship transportation) but at a large extent economic downturn
134 L. Kallinikos et al.
relates also to the diminishing growth potential of the country since no significant
changes have occurred in the domestic production model towards innovative or
high value added activities.
Before this 5 years period, Greek growth performance was impressive. The
annual rate of increase of the GDP during the period 2000–2004 was approximately
4.5% due to the financial market liberalization coupled with membership in the
monetary union, which led to substantial increase in credit expansion and reduction
in borrowing costs, the stimulus given by the Olympic Games hosted in Athens in
2004 and the Community Structural Funds. Contrary to expectations of a post-
Olympics slump, the economy continued to grow briskly in 2005–2007 period.
GDP increased by an average growth rate of 3.7% and thus Greece enjoyed one of
the highest growth rates in the EU and the Eurozone.
Regarding EU-15 and E-28 related information are provided by the annual
emissions inventory submission of European Commission (European Environmen-
tal Agency 2014b). In 2012 total GHG emissions in the EU-15, without LULUCF,
were 15.1% (644 million tonnes CO2 equivalents) below 1990. Between 2011 and
2012 emissions decreased by 0.8% (31 Mt of CO2 equivalents) (http://unfccc.int/).
Total GHG emissions, without LULUCF, in the EU-28 decreased by 19.2%
between 1990 and 2012 (�1082 Mt of CO2 equivalent). Between 2011 and 2012, emissions decreased by 1.3% (59 Mt CO2 equivalent) (Fig. 12.2).
In the same figure the evolution of the GDP is provided. As it is observed GDP of
the European Union, for both EU-15 and EU-28, decreases only for 2009, while
GHG emissions decreases for the period 2005–2012 as a result of the mitigation
measures adopted by its members.
2.E+05
Greece
GDP1.E+05
1.E+05
1.E+05
8.E+04
6.E+04
4.E+04
2.E+04
0.E+00
19 90
19 91
19 92
19 93
19 94
19 95
19 96
19 97
19 98
19 99
20 00
20 01
20 02
20 03
20 04
20 05
20 06
20 07
20 08
20 09
20 10
20 11
20 12
300
250
200
150
100
50
0
G D
P (
co n
st an
t 20
05 U
S E
)- b
ill io
n s
U S
E
T o
ta l G
H G
e m
is si
o n
s, E
xc lu
d in
g L
U L
U C
F (
G g
C O
2e q
)
Fig. 12.1 Total GHG emissions of Greece and GDP
12 Greenhouse Gas Emissions Trends from Waste in Greece 135
Waste Sector
In general, waste sector is the fourth largest sector in Greece, contributing 4.3% of
the total greenhouse gas emissions sector in 2012 (excluding Land Use, Land-Use
Change and Forestry, LULUCF), while GHG emissions from waste decreased by
19.6% in 2012 compared to 1990 levels, based on the latest official GHG inventory
for the country. Similarly, the waste sector is the fourth largest sector in the EU-28
with approximately 3.1% contribution on the total GHG emissions for 2012, while
the total decrease over the period 1990–2012 is about 31.5% (Fig. 12.3).
Information regarding the methodologies utilized on the estimation of emissions
from the waste sector and the data collection are provided by the annual emissions
inventory submission of Greece (MRPEE 2014b).
Specifically, the major Waste category since 1999 for Greece is the solid waste
disposal on land with its contribution increasing from 37.8% in 1990 to 67.7% in
2012. On the contrary, GHG emissions from wastewater handling was the major
source up to 1999, presenting a declining trend with an average annual rate of
�2.69% for the period 1990–2012. Emissions from the incineration of waste present a negligible contribution on the total GHG from the waste sector. Similarly,
GHG emissions from waste disposal on land accounts for 72.3% of the total waste
greenhouse gas emissions in the EU-28 for the 2012.
Emissions from the Waste Sector (4.27% of the total emissions, without
LULUCF), decreased by approximately 19.58% from 1990. Living standards
improvement resulted in an increase of the generated waste and thus of emissions.
However, the increase of recycling along with the exploitation of the biogas
European Union (15)
GDP
European Union (28)
GDP 6.E+06
5.E+06
4.E+06
3.E+06
2.E+06
1.E+06
0.E+00
19 90
19 91
19 92
19 93
19 94
19 95
19 96
19 97
19 98
19 99
20 00
20 01
20 02
20 03
20 04
20 05
20 06
20 07
20 08
20 09
20 10
20 11
20 12
16000
14000
12000
8000
10000
6000
4000
2000
0
G D
P (
co n
st an
t 20
05 U
S D
)- b
ill io
n s
U S
D
T o
ta l G
H G
e m
is si
o n
s, E
xc lu
d in
g L
U L
U C
F (
G g
C O
2e q
)
Fig. 12.2 Total GHG emissions for European Union (EU15 and EU28) versus GDP
136 L. Kallinikos et al.
produced limits the increase of methane emissions. At the same time, emissions
from wastewater handling have considerably decreased, due to the continuous
increase of the population served by aerobic wastewater handling facilities.
Waste sector is the fourth largest sector in the EU-15, after energy, agriculture
and industrial processes, contributing 3% to total GHG emissions (European
Environmental Agency 2014b). Total emissions from Waste have been decreasing
by 40% from 171 Tg in 1990 to 102 Tg in 2012 (Fig. 12.4 for EU-15, Fig. 12.5 for
EU-28). In 2012, emissions decreased by 3.3% compared to 2011.
As it shown in this figure, CH4 emissions from Managed Waste Disposal on
Land had the greatest decrease of all waste-related emissions, but still account for
66% of waste-related GHG emissions in the EU-15 in 2012.
Solid Waste Disposal
Given the fact that solid waste sector is the main source for both Greece and EU, an
analysis on it is presented in this paragraph. As it is observed in the Fig. 12.2,
Greenhouse gas emissions from solid waste disposal on land present an increasing
trend, with some fluctuations due to variations on the CH4 recovered each year. This
is the result of the increasing trend observed on the municipal solid waste disposal
on land for the period 1990–2012, Fig. 12.6. While the solid waste generation
increase rate is significantly higher than this of disposal on solid waste disposal
Other
Incineration
Solid Waste
Wastewater Handling
7.E+03
6.E+03
5.E+03
3.E+03
4.E+03
2.E+03
1.E+03
0.E+00
19 90
19 91
19 92
19 93
19 94
19 95
19 96
19 97
19 98
19 99
20 00
20 01
20 02
20 03
20 04
20 05
20 06
20 07
20 08
20 09
20 10
20 11
20 12
T o
ta l G
H G
e m
is si
o n
s fr
o m
W as
te S
ec to
r (G
g C
O 2e
q )
Fig. 12.3 GHG emissions from Waste Sector for Greece
12 Greenhouse Gas Emissions Trends from Waste in Greece 137
2.E+05
2.E+05
2.E+05
1.E+05
1.E+05
1.E+05
8.E+04
6.E+04
4.E+04
2.E+04
0.E+00
T o
ta l G
H G
e m
is si
o n
s fr
o m
W as
te S
ec to
r fo
r E
U -1
5 (G
g C
O 2e
q )
19 90
19 91
19 92
19 93
19 94
19 95
19 96
19 97
19 98
19 99
20 00
20 01
20 02
20 03
20 04
20 05
20 06
20 07
20 08
20 09
20 10
20 11
20 12
Other
Incineration
Solid Waste
Wastewater Handling
Fig. 12.4 GHG emissions from Waste Sector for European Union (EU15)
3.E+05
2.E+05
2.E+05
1.E+04
5.E+04
0.E+00
T o
ta l G
H G
e m
is si
o n
s fr
o m
W as
te S
ec to
r fo
r E
U -2
8 (G
g C
O 2e
q )
19 90
19 91
19 92
19 93
19 94
19 95
19 96
19 97
19 98
19 99
20 00
20 01
20 02
20 03
20 04
20 05
20 06
20 07
20 08
20 09
20 10
20 11
20 12
Other
Incineration
Solid Waste
Wastewater Handling
Fig. 12.5 GHG emissions from Waste Sector for European Union (EU28)
138 L. Kallinikos et al.
sites, the increasing trend on the treatment of solid waste, recycling and
composting, is not able to decrease the amounts of solid waste disposal on sites.
For this reason, emissions of the sector are showing an increasing trend. In contrast,
both for EU-15 and EU-28 the solid waste amount treatment increases for all the
period of 1990–2012 resulting in a decreasing trend on the amounts of solid waste
disposal on sites and the emissions (Figs. 12.7 and 12.8).
Projections
For the projection of the evolution of the emissions for the period 2013–2030 the
impact of the implemented, adopted and planned policies and measures for the
mitigation of the emissions are utilized (MRPEE 2014a). This policy is fully
harmonized with the EU policy for the mitigation of GHG emissions from waste
and is mainly described by the regulation for the Municipal Waste disposal on land
(Landfill Dir. 1999/31/EC), the sewage sludge use in agricultures (Dir. 86/278/
EEC), the Paper/Cardboard recycling (Dir. on Packaging and Packaging Waste,
94/62/EC) and the Bio-wastes in the Waste Framework Dir. (art. 22, 2008/98/EC).
With Decision 50910/2727 (December 2003), the National Law 4042/2012
(OJG 24 A) and the transposition of Directive 2008/98/EC into national legislation
the measures, the terms and the processes for the rational management of waste in
national and regional level have been specified.
S o
lid W
as te
D is
p o
sa l (
G g
)
19 90
19 91
19 92
19 93
19 94
19 95
19 96
19 97
19 98
19 99
20 00
20 01
20 02
20 03
20 04
20 05
20 06
20 07
20 08
20 09
20 10
20 11
20 12
6.E+03
5.E+03
4.E+03
3.E+03
2.E+03
1.E+03
0.E+00
170.00
150.00
130.00
90.00
110.00
70.00
50.00
S o
lid w
as te
G en
er at
ed c
o m
p . t
o 1
99 0
(% )
Annual MSW at Managed SWDS (Gg)
Annual MSW at Unmanaged SWDS (Gg)
Solid waste Generated comp. to 1990 (%)
Fig. 12.6 Annual municipal solid waste disposal and solid waste generated compared to 1990 of Greece
12 Greenhouse Gas Emissions Trends from Waste in Greece 139
S o
lid W
as te
D is
p o
sa l (
G g
)
19 90
19 91
19 92
19 93
19 94
19 95
19 96
19 97
19 98
19 99
20 00
20 01
20 02
20 03
20 04
20 05
20 06
20 07
20 08
20 09
20 10
20 11
20 12
3.E+05
2.E+05
2.E+05
1.E+05
5.E+04
0.E+00
110.00
120.00
130.00
140.00
150.00
100.00
90.00
70.00
80.00
60.00
50.00
S o
lid w
as te
G en
er at
ed c
o m
p . t
o 1
99 0
(% )
Annual MSW at Managed SWDS (Gg)
Annual MSW at Unmanaged SWDS (Gg)
Solid waste Generated comp. to 1990 (%)
Fig. 12.7 Annual municipal solid waste disposal and solid waste generated compared to 1990 of EU-15
19 90
19 91
19 92
19 93
19 94
19 95
19 96
19 97
19 98
19 99
20 00
20 01
20 02
20 03
20 04
20 05
20 06
20 07
20 08
20 09
20 10
20 11
20 12
S o
lid W
as te
D is
p o
sa l (
G g
)
3.E+05
2.E+05
2.E+05
1.E+05
5.E+04
0.E+00
110.00
120.00
130.00
140.00
150.00
100.00
90.00
70.00
80.00
60.00
50.00
S o
lid w
as te
G en
er at
ed c
o m
p . t
o 1
99 0
(% )
Annual MSW at Managed SWDS (Gg)
Annual MSW at Unmanaged SWDS (Gg)
Solid waste Generated comp. to 1990 (%)
Fig. 12.8 Annual municipal solid waste disposal and solid waste generated compared to 1990 of EU-28
140 L. Kallinikos et al.
Fundamental objectives are the elimination of unmanaged solid waste disposal
sites, the coverage of all urban and rural areas of the country with modern instal-
lations for final disposal and the promotion of measures for the prevention and
reduction of produced waste, as well as the exploitation of materials with maximi-
zation of recycling and recovery of products and energy. The necessity to reduce the
quantities of biodegradable wastes landfill through the installation of treatment
facilities, Joint Ministerial Decision 29407/3508 in agreement with Directive 1999/
31/EC, is acknowledged.
The reduction of biodegradable waste landfill is enhanced by the directive for
Packaging and Packaging Waste (94/62/EC) Paper/Cardboard recycling.
Concerning bio-wastes treatment the legislative framework is based in theWaste
Framework Dir. (art. 22, 2008/98/EC). According to this, Article 41, until 2015
separately collected bio-waste shall be minimum 5% of the total produced
bio-waste and until 2020, separately collected bio-waste shall be minimum 10%
of the total produced bio-waste.
The flaring of landfill gas in all managed sites for urban centres with population
more than 100,000 is partially an integrated measure. Already, the managed
disposal sites serving the population of the largest cities of Greece are equipped
with systems for the collection or for the flaring of biogas.
As regards wastewater, a collection network with its corresponding wastewater
treatment plants has already been developed during the last 5-years, covering the
needs of 70% of the population in 2001 and the 91% in 2011, in compliance with
the Directive 91/271/EEC concerning the collection, treatment and discharge of the
urban wastewater. In the Psyttalia wastewater treatment plant that serves approx-
imately four millions of Attica population, a part the sludge produced is treated
under anaerobic conditions resulting in the production of biogas. The biogas
produced covers the energy needs of the wastewater treatment facilities, while the
surplus is flared.
The quantities of the solid waste end out at disposal sites were estimated on the
bases of historical data as well as on the implementation of adopted policies and
measures taking into consideration the deflection from the targets due to economic
recession. The composition of the solid waste landfill at disposal sites was esti-
mated taking into account the composition of MSW generated and the amounts of
waste recycling and compost.
The obtained results for Greece are presented in Fig. 12.9 and for EU in
Fig. 12.10 (European Environmental Agency 2014a).
As it is shown, in 2020 emissions from waste sector of Greece are estimated to be
decreased by 22% compared to 1990 and in 2030 28% compared to 1990. At the
same time, emissions from waste for EU are estimated to be decreased in 2020 49%
(EU-15) and 44% (EU-28) compared to 1990 and in 2030 63% (EU-15) and 50%
(EU-28) compared to 1990. Therefore, it is estimated that if the total targets for the
Greenhouse Gas emissions are equal to the targets for the waste sector (20% in
2020 compared to 1990 and 40% in 2030 compared to 1990) EU-15 and EU-28
have already achieved with the measures that already have adopted/planned, while
for Greece additional measures are needed for 2030.
12 Greenhouse Gas Emissions Trends from Waste in Greece 141
19 90
20 30
20 25
20 20
20 15
20 10
20 05
20 00
19 95
7.E+03
6.E+03
5.E+03
3.E+03
4.E+03
2.E+03
1.E+03
0.E+00
G H
G e
m is
si o
n s
fr o
m W
as te
S ec
to r
(G g
C O
2e q
) Waste incineration
Industrial wastewater
Domestic wastewater
Solid waste disposal on land
Fig. 12.9 Emissions from waste sector projections for Greece
19 90
20 30
20 20
20 10
G H
G e
m is
si o
n s
fr o
m W
as te
S ec
to r
(G g
C O
2e q
)
European Union (15) European Union (28)3.E+05
2.E+05
2.E+05
1.E+04
5.E+04
0.E+00
Fig. 12.10 Emissions from waste sector projections for EU-15 and EU-28
142 L. Kallinikos et al.
Conclusions
Based on the analysis presented in the current work the following conclusions
derive:
• Total GHG emissions of Greece follow the trend of GDP. They increase up to
2007 and they decrease in the period 2008–2012 during economic recession.
• Total GHG emissions of EU trend decreases for all the period 1990–2012.
• Waste sector is the fourth largest sector in Greece and it has shown a decreased
trend from 2000 mainly due to declining trend of emissions from wastewater
handling subsector while GHG emissions from waste sector for EU decrease for
all the period 1990–2012.
• If the total targets for the Greenhouse Gas emissions are equal to the targets for
the waste sector, EU-15 and EU-28 has already achieved their targets with the
measures that already have adopted/planned.
• Greece seems to need some additional measures for 2030.
• It must be mentioned that specific targets for waste sector depends on the
disaggregation of total GHG emission targets taking into consideration
EU-ETS and non EU-ETS specific targets and the ability for emission decrease
of the sectors like F-gases and Agriculture sector.
References
Bogner, J., Pipatti, R., & Hashimoto, S. (2008). Mitigation of global greenhouse gas emissions
from waste: Conclusions and strategies from the Intergovernmental Panel on Climate Change
(IPCC) Fourth Assessment Report. Working Group III (Mitigation). Waste Management & Research, 26, 11–32.
Braschel, N., & Posch, A. (2013). A review of system boundaries of GHG emission inventories in
waste management. Journal of Cleaner Production, 44, 30–38. European Environmental Agency. (2014a). Sixth National Communication and first biennial
report from the European Union under the UN framework convention on climate change (UNFCCC), technical report.
European Environmental Agency. (2014b). Annual European Union greenhouse gas inventory 1990–2012 and inventory report 2014 Submission to the UNFCCC.
Gentil, E., Christensen, T. H., & Aoustin, E. (2009). GHG accounting and waste management.
Waste Management and Research, 27, 696–706. Intergovernmental Panel on Climate Change (IPCC). (1997). Revised 1996 IPCC guidelines for
national greenhouse gas inventories—Greenhouse gas inventory reference manual (Vol. 3). Bracknell: IPCC/OECD/IEA, UK Meteorological Office.
Intergovernmental Panel on Climate Change (IPCC). (2002).Good practice guidance for land use, land use change and forestry. Japan: IPCC National Greenhouse Gas Inventories Programme, Institute for Global Environmental Strategies.
Intergovernmental Panel on Climate Change (IPCC). (2006). IPCC guidelines for national GHG inventories. Japan: IPCC National Greenhouse Gas Inventories Programme, Institute for Global Environmental Strategies.
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Ministry of Reconstruction of Production Environment & Energy (MRPEE) (former: Ministry of
Environment, Energy and Climate Change). (2014a). Sixth National Communication and 1st biennial report under the United Nations framework convention on climate change.
Ministry of Reconstruction of Production Environment & Energy (MRPEE) (former: Ministry of
Environment, Energy and Climate Change). (2014b). Emissions inventory annual inventory submission of Greece under the convention and the Kyoto protocol for greenhouse and other gases for the years 1990–2012.
Ragossnig, A., & Hilger, H. (2008). Editorial: Waste management: Stepping up to the climate
change challenge. Waste Management & Research, 26, 3–4. United Nations (UN). (1998). Kyoto-protocol to the United Nations Framework Convention on
Climate Change. http://ec.europa.eu/clima/policies/ets/index_en.htm on March 31, 2015. http://unfccc.int/, Accessed on March 31, 2015
144 L. Kallinikos et al.
Part IV
Global Warming and Climate Change: General Issues and Challenges
Climate Prediction Tools
Development and Application of Climate Prediction Tools
Chapter 13
Development of Models for the Estimation of Global Solar Radiation Over Selected Stations in India
M. Maroof Khan, M. Jamil Ahmad, and Basharat Jamil
Introduction
Solar radiation, passing through the atmosphere, reaching the earth on a horizontal
surface can be classified into two components: beam radiation and diffuse radiation.
Beam radiation is the solar radiation propagating along the line joining the receiv-
ing surface and the center of the sun. It is also referred to as direct radiation. Diffuse
radiation on the other hand, is the solar radiation scattered by aerosols, dust and
molecules in the atmosphere, it does not have a unique direction. The total radiation
is the sum of the beam and diffuses radiation and is sometimes referred to as the
global radiation. When the amount of diffuse radiation reaching the earth’s surface is less than or equal to 25% of global radiation, the sky is termed as clear sky
(Duffie and Beckman 1991).
In many applications of solar energy, the solar irradiance incident on the surface
of the earth at the location of interest is an important input parameter. The temporal
and spatial fluctuations of such irradiance necessitate a method to predict them.
M.M. Khan
Mechanical Engineering Section, University Polytechnic, Aligarh Muslim University,
Aligarh, 202002 Uttar Pradesh, India
e-mail: [email protected]
M.J. Ahmad
Department of Mechanical Engineering, Zakir Husain College of Engineering
and Technology, Aligarh Muslim University, Aligarh, 202002 Uttar Pradesh, India
e-mail: [email protected]
B. Jamil (*) Heat Transfer and Solar Energy Laboratory, Department of Mechanical Engineering, Zakir
Husain College of Engineering and Technology, Aligarh Muslim University,
Aligarh, 202002 Uttar Pradesh, India
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_13
149
The systematic variation of solar irradiance outside the earth’s atmosphere makes it possible to introduce many models for such prediction (Munroe 1980).
Knowledge of global solar irradiance at a site is essential for the proper design
and assessment of solar energy conversion systems. Some of the systems such as
concentrating systems require information on direct beam component whereas in
the case of tilted plain surfaces the diffuse component of solar irradiance is also
important for the computation of system performance (Khogali et al. 1983). How-
ever, at locations on the Earth’s surface, the solar radiation is also a function of variables such as the nature and extent of cloud cover, the aerosol and water vapor
content of atmosphere, etc. Good prediction of the actual value of solar irradiance
for a given location requires, in principle, long-term, average meteorological data,
which are still scarce for many developing countries like India (Leung 1980;
Ezekwe and Ezeilo 1981; Khogali 1983). It is, therefore, not always possible to
predict the actual value of solar irradiance for a location of interest.
There are several formulae available in literature on solar radiation modelling
that relate global radiation to climatological parameters such as sunshine hours,
relative humidity, maximum temperature, and average temperature. The first such
correlation proposed for estimating the monthly average daily global irradiation is
due Angstrom (1924). The original Angstrom-type regression equation relates
monthly average daily radiation to clear day radiation at the location in question
and average fraction of possible sunshine hours:
H=Hc ¼ aþ b S So
� � ð13:1Þ
A basic difficulty with Eq. (13.1) lies in the ambiguity of the terms S/So and Ho.
Page (1961) modified the method to base it on extraterrestrial radiation on a
horizontal surface rather than on clear sky day radiation.
H=H0 ¼ a0 þ b0 S So
� � ð13:2Þ
Inspite of having complication in Hc calculations, better results were obtained
using Hc instead of H0 (To�grul 1999). The major objective of this article to investigate usability of clear sky radiation to predict and express the average
measured values of solar irradiance on a horizontal surface by using various
regression analyses for selected locations in India.
Clear Sky Solar Radiation
Hottel (1976) has presented a method for estimating the beam radiation transmitted
through clear atmospheres which takes into account zenith angle and altitude for a
standard atmosphere and four climate types. The atmospheric transmittance for
beam radiation is given in the form:
150 M.M. Khan et al.
τb ¼ ao þ a1exp �k cos θzð Þ ð13:3Þ
The constant and k for the standard atmosphere with 23 km visibility are found
from ao*, a1* and K* which are given for altitudes less than 2.5 km by
a*o ¼ 0:4237� 0:00821 6� Að Þ2 ð13:4Þ a*1 ¼ 0:5055þ 0:00595 6:5� Að Þ2 ð13:5Þ K* ¼ 0:2711þ 0:01858 2:5� Að Þ2 ð13:6Þ
where, A is the altitude of the observer in kilometers.
The correction factors are applied to ao*, a1* and K* to allow for changes in climate types.
The correction factors ro¼ ao/ao*, r1¼ a1/a1* and rk¼ k/K* are given in Table 13.1.
Thus, the transmittance of this standard atmosphere for beam radiation can be
determined for any zenith angle and any altitude up to 2.5 km. The clear sky beam
radiation (Gcb, W/m 2) is than
Gcb ¼ Gonτb ð13:7Þ
where, Gon is the extraterrestrial radiation, measured on the plane normal to the
radiation on the nth day of the year and given in the following form (W/m2).
Gon ¼ Gsc 1þ 0:33 cos 360n 365
� �� � ð13:8Þ
where, Gsc is the solar constant equal to 1367 W/m 2.
The clear sky horizontal beam radiation is
Gcb ¼ Gonτb cos θz ð13:9Þ
It is also necessary to estimate the clear sky diffuse radiation on a horizontal
surface to get the total radiation as suggested by Liu and Jordan (1960). They
developed an empirical relationship between the transmission coefficients for beam
and diffuse radiation for clear days.
Table 13.1 Correction factors for different climates
Climate type r0 r1 rk
Tropical 0.95 0.98 1.02
Midlatitude summer 0.97 0.99 1.02
Subarctic summer 0.99 0.99 1.01
Midlatitude winter 1.03 1.01 1.00
13 Development of Models for the Estimation of Global Solar Radiation Over. . . 151
τd ¼ 0:271� 0:294τb ð13:10Þ
where τd is the ratio of diffuse radiation to the extraterrestrial radiation on the horizontal plane. The clear sky diffuse radiation Gcd (W/m
2).
Gcd ¼ Gonτd cos θz ð13:11Þ
Thus, the clear sky global solar radiation is given by
Gc ¼ Gcb þ Gcd ð13:12Þ
Meteorological Data
In the present study, the monthly average global solar radiation, have been calcu-
lated, using sunshine hour data on horizontal surfaces. Six models have been
developed which include the effect of latitude and altitude of a location. These
six stations have been selected for different geographical locations covering most
part of India (Table 13.2).
The measured values of the monthly average global solar radiation (G) and the
S/So ratio for six locations are obtained from Chandel et al. (2005) and are provided
in Table 13.3. Gc values calculated by Hottle’s model for six cities are given in Table 13.4.
Development of Models
The following equations were obtained by investigating the relation between G/Gc and S/So by different regression analysis. The scatter of monthly mean values
between G/Gc and S/So are given in Fig. 13.1.
Table 13.2 Geographical location of six Indian cities (Chandel et al. 2005)
Station (State) Longitude (�E) Latitude (�N) Altitude (m) Palampur (Himachal Pradesh) 76.30 32.60 1270
Amritsar (Punjab) 74.87 31.63 234
Kodaikanal (Tamil Nadu) 77.47 10.23 2339
Nandi Hill (Karnatka) 77.68 13.37 1479
New Delhi (Delhi) 77.20 28.58 216
Shillong (Meghalaya) 91.88 25.57 1600
152 M.M. Khan et al.
T a b le
1 3 .3
M ea su re d v al u es
o f m o n th ly
av er ag e g lo b al
so la r ra d ia ti o n (G
) an d S /S
o fo r si x ci ti es
(C h an d el
et al . 2 0 0 5 )
P al am
p u r
A m ri ts ar
K o d ai k an al
N an d i H il ls
D el h i
S h il lo n g
M o n th
G S/ S o
G S/ S o
G S/ S o
G S/ S o
G S/ S o
G S/ S o
Ja n u ar y
2 .8 0
0 .5 7
3 .1 0
0 .6 6
6 .2 8
0 .6 2
6 .3 7
0 .8 6
3 .9 9
0 .7 3
4 .0 1
0 .5 2
F eb ru ar y
3 .3 7
0 .5 5
3 .9 9
0 .6 9
6 .7 1
0 .6 7
6 .2 6
0 .8 1
5 .0 0
0 .8 1
5 .0 8
0 .6 5
M ar ch
4 .3 1
0 .5 8
4 .8 8
0 .6 3
6 .8 7
0 .6 3
7 .4 9
0 .8 4
6 .1 4
0 .6 9
5 .6 3
0 .6 8
A p ri l
5 .2 4
0 .6 5
6 .2 6
0 .7 3
6 .4 3
0 .5 5
7 .3 3
0 .8 0
6 .9 4
0 .6 8
5 .7 0
0 .6 2
M ay
6 .1 5
0 .6 9
6 .2 3
0 .6 5
5 .8 4
0 .4 1
7 .2 9
0 .6 2
7 .2 9
0 .6 0
5 .2 3
0 .5 3
Ju n e
5 .3 3
0 .6 0
6 .6 0
0 .7 4
5 .2 8
0 .2 7
6 .2 7
0 .3 3
6 .5 4
0 .4 3
4 .1 2
0 .3 3
Ju ly
3 .9 2
0 .2 9
6 .3 2
0 .6 3
4 .5 4
0 .2 0
4 .9 2
0 .2 9
5 .3 3
0 .4 3
4 .2 6
0 .3 9
A u g u st
4 .3 4
0 .3 3
5 .3 0
0 .6 5
4 .7 0
0 .3 2
5 .1 7
0 .3 2
5 .0 5
0 .4 3
4 .2 1
0 .3 5
S ep te m b er
3 .9 4
0 .5 3
5 .4 5
0 .7 1
4 .8 0
0 .3 3
4 .7 8
0 .3 6
5 .6 0
0 .5 7
3 .8 7
0 .4 1
O ct o b er
5 .0 8
0 .8 5
4 .4 7
0 .7 6
4 .4 4
0 .3 0
5 .6 6
0 .5 5
5 .3 6
0 .7 8
4 .0 2
0 .5 4
N o v em
b er
3 .6 1
0 .8 2
3 .7 1
0 .7 8
4 .7 4
0 .3 6
3 .4 7
0 .3 9
4 .5 2
0 .8 7
3 .9 4
0 .5 5
D ec em
b er
2 .7 6
0 .6 6
3 .0 1
0 .7 4
5 .2 2
0 .5 3
4 .3 8
0 .5 7
3 .8 4
0 .7 8
4 .1 5
0 .5 7
13 Development of Models for the Estimation of Global Solar Radiation Over. . . 153
G
Gc ¼ 0:7604 S
So
� � þ 0:3750 linearð Þ ð13:13Þ
G
Gc ¼ 0:0163 S
So
� �2 � 0:7424 S
So
� � þ 0:3794 quadraticð Þ ð13:14Þ
G
Gc ¼ �3:2664 S
So
� �3 þ 5:5108 S
So
� �2 � 2:1434 S
So
� � þ 0:8428 cubicð Þ
ð13:15Þ G
Gc ¼ 1:0742 S
So
� �0:4933 powerð Þ ð13:16Þ
Table 13.4 Calculated Gc values for each city (using Hottle’s Model) in kW/m 2/day
Months Palampur Amritsar Kodaikanal Nandi Hill Delhi Shillong
January 3.6401 3.3702 6.6410 6.0672 3.7228 4.6388
February 4.6831 4.3351 7.2561 6.7572 4.6764 5.6139
March 5.9138 5.4802 7.7983 7.4148 5.7955 6.7156
April 6.9983 6.4898 8.0260 7.7831 6.7738 7.6232
May 7.5867 7.0321 7.9153 7.7856 7.2861 8.0549
June 7.7606 7.1892 7.7717 7.6932 7.4271 8.1534
July 7.6540 7.0924 7.8044 7.7038 7.3364 8.0782
August 7.2133 6.6886 7.9330 7.7408 6.9578 7.7667
September 6.3071 5.8471 7.8448 7.5193 6.1472 7.0345
October 5.0445 4.6710 7.3853 6.9265 5.0007 5.9287
November 3.8828 3.5941 6.7671 6.2146 3.9439 4.8615
December 3.3433 3.0965 6.4305 5.8408 3.4459 4.3497
Fig. 13.1 G/Gc vs S/So for six cities in India
154 M.M. Khan et al.
G
Gc ¼ 0:3761ln S
So
� � þ 1:0401 logarithmicð Þ ð13:17Þ
G
Gc ¼ 0:4511exp0:989 SSoð Þ exponentialð Þ ð13:18Þ
Various statistical methods are available in solar energy literature, which deal
with the assessment and comparison of solar radiation estimation models (Stone
1993; To�grul 1999; To�grul and Onat 1999; Walpole and Mayers 1989; Şahin 2007). Presently, statistical tests, root mean square error (RMSE), mean bias error (MBE)
and t-statistics are utilized to evaluate the accuracy of the correlations developed.
Methods of Comparison
Statistical tests, root mean square error (RMSE) and mean bias error (MBE) were
used to evaluate the accuracy of the correlations developed. Also, t-statistics was
applied to the developed models to illustrate the statistically significant results.
Root Mean Square Error (RMSE)
The root mean square error is defined as
RMSE ¼ 1 N
XN i¼1
Gi,pre � Gi,meas � �2 !12 ð13:19Þ
where, Gi,pre is ith predicted value, Gi,meas is the ith measured value, andN is the total number of observations. The RMSE is always positive, a zero value is ideal. This test
provides information on short-terms performance of the correlation by arranging a
term by term comparison of the actual deviation between the calculated value and
the measured value. The smaller the value, the better the model’s performance, however, a few large errors in the sum can produce a significant increase in RMSE.
Mean Bias Error (MBE)
The mean bias error is defined as
MBE ¼ 1 N
XN i¼1
Gi,pre � Gi,meas � � ð13:20Þ
13 Development of Models for the Estimation of Global Solar Radiation Over. . . 155
This test provides information on the long term performance. A low value is
desired. Ideally a zero value of MBE should be obtained. A positive value gives the
average amount of over-estimation in the calculated value and vice versa. A
drawback of this test is that over estimation of an individual observation will cancel
under estimation in a separate observation.
It is obvious that each test by itself may not be an adequate indicator of a model’s performance. It is possible to have a large RMSE value and at the same time a small
MBE (a large scatter about the line of perfect estimation). On the other hand, it is
also possible to have a relatively small RMSE and a relatively large MBE
(a consistently small over or under estimation).
However, these statistical indicators generally provide a reasonable procedure to
compare models, they do not objectively indicate whether a model’s estimates are statistically significant, i.e. not significantly different from their measured counter-
parts. Therefore, an additional statistical indicator, the t-statistic is used. This
statistical indicator allows models to be compared and at the same time indicate
whether or not a model’s estimates are statistically significant at a particular confidence level. It was seen that the t-statistic used in addition to the RMSE and
MBE gave more reliable and explanatory results (Walpole and Mayers 1989).
t-Statistics
t ¼ N � 1ð ÞMBE 2
RMSE2 �MBE2 � �1
2
ð13:21Þ
The smaller the value of t, the better is the model’s performance. To determine whether a model’s estimates are statistically significant, one simply has to deter- mine a critical t-value obtainable from standard statistical tables, at a particular confidence level, i.e. tα/2 at an α-level of significance and (N-1) degrees of freedom. For the model’s estimates to be judged statistically significant at the (1-α) confi- dence level, the calculated t-value must be less than the critical t-value.
Results and Discussion
As observed from Table 13.5, good results were not seen in the short term (RMSE)
but relatively good results were observed in the long term performance (MBE).
Equation (13.17) has the best result among the equations developed.
When investigations were compared among all the equations the best MBE
value was seen in Eq. (13.17). The best RMSE value was obtained with
Eq. (13.15) which is a cubic equation.
156 M.M. Khan et al.
Also, it is observed that considering country as a whole and each city individ-
ually, the performance of developed equations is different. Therefore, the MBE and
RMSE values of the developed equations separately for each city were calculated.
The results of this statistical comparison are given in Table 13.6.
At the first view, it is seen that the MBE values of Table 13.4 are higher than
tabulated in Table 13.5 RMSE and MBE for the whole country (India). Each
equation developed for the city was compared with the equations in its group and
the results obtained were setup in order below (Table 13.7).
Although the models give overall good results for the whole country (Table 13.5)
but the errors were higher for individual cities (Table 13.6). These tables did not
include adequate information about on usability of the developed equation. In view
of this, t-statistics is applied to the developed models to investigate the usability of
each model. The critical t-values are shown in Table 13.8, t-values higher than the critical t-values show that the equation has no statistical significance.
Equations which have t-values lower than the critical t-value exhibited good and logical results. In case of Palampur, Eqs. (13.16) and (13.17) are significant. In case
of Amritsar and Kodaikan almost all of the equations showed good and logical
results. In case of Nandi Hills and Delhi Eqs. (13.13), (13.14) and (13.18) are
significant. In case of Shillong, Eqs. (13.15) and (13.18) are significant.
Conclusions
It was observed that the clear sky solar radiation and sunshine hour can be used to
estimate the global radiation in India. It was further observed that the cubic
equation gave the lowest RMSE error, and the lowest MBE error was obtained by
the logarithmic equation developed for the whole year (Table 13.5). It is also
observed that the performance of the equations is different for all the stations taking
together and for the cities individually. Cubic and logarithmic models gave the best
results among all the developed equations for the country as a whole. While for
individual cities cubic, logarithmic and exponentials yield better results.
Finally these results clearly indicate that reliance on the RMSE and MBE used
separately can lead to a wrong decision in selecting the best model suited from the
candidate models and that the use of the RMSE and MBE in isolation is not an
adequate indicator of model performance. Therefore, the t-statistics should be used
in conjunction with these two indicators to evaluate a model’s performance in a better way.
Table 13.5 RMSE and MBE for the whole country (India)
Equation number RMSE MBE
13.13 0.5726 �0.0222 13.14 0.5723 �0.0227 13.15 0.5662 �0.0233 13.16 0.5869 �0.0496 13.17 0.6096 �0.0192 13.18 0.5711 �0.0511
13 Development of Models for the Estimation of Global Solar Radiation Over. . . 157
T a b le
1 3 .6
T h e R M S E an d M B E v al u es
o f th e eq u at io n d ev el o p ed
fo r ea ch
ci ty
P al am
p u r
A m ri ts ar
K o d ai k an al
N an d i H il ls
D el h i
S h il lo n g
E q u at io n
R M S E
M B E
R M S E
M B E
R M S E
M B E
R M S E
M B E
R M S E
M B E
R M S E
M B E
1 3 .1 3
0 .5 9 9 2
0 .4 9 4 5
0 .2 1 6 2
�0 .0 6 9 9
0 .3 7 9 6
�0 .2 5 5 2
0 .5 6 4 5
�0 .1 0 2 8
0 .7 3 7 3
�0 .6 4 2 4
0 .7 4 4 8
0 .4 4 2 8
1 3 .1 4
0 .5 9 7 7
0 .4 9 3 8
0 .2 1 6 4
�0 .0 7 1 1
0 .3 7 9
�0 .2 5 4 7
0 .5 6 4 3
�0 .1 0 1 6
0 .7 3 8 5
�0 .6 4 3 1
0 .7 4 4
0 .4 4 0 8
1 3 .1 5
0 .6 2 1 3
0 .1 1 7 3
0 .2 1 3 7
�0 .0 0 6 7
0 .3 5 3 7
�0 .2 0 7 5
0 .5 6 3 4
�0 .1 5 4 8
0 .7 5 4 3
�0 .6 7 0 9
0 .6 9 3 1
0 .4 0 3 1
1 3 .1 6
0 .5 9 8 8
0 .1 1 1 5
0 .2 3 0 1
�0 .1 0 2 3
0 .4 3 3
�0 .2 9 4 1
0 .5 7 5 7
�0 .1 6 7 3
0 .7 5 2 7
�0 .6 6 6
0 .7 5 4 9
0 .4 5 9 4
1 3 .1 7
0 .6 4 9 5
0 .1 1 9 4
0 .2 2 7 5
�0 .0 7 2 9
0 .4 9 8 4
�0 .2 9 0 6
0 .5 8 6 4
�0 .1 6 0 8
0 .7 1 7 1
�0 .6 2 7 7
0 .8 0 6
0 .5 3 0 7
1 3 .1 8
0 .5 5 1 5
0 .1 0 9 1
0 .2 2 7 3
�0 .1 0 1 1
0 .3 9 9 8
�0 .2 8 2 6
0 .5 8 2 3
�0 .0 8 9 7
0 .7 7 6 5
�0 .6 6 8 6
0 .7 0 6 4
0 .3 7 2 9
158 M.M. Khan et al.
Nomenclature
A Altitude (km)
a, b, a’, b’ Empirical constants Gc Clear sky global solar radiation (W/m
2)
Gcb Clear sky beam radiation (W/m 2)
Gcd Clear sky diffuse radiation (W/m 2)
Gon Extraterrestrial radiation (W/m 2)
Gsc Solar constant (¼1367 (W/m2)) H Monthly mean daily global radiation on a horizontal surface (MJ/m2) Hc Clear sky monthly mean daily global radiation on a horizontal surface
(MJ/m2)
Ho Monthly mean daily extraterrestrial radiation (MJ/m 2)
n Day of the year N Number of observations S Monthly average daily hours of bright sunshine So Monthly average of maximum possible daily hours of bright sunshine
(i.e. day length of average day of the month)
Greek Symbols
α Level of significance θz Zenith angle (�) τb Atmospheric transmittance for beam radiation
Table 13.7 Equations with significant results for selected
stations
Station Equation number
Palampur 13.18
Amritsar 13.15
Kodaikanal 13.15
Nandi Hills 13.15 and 13.18
Delhi 13.17
Shillong 13.15 and 13.18
Table 13.8 Critical t-values and the results of t-statistics analyses for each city
Equation Palampur Amritsar Kodaikanal Nandi Hills Delhi Shillong
13.13 4.8466 1.1332 3.012 0.6143 5.8881 2.4523
13.14 4.8633 1.1538 3.0099 0.6071 5.875 2.4392
13.15 4.4236 0.104 2.4026 0.9478 5.4541 2.3712
13.16 4.2603 1.6462 3.0693 1.0073 6.2982 2.5436
13.17 4.1172 1.1219 2.3803 0.9457 6.0041 2.9015
13.18 5.1024 1.6471 3.3142 0.5171 5.6157 2.0614
Critical t 4.2658 1.2702 3.1036 0.7687 5.979 2.4175
13 Development of Models for the Estimation of Global Solar Radiation Over. . . 159
τd Atmospheric transmittance for diffuse radiation ω The sunset hour angle (�) ϕ Latitude (�) δ Declination angle (�)
References
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radiation on horizontal surfaces using sunshine hour and temperature data for indian sites.
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Ezekwe, G. I., & Ezeilo, C. C. O. (1981). Measured solar radiation in a Nigerian environment
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160 M.M. Khan et al.
Chapter 14
Effect of Gap Between Absorber Plate and Condenser Cover on the Performance of a Solar Still
Basharat Jamil and Naiem Akhtar
Introduction
Availability of fresh water for domestic and industrial use is an important issue
facing the human world today. Lack of potable sources of water in developing
countries is even severe. Rise is pollution levels of the local surface water resources
have worsened the conditions leading to fatal water borne diseases and conse-
quently an increase in human mortality rate.
Although several methods to purify water are available in industry, but most of
them involve high energy requirements and are technologically complicated, thus,
require sophisticated personnel for operation. Therefore, it is required that simple
yet effective methods of water purification/desalination must be developed to
reduce dependence on conventional energy resources.
Solar energy is a capable prospect for utilization in solar-energy conversion
systems. This can be exploited to heat and evaporate brackish or polluted water
which can later be condensed to form purified water suitable for drinking. Distil-
lation is one of the important methods of making clean and potable water from
brackish or polluted water using the abundant energy supply from the sun. Forma-
tion of clouds and rains in the atmosphere of earth is an example of desalination
cycle using solar energy to produce huge amounts of pure water from the sea.
B. Jamil (*) • N. Akhtar Heat Transfer & Solar Energy Laboratory, Department of Mechanical Engineering,
Zakir Husain College of Engineering and Technology, Aligarh Muslim University,
Aligarh, 202002 Uttar Pradesh, India
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_14
161
Conventional Solar Still
A solar still is a promising device for the desalination of brackish water into potable
form. The schematic diagram of conventional single slope solar still is shown in
Fig. 14.1. A solar still imitates the process of desalination through which the earth’s atmosphere forms rain. Water is heated through incoming solar radiation in a closed
chamber with an inclined transparent glass cover to form vapours. The vapours
travel through the chamber height to reach the inclined condensing cover and lose
heat to form liquid water. The condensed liquid water trickles on the condensing
cover and falls in the collection trough. The condensed liquid produced is usually
highly purified and free of microorganisms and other harmful bacteria. This is
because only heated water evaporates leaving behind the salts and other dissolved
impurities. Also, temperatures within the solar still reaches sufficiently high values
to kill the microorganisms and bacteria present in polluted water.
Although the construction, operation, and maintenance of a solar still is quite
simple but the main limitation of a simple solar still is its low output (yield) and
efficiency of the order of 2 lt/m2/day and 20–30% respectively (Tiwari and Tiwari
2006). A large number of research activities around the world address the perfor-
mance improvement and evaluation of solar stills.
Heat Transfer in a Solar Still
Heat transfer in a conventional solar still can be categorized in two parts: internal
heat transfer and external heat transfer (Tiwari and Tiwari 2007). Internal heat
transfer in a solar still consists of three modes viz; convection, radiation and
evaporation heat transfers.
Fig. 14.1 Schematic diagram of conventional single slope solar still
162 B. Jamil and N. Akhtar
The incoming solar radiation heats the blackened absorber of the solar still. Heat
is transferred from the heated absorber plate to the water in basin and from vapors to
inner surface of glass cover by convection. Radiative heat exchange occurs between
water interface and glass surface. Evaporative heat transfer occurs due to mass
transfer of vapors from the basin to inner surface of glass cover. While the external
heat transfer refers to heat exchange between the solar still and the surrounding
atmosphere. This consists of convection and radiation heat transfers. Heat is
transferred through convection between the glass cover and the ambient; and
bottom and side insulations and ambient. Radiative heat exchange occurs between
glass cover and sky. Heat transfer interactions of a solar still and the relationships to
model these mathematically are presented below.
Factors Affecting Performance of Solar Still
Meteorological parameters (such as solar intensity, ambient temperature and wind
velocity etc.), design features (such as slope of condensing cover, different cover
materials, various absorber material and their thickness and aspect ratio of absorber,
thickness of insulation etc.) and operational parameters (such as input water
temperature, effect of water depth, orientation of still etc.) have been extensively
studied and presented in literature for different designs under local operating
conditions of environment for various locations (Refalo et al. 2014). However,
meteorological parameters cannot be controlled. On the other hand design features
and operational parameters can be optimized for better yield from the solar still.
Some important studies related to factors that affect the performance of a solar still
are discussed below.
Manokar et al. (2014) presented an extensive review of factors affecting the
rate of evaporation and condensation on passive solar still. They reported that the
rate of evaporation is dependent on basin construction materials, depth of water in
basin, absorption rate of basin water, absorption rate of still basin, volumetric heat
capacity of the basin, inlet temperature of water and temperature of top surface
water. They also reported that the condensation rate is affected by glass cover
temperature and wind speed. As the wind velocity increases the cover temperature
decreases and hence an increase in the overall yield is observed (Dimri
et al. 2008). In other word, convective heat transfer increases with increase in
wind velocity.
A cover inclination equal to the latitude angle of the site help receive sun rays
close to normal throughout the year was reported by Murugavel et al. (2008).
Studies conducted on the effect of water depth in stills have shown that the highest
outputs and efficiencies occur at lower depths (Nafey et al. 2000).
14 Effect of Gap Between Absorber Plate and Condenser Cover on the Performance. . . 163
Performance Gap
It was observed from thorough literature review that although several solar still
designs are analysed in literature but the effect of distance (or gap) between the
absorber plate and the condensing cover has never been properly addressed. Only a
single study concerned with 2-D simulation study performed by Rahbar and
Esfahani (2013) reported that when the specific height of the solar still decreases,
the distance between the glass-cover and water-surface also decreases. This
enhances the convective heat transfer and, therefore, the condensation rate of
water-vapor increases. This is an important parameter since the distance between
the absorber plate and the condensing cover directly affect the amount of solar
radiation incident on the absorber plate. Also, the formation of water vapours in the
cavity is greatly affected. The distance vapours travels from the heated water
surface in absorber basin to condensing cover determines the yield of the solar
still. Hence, this distance (or gap) has to be experimentally analysed for optimum
solar still design.
Experimental Setup and Procedure
Fabrication of Solar Still
In this work, a conventional single slope solar still is designed and analysed for
desalination of brackish water. Solar still was fabricated using locally available
materials. Solar still is made out of Galvanised Iron (GI) sheet of 22 gauge. The
area of the absorber plate is 1 m2, with an aspect ratio of 2:1. Glass wool insulation
of 1 in. is provided around all the sides and bottom of the solar still to avoid heat
losses. The basin was painted black to maximize the absorption of solar radiation
in the solar still. Ordinary glass of 5 mm thickness forms the condensing cover
with the inclination of 28� (approximately equal to latitude of Aligarh City, 27.88�). Aluminium frame is used to support the glass cover over the solar still cavity and silicon sealant is used to fix the glass to the aluminium frame. An
aluminium trough is fixed along the lower edge of the condenser cover to collect
the condensate trickling from the inclined glass cover. Finally, a flexible rubber
tube transfers the condensate (distillate) to the collection bottle. Every possible
effort is made to make the solar still leak proof. The experimental setup was
aligned in a way so that the glass cover faces the exact south direction to receive
maximum solar radiation. Figure 14.2 shows the clear view of the experimental
setup (conventional solar still) and Fig. 14.3 gives the dimensional details of the
absorber/water basin.
164 B. Jamil and N. Akhtar
Instrumentation
• Temperatures were measured using T-type (copper-constantan) thermocouples.
Thermocouples were used to measure temperatures of absorber, water,
air-vapour mixture, glass inner and outer surface and ambient air. The output
of the thermocouples was read on a digital multimeter.
• Global solar radiation was measured using Kipp and Zonen Pyranometer
(CMP-11) and diffused solar radiation was measured using CMP-11 with
CM-121B shading ring. Difference of the two provides the beam radiation.
Global and diffused solar radiation values were stored in LOGBOX SD
datalogger.
Fig. 14.2 Actual view of experimental setup (conventional solar still)
Fig. 14.3 Details of absorber basin
14 Effect of Gap Between Absorber Plate and Condenser Cover on the Performance. . . 165
• Wind speed was observed using Precision AM804 CPM/CMM vane-type digital
anemometer.
• A borosil measuring flask with a least count of 1 ml was used to measure the
yield of distilled water from the solar still.
Observations
Experiments were conducted at Department of Mechanical Engineering, Aligarh
Muslim University, Aligarh (27.88�N, 78.08�E), Uttar Pradesh, India. The exper- iments have been conducted during the month of March 2015 on clear days under
similar conditions of environment.
Experiments were firstly conducted to investigate the depth of water. Solar
radiation, wind velocity and atmospheric temperatures were measured. The tem-
peratures, solar radiation intensity, wind speed and the distillate yield were
observed from morning 8 a.m. to evening 5 p.m.
A separate absorber plate was also fabricated for the solar still so that it can be
adjusted to effectively change the distance between the absorber and condenser
cover. The separate absorber can be raised from the bottom to change the height of
vapour chamber while the condensing cover remains fixed at top of the solar still.
Effect of varying the gap between absorber and condensing cover of the solar still is
presently analysed. The yield was analysed in terms of productivity of fresh water
per unit area of the absorber plate. Regular cleaning of deposits in the basin and
cleaning of dust on glass cover was taken care to maintain radiation absorption in
the absorber and transparency properties of glass respectively.
Results and Discussion
The first set of experiments was performed to verify the depth of water for
maximum water distillation in solar still. Figure 14.4 shows the measured temper-
ature of basin or absorber, water, air-vapours mixture and average glass tempera-
tures for different depths of water.
It is observed that the water temperature rises rapidly in case of lower depths and
gradually at higher depths. Also the highest temperature attained shows a phase
shift in case of higher depths.
Figure 14.5 shows the hourly and cumulative yield for different depths of water.
The variation of metrological parameters viz., solar radiation (global, diffused and
direct), ambient temperature and wind speed on the day of experiments are also
depicted.
It can be observed that the meteorological parameters were similar on the days of
experiment. The effect of increasing the depth of water in the basin has been
166 B. Jamil and N. Akhtar
analysed. It can be observed that increasing the depth of water in the basin reduces
the productivity (or yield) of the solar still.
Figure 14.6a shows the comparison of cumulative distillate yield for three
different depths of water Hw ¼ 1 cm, 2cm and 3cmð Þ. The observed cumula- tive yield during the day is 1260 ml, 1045 ml and 635 ml respectively. In other
words, twice the depth of water reduces the yield by 17.06% and thrice the depth of
water reduces the yield by 49.60%. This can be attributed to the higher amount of
energy required for heating and further evaporating a larger mass of water in the
basin. In other words, total specific energy requirement of the basin water increases.
Thus, it is verified that lower level of water should be kept in basin for better yield.
The distillation process continue even after the experiments were stopped
(at 5 p.m.) due to available thermal energy within the solar still. The distilled
Fig. 14.4 Comparison of temperature variation during the day for different depths of water (a) absorber or basin (b) water (c) vapour and (d) glass
14 Effect of Gap Between Absorber Plate and Condenser Cover on the Performance. . . 167
water collected between evening 5 p.m. to 7 a.m. the next morning (known as
“overnight productivity”) was also observed. It was found that increasing the
depth of water in the basin increases the overnight productivity (Fig. 14.6b).
But the amount of overnight distillate is small in comparison to daytime distillate.
Therefore, the total yield is still greater at lower depth of water. The observed
values of overnight distilled water were 30 ml, 55 ml, 96 ml for
Hw ¼ 1cm,ð 2cm and 3 cmÞ respectively. The second set of experiments was performed to investigate the effect of
distance between absorber plate and condenser cover on the performance of the
solar still. For this purpose a separate absorber was fabricated in the form of water
tray of approximately the same dimensions as the original absorber of the solar still.
This secondary absorber or water tray was then raised from the bottom with the help
of 1 in. thick polystyrene sheets as shown in Fig. 14.7. This effectively changes the
Fig. 14.5 Yield (hourly and cumulative) of distilled water for different depths of water in the basin along with observed solar radiation, ambient temperature and wind speed
168 B. Jamil and N. Akhtar
average distance between the absorber and condensing glass cover (H), thereby
reducing the height of vapour chamber.
Experiments were performed with different gaps as shown in figure above with
each time raising the absorber (or water tray) from the base by 1 in. Thus, H1
(¼15 in.) forms the first experiment with the largest distance between absorber and condenser cover and H4 (¼12 in.) forms the last experiment of the set with smallest distance between the absorber and condenser. For each experiment 1 cm depth of
water was maintained in the water tray throughout the experiment. Figure 14.8
shows the measured absorber, water, air-vapour mixture and glass temperatures for
different gaps between the absorber and condenser.
It can be observed that at the largest gap (H1), the observed temperatures are the
lowest while at the smallest gap (H4) the observed temperatures are the highest.
Fig. 14.5 (continued)
14 Effect of Gap Between Absorber Plate and Condenser Cover on the Performance. . . 169
Also, all the temperature curves show a similar trend with peak temperatures
between 12 p.m. to 1 p.m.
Figure 14.9a shows the observed hourly distillate yield for various gaps and
Fig. 14.9b compares the cumulative productivity of the solar still with different
gaps. It can clearly be observed that reducing the gap improves the distillate yield
significantly. This can be attributed to higher rate of convective heat transfer. As the
heated water surface and comparatively cooler glass surface comes closer the rate
of distillation increases. Therefore an increase in productivity is observed on
reducing the gap.
Observed yield at H1, H2, H3 and H4 are 1260 ml, 1964 ml, 2312 ml and
2695 ml respectively. Therefore, an increase of 55.87% (for H2), 83.49% (for H3)
and 113.88% (for H4) is observed in comparison to the base case (H1).
Fig. 14.5 (continued)
170 B. Jamil and N. Akhtar
Conclusions
A conventional single slope solar still was designed, fabricated and analysed for
desalination of brackish water. Initially, the effect of water depth was investigated.
It was found that increasing the depth of water in the basin of solar still decreases
the daytime productivity or yield. Also it was observed that the overnight produc-
tivity of the solar still increases with increase in water depth. These results verified
the investigations of previous researchers. Next, the effect of reducing the gap
Fig. 14.6 Comparison of (a) hourly cumulative yields (b) overall daytime, overnight and total yields at different depths of water
Fig. 14.7 Gap between absorber and condenser
14 Effect of Gap Between Absorber Plate and Condenser Cover on the Performance. . . 171
between absorber and condenser cover was experimentally evaluated. It was found
that reducing the gap increases the daily productivity. Reducing the gap increases
the convective heat transfer between the water surface and condenser cover.
This distance or gap is important because it directly affects the overall yield of
the solar still. It is believed that the results obtained under this study are valuable for
future solar still designs and optimization of heat and mass transfer processes
involved.
Fig. 14.8 Temperatures of (a) absorber or basin (b) water mass (c) air-vapour mixture (d) glass at different gaps between absorber and condenser
172 B. Jamil and N. Akhtar
References
Dimri, V., Sarkar, B., Singh, U., & Tiwari, G. (2008). Effect of condensing cover material on yield
of an active solar still: An experimental validation. Desalination, 227, 178–189. Manokar, A. M., Murugavel, K. K., & Esakkimuthu, G. (2014). Different parameters affecting the
rate of evaporation and condensation on passive solar still-A review. Renewable and Sustain- able Energy Reviews, 38, 309–322.
Murugavel, K., Chockalingam, K. K. S., & Srithar, K. (2008). Progresses in improving the
effectiveness of the single basin passive solar still. Desalination, 220, 677–686. Nafey, A. S., Abdelkader, M., Abdelmotalip, A., & Mabrouk, A. (2000). Parameters affecting
solar still productivity. Energy Conversion and Management, 41, 1797–1809. Rahbar, N., & Esfahani, V. (2013). Productivity estimation of a single-slope solar still: Theoretical
and numerical analysis. Energy, 49, 289–297. Refalo, P., Ghirlando, R., & Abela, S. (2014). The effect of climatic parameters on the heat transfer
mechanisms in a solar distillation still. Heat Transfer Engineering, 35(16-17), 1473–1481. Tiwari, A., & Tiwari, G. (2006). Effect of water depths on heat and mass transfer in a passive solar
still: In summer climatic condition. Desalination, 195, 78–94. Tiwari, A., & Tiwari, G. (2007). Thermal modeling based on solar fraction and experimental study
of the annual and seasonal performance of a single slope passive solar still: The effect of water
depths. Desalination, 207, 184–204.
Fig. 14.9 (a) Hourly yields for different gaps (H) between absorber and condenser cover. (b) Corresponding cumulative productivity
14 Effect of Gap Between Absorber Plate and Condenser Cover on the Performance. . . 173
Chapter 15
Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative Analysis for Natural Working Fluids
€Onder Kizilkan, Sandro Nižetić, and Gamze Yildirim
Introduction
The steam Rankine cycle is one of the most important ways to transform on large
scale thermal energy into power. Because of its good properties, water is the most
suitable working fluid for high temperature applications and large centralized
systems. Seeking for small and medium scale power plants, the problems encoun-
tered with water can be partially mitigated by selecting an appropriate fluid.
Organic compounds characterized by higher molecular mass and lower critical
temperature than water have been proposed in so called Organic Rankine Cycles
(ORC) (Tchanche et al. 2011). ORC, as a method of low grade heat utilization can
rise the energy utilization by conversion of heat into electric energy
(He et al. 2012). There are lots of low temperature practices in which the ORC
can be used such as solar thermal, biomass geothermal oceanic, waste heat from
power plants, combined heat and power, waste heat from industrial processes, etc.
(Peris et al. 2015).
The development of solar assisted power plants is becoming more crucial
because of effects of fossil fuels. For this reason, there is a need to improve existing
technologies integrated with solar energy. These systems offer better advantages
Ö. Kizilkan • G. Yildirim (*) Department of Energy Systems Engineering, Faculty of Technology,
Süleyman Demirel University, 32200 Isparta, Turkey
e-mail: [email protected]; [email protected]
S. Nižetić Department of Thermodynamics and Heat Engines, Faculty of Electrical
and Mechanical Engineering and Naval Architecture,
University of Split, R. Boskovica 32, 21000 Split, Croatia
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_15
175
when compared traditional energy sources. Parabolic trough solar collector
(PTSC) technology is considered the most established solar thermal technology
for power generation. Therefore, this technology has been chosen for this study
(Al-Sulaiman 2013).
Organic Rankine Cycle (ORC) as a promising energy transformation technology
has been the focus of many investigators (Kerme and Orfi 2014). Over the last
decades, significant researches have been carried out in the field of ORC systems.
Dai et al. (2009) studied ORC for low grade waste heat recovery using various
fluids. They examined thermodynamic parameters of the ORC for every working
fluid. They concluded that the cycle with R236EA had the highest exergy perfor-
mance. He et al. (2012) recommend a theoretical model to check out optimal
evaporation temperature of subcritical ORC. In a different study, organic Rankine
cycle and supercritical Rankine cycle for the transformation of low-grade heat into
electrical power investigated by Chen et al. (2010). They analysed 35 different
fluids for two cycles and analysed the effects of the selected fluid characteristics on
the cycle performance. Wang et al. (2013) conducted a regenerative ORC to make
use of the solar energy over a low temperature series. They used flat-plate solar
collectors to collect the solar radiation for their low costs. Lee et al. (2012) inves-
tigated the impact of changing the proportion of the cooling water to the condenser
on the performance of the ORC. They used R245fa in their analysis. Shengjun
et al. (2011) studied performance comparison of the fluids in subcritical and
transcritical ORC power cycle in 80–100 �C binary geothermal power system. They conducted the analyses with a program in MATLAB for thermal efficiency,
exergy efficiency, recovery efficiency, heat exchanger area and levelized energy
cost. Thermodynamic optimization of ORCs for power generation combined
heating and power from different average heat source profiles researched by
Maraver et al. (2014). Vélez et al. (2011) investigated the use of a low temperature
heat source for power generation a carbondioxide transcritical power cycle theo-
retically. They reported that the efficiency have been increased by the use of an
additional internal heat exchanger. Franchini et al. (2013) carried out simulations to
estimate the performance of a solar Rankine Cycle and an integrated solar com-
bined cycle. They combined the system with two different solar field configurations
based on parabolic trough and power tower systems.
In this study, solar energy driven ORC is investigated thermodynamically for
different natural refrigerants. For collecting the solar energy, PTSCs are used
because of their good advantages. For the analyses of ORC, eight natural working
fluids and a HFC type fluid are considered including, R170 (ethane), R1270
(propylene), R600 (butane), R600a (isobutene), R717 (ammonia), R744
(carbondioxide), R161 (fluoroethane), R218 (octofluoropropane), and a HFC type
fluid, R134a. Analyses are made to examine the system performances energetically
and exergeticaly. An attempt is also made to evaluate the exergy destruction rates in
order to determine how to improve the process. Furthermore, a comprehensive
performance assessment of the integrated system is conducted through parametric
analysis to investigate the effects of changing operating conditions on the system
efficiencies.
176 Ö. Kizilkan et al.
Natural Refrigerants and System Description
Natural refrigerants provide alternatives to a number of HCFC, CFC and HFC type
refrigerants in addition to their zero ozone depletion potential (ODP) and low or no
global warming potential (GWP) (Bolaji and Huan 2013). They are naturally
occurring substances, such as hydrocarbons, ammonia, carbon dioxide, water and
air. These substances can be used as cooling agents (heat transfer medium) in
refrigerators and air conditioners (Refrigerants naturally 2015).
The general properties of the previously mentioned working fluids are given in
Table 15.1 (ASHRAE 2004; Restrepo et al. 2008; Calm and Hourahan 2011).
In the table, critical properties of the fluids are obtained using EES software
(F-Chart 2015). As seen from the table, the selected natural refrigerants have zero
ODP and relatively very small GWP values excluding R218 and R134a. Addi-
tionally, their atmospheric life times are relatively short. In spite of this, it must
be noted that some natural refrigerants such as R170, R1270, R600, R600a and
R161 are in A3 safety group which means they are highly flammable. Besides,
R744, R218, R134a are belonged to A1 group that means they are
non-flammable. The last fluid, R717, is in the lower flammability group with
higher toxicity.
The ORC consists of four compounds: a turbine, an evaporator, a condenser and
a pump. Required heat energy for the evaporator of the ORC is supplied by means
of PTSCs. Therminol-VP1 is for the PTSC system as the heat transfer fluid (HTF),
for its good heat transfer properties and good temperature control (Therminol
2014). Because of its good properties, it is used in many high temperature applica-
tions driven by PTSC such as power plants (Kumar and Reddy 2009; Vogel
et al. 2014; Cheng et al. 2012; Al-Sulaiman 2014). The system operates as follows:
The liquid organic working fluid from condenser is compressed by the pump and
fed back to the evaporator, where it is heated by the useful heat delivered by the
solar PTSCs, and becomes superheated vapor. The superheated vapor then enters to
the turbine and expands to a low pressure. Subsequently, the turbine exhaust is
intensified to liquid in the condenser by extracting heat to the environment and the
cycle completes when the fluid is compressed by the pump. The schematic repre-
sentation of the system and the T–s diagrams of the case study are given in
Figs. 15.1 and 15.2 respectively.
In Fig. 15.2, there are two T–s diagrams, where the first one is for subcritical
and the second one is transcritical cycle. In subcritical cycle, the system properties
are under the critical values and in transcritical cycle, the heat absorption process
takes place above the critical values where heat rejection process takes place
below the critical values. For the second case, the gas heater placed instead of
evaporator.
15 Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative. . . 177
T a b le
1 5 .1
P ro p er ti es
o f th e se le ct ed
w o rk in g fl u id s
A S H R A E n u m b er
M o le cu la r fo rm
u la
C ri ti ca l
p re ss u re
(k P a)
C ri ti ca l
te m p er at u re
(� C )
S af et y
g ro u p
O D P (r el at iv e
to R 1 1 )
G W P (r el at iv e
to C O 2 )
A tm
o sp h er ic
li fe
ti m e (y ea r)
R 1 7 0
C H 3 C H 3
4 8 7 2 .2
3 2 .1 7 2
A 3
0 2 0
0 .2 1
R 1 2 7 0
C H 3 C H ¼C
H 2
4 6 6 4 .6
9 2 .4 2 0
A 3
0 3
0 .0 0 1
R 6 0 0
C H 3 C H 2 C H 2 C H 3
3 7 9 6 .0
1 5 1 .9 7 5
A 3
0 2 0
0 .0 1 8
R 6 0 0 a
C H (C H 3 ) 3
3 6 4 0 .0
1 3 4 .6 6 7
A 3
0 2 0
0 .0 1 9
R 7 1 7
N H 3
1 1 ,3 3 3
1 3 2 .2 5
B 2
0 0
0 .2 5
R 7 4 4
C O 2
7 3 7 7 .3
3 0 .9 8
A 1
0 1
1 2 0
R 1 6 1
C H 3 C H 2 F
5 .0 9
1 0 2 .2 0
A 3
0 1 2
0 .1 8
R 2 1 8
C F 3 C F 2 C F 3
2 .6
7 1 .9 5
A 1
0 8 8 3 0
2 6 0 0
R 1 3 4 a
C H 2 F C F 3
4 0 5 9 .0
1 0 1 .0 3 0
A 1
0 .0 0 0 0 1 5
1 4 1 0
1 4
178 Ö. Kizilkan et al.
Thermodynamic Analysis
The performance of the solar driven ORC is mathematically modelled using mass,
energy and exergy balance equations. Some assumptions are made in order to find
the work and heat interactions, the rate of exergy destructions, and the energy and
exergy efficiencies. These are as follows:
• All the processes in the system are steady state and steady flow.
• The changes in potential and kinetic energies are neglected.
• The turbine and pumps are adiabatic.
• The heat transfer to/from ambient and pressure drops in the pipes are neglected.
Fig. 15.1 Schematic representation of solar assisted ORC system (modified from Volker 2015)
T T
ss
a b
Fig. 15.2 T–s diagrams for ORC (a) subcritical (b) transcritical
15 Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative. . . 179
• The natural fluid at pump inlet is saturated liquid.
• The dead state pressure and temperature are taken to be P0¼ 101.325 kPa and T0¼ 25 �C.
• The pinch point temperature of the evaporator and condenser/gas heater are
taken as 10 �C (Al-Sulaiman 2014).
The general mass balance equation can be written as (Cengel and Boles 2006):X _m in ¼ X
_m out
ð15:1Þ
where m is the mass flow rate, subscripts in and out are entering and exiting streams
to and from the system, respectively.
The general energy balance X _E in ¼ X
_Eout ð15:2Þ
For steady-flow processes the general energy balance can be written in more
detail as:
_Q þ X
_m in hin ¼ _W þ
X _m out hout ð15:3Þ
In above equations, Ein is the ratio of net energy transfer to the system, Eout is
the ratio of net energy transfer from the system, Q is the ratio of net heat, W is the
ratio of net work, and h is the specific enthalpy.
The rate of useful energy delivered by solar collector is (Tiwari 2003;
Kalogirou 2009)
_Qu ¼ FR SAa � ArUL Ti � T0ð Þ½ � ð15:4Þ
_Qu ¼ _mcp T0 � Tið Þ ð15:5Þ
where FR is the heat removal factor, S is the solar irradiation, Aa is the aperture area,
Ar is the receiver area, UL is the overall heat loss coefficient of solar collector,
subscripts i, o and 0 are inlet, outlet and dead state, respectively.
The heat removal factor, FR can be calculated from (Kalogirou 2009)
FR ¼ _mCp ArUL
1� exp �ArULF 0
_mCp
� �� � ð15:6Þ
where F’ is the collector efficiency factor and given by
F0 ¼ U0 UL
ð15:7Þ
180 Ö. Kizilkan et al.
In Eq. (15.7), U0 is the overall heat transfer coefficient. Based on PTSC
properties, U0 and UL can be determined from (Kalogirou 2009):
U0 ¼ 1 UL
þ Do hfDi
þ Doln
Do Di
2k
0 @
1 A
2 4
3 5 �1
ð15:8Þ
UL ¼ Ar hc,c�a þ hr,c�að ÞAg þ
1
hr, r�c
� ��1 ð15:9Þ
In above equations, hc,c-a is the convection heat loss coefficient between ambient
and the cover, hr,c-a is the radiation heat transfer coefficient for the glass cover to the
ambient, hr,r-c is the radiation heat transfer coefficient between the receiver tube and
the glass cover and hf is the heat transfer coefficient of fluid inside the tube.
Additionally, D is the tube diameter and Ag is the glass cover area. The definitions
of heat transfer coefficients mentioned above can be found in reference Kalogirou
(2009) in more detail.
The general exergy balance equation can be defined as (Dincer and Rosen 2007):X _Exin ¼
X _Ex
out þ X
_Ex dest
ð15:10Þ
The exergy balance equation can be expressed more explicitly as:
_ExQ � _ExW � X
_m in ein �
X _m out eout þ T0 _Sgen ð15:11Þ
where, ExQ and ExW terms are the exergies of heat and work, e is the specific
exergy, T0 is the dead state temperature and Sgen is the rate of entropy generation.
The exergy terms in Eq. (15.11) are described below (Dincer and Rosen 2007):
_Exdest ¼ T0 _Sgen ð15:12Þ
_ExQ ¼ _Q T � T0 T
� � ð15:13Þ
_ExW ¼ _W ð15:14Þ
The specific exergy can be expressed as (Cengel and Boles 2006; Bejan 1997):
e ¼ h� h0ð Þ � T0 s� s0ð Þ ð15:15Þ where, s is entropy, and subscript 0 stands for dead state properties.
The exergy of the solar radiation in terms of reference and sun’s temperature is given by Petela (2005):
15 Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative. . . 181
_Exsolar ¼ SAa 1þ 1 3
T0 Tsun
� �4 � 4 3
T0 Tsun
� � ! ð15:16Þ
where Tsun is the temperature of sun’s surface and assumed as 5739 K (Tiwari 2003).
The energy and exergy efficiencies are described below (Dincer and
Rosen 2007):
η ¼ _WORC _QE
ð15:17Þ
ηex ¼ _Exout _Exin
¼ 1� _Exdest _Exin
ð15:18Þ
Results and Discussion
For the thermodynamic analyses of the solar driven ORC, the system parameters for
baseline conditions are given in Table 15.2. System characteristics of solar assisted
ORC Table 15.2.
Using the general balance equations given in previous section, the analyses were
made for the base line conditions first. According to data given in Table 15.2,
the turbine power generations for different working fluids are given in Fig. 15.3.
Table 15.2 System characteristics of solar assisted ORC
PTSC system (Al-Sulaiman 2014;
Kalogirou 2009)
Pipe receiver inner diameter 0.04 m
Pipe receiver outer diameter 0.05 m
Glass cover diameter 0.09 m
Total length of PTSC 50 m
Mass flow rate of HTF 0.32 kg/s
Receiver emissivity 0.92
Glass cover emissivity 0.87
Temperature of the sun 5739 K
Absorbed solar radiation 500 W/m2
Wind velocity 5 m/s
ORC Turbine isentropic efficiency 0.85
Pump isentropic efficiency 0.90
Evaporator temperaturea 50 �C Condenser temperature 27 �C Turbine inlet temperature 150 �C
aTurbine inlet pressure of ORC is determined from saturation pressure corresponding to evaporator
temperature excluding R170 and R744, since the critical properties of these fluids are below from
the specified values
182 Ö. Kizilkan et al.
As seen from the figure, ORC working with R744 has the highest power generation
capacity and followed by R170, R717 and R161.
Figures 15.4 and 15.5 show the energy and exergy efficiencies of ORC for
different working fluids according to the energy and exergy analysis. As seen
from Fig. 15.4, the best energy performance is obtained using R744 with an energy
efficiency of 8%, whereas the lowest energy efficiency belongs to R218 with an
efficiency rate of 4.3%. The exergy efficiency results show that the highest
efficiency is found to be 7.1% with R744 and followed by R170 and R717.
A comparison of the calculated exergy destruction rates of the solar assisted
ORC is given in Fig. 15.6. As seen from the figure, R218 has the highest exergy
destruction rate and followed by R600a, R600 and R134a. The lowest exergy
destruction rate is found to be 75.33 kW using R717.
Fig. 15.3 Comparison of net power generation for different natural refrigerants
Fig. 15.4 Comparison of energy efficiencies of ORC for different natural refrigerants
15 Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative. . . 183
In Fig. 15.7, exergy destruction in the heat transfer process between the HTF and
the working fluid in the evaporator is given. As mentioned earlier, Therminol-VP1
was used as HTF and its properties were kept constant during the calculations.
Therefore, the differences between exergy destruction of evaporator is mainly
depends on the working fluid properties. From the figure, it can be seen that the
lowest exergy destruction rate in the evaporator is found to be 16.55 for R170,
followed by R218 and R744 where evaporator of R717 has the highest exergy
destruction with 19.41 kW.
Through parametric analyses, a comprehensive performance assessment of the
integrated system was conducted to investigate the effects of varying operating
conditions on the system efficiencies. For the parametric analyses, the variable
parameters were selected to be solar radiation intensity, turbine inlet temperature,
Fig. 15.5 Comparison of exergy efficiencies of ORC for different natural refrigerants
Fig. 15.6 Comparison of exergy destruction rates of ORC for different natural refrigerants
184 Ö. Kizilkan et al.
and normalized pressure at the turbine inlet and condenser temperature. Figure 15.8
shows the variation of solar radiation intensity with turbine power generation. As
seen from the figure, turbine power generation increases with increase of solar
radiation from 350 to 800 W/m2.
Turbine inlet temperature also affects the cycle performance characteristics. To
determine the variation of turbine inlet temperature on energy and exergy efficien-
cies, it was varied between 70–150 �C (Figs. 15.9 and 15.10). As seen from the figures, with the increase of turbine inlet temperature, energy and exergy efficien-
cies increase for R717. For the working fluids R744, R170, R134a, R600, R600a
and R218, the efficiencies decrease whereas they are not affected so much for R161
and R1210 with the temperature.
Figure 15.11 shows the variation of turbine inlet temperature with the total
exergy destruction rate of the system. As seen from the figure, the trend is contrary
Fig. 15.7 Comparison of exergy destruction rates of evaporator for different natural refrigerants
Fig. 15.8 Variation of net power generation with solar radiation
15 Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative. . . 185
Fig. 15.9 Variation of turbine inlet temperature with energy efficiency
Fig. 15.10 Variation of turbine inlet temperature with exergy efficiency
Fig. 15.11 Variation of turbine inlet temperature with exergy destruction rate
186 Ö. Kizilkan et al.
to energy and exergy efficiency variation. The total exergy destruction rate
decreases with increasing the turbine inlet temperature for R1270, R717, R744,
R170, it increases for R600a, R134a, R600, R218 and R161.
The condensation temperature is also one of the important parameter for assess-
ment of the system performance. To determine its effect on system performance, it
was changed from 25 �C to 30 �C and energy, exergy efficiencies and exergy destruction rates were calculated (Figs. 15.12, 15.13 and 15.14). The results are
showed that, the energy and exergetic efficiencies decrease with the increase of the
condenser temperature for all working fluids except for R744 and R170. This result
is interesting since these two fluids are transcritical fluids. On contrary to this, the
total exergy destruction rate increase with the temperature, while for R744 and
R170 it decreases.
As declared in Table 15.2 at the beginning of this section, working pressures of
solar assisted ORC were determined according to the corresponding saturation
Fig. 15.12 Variation of condensation temperature with energy efficiency
Fig. 15.13 Variation of condensation temperature with exergy efficiency
15 Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative. . . 187
temperatures of evaporator for subcritical working fluids. For transcritical fluids,
the pressures were determined from the literature. Since the pressure values
of each working fluid differs from each other, they were normalized and the
figures were plotted using normalized pressure ranges for better understanding
of the results.
Figures 15.15 and 15.16 show the variation of energy and exergy efficiencies
with normalized turbine inlet pressure. It is very clear from the figures that with the
increase of turbine inlet pressure, efficiencies increase, too.
The effect of normalized turbine inlet pressure on the exergy destruction is given
in Fig. 15.17. From the figure, exergy destruction rates decrease with the turbine
inlet pressure since the exergy destruction rate is inversely proportional to the
energy and exergy efficiencies.
Fig. 15.14 Variation of condensation temperature with exergy destruction rate
Fig. 15.15 Variation of normalized turbine inlet pressure with energy efficiency
188 Ö. Kizilkan et al.
Conclusions
A comparative analysis of solar assisted Organic Rankine Cycle for power gener-
ation using natural working fluids was investigated. The analyses were carried out
for environmentally friendly subcritical and transcritical natural working fluids.
The heat energy demand of the ORC was supplied using PTSCs working with
Therminol-VP1 as the heat transfer fluid. From the results it was observed that the
best cycle performance was obtained using R744 with a power generation rate of
4.87 kW and followed by R170, R717 and R161. Energy analysis results showed
that the best cycle had an energy efficiency of 8% using R744 as working fluid. The
exergy efficiency of the same cycle was found to be 7.1%. The highest total exergy
destruction rate was found to be 76.98 kW for R218. Additionally, the effects of
turbine inlet temperature, turbine inlet pressure and condensation temperature on
Fig. 15.17 Variation of normalized turbine inlet pressure with exergy destruction rate
Fig. 15.16 Variation of normalized turbine inlet pressure with exergy efficiency
15 Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative. . . 189
system performance were analysed for different working fluids. This study points
out that natural refrigerants are compatible with ORC power generation systems
and more detailed experimental studies should be carried out for green energy
production assisted by solar energy.
Nomenclature
Aa Aperture area, m 2
Ag Glass cover area, m 2
Ar Receiver area, m 2
Cp Specific heat, kJ/kg K
D Tube diameter, m
e Specific exergy, kJ/kg _E: Energy, kW
_E x Exergy, kW
F’ Collector efficiency factor
FR Heat removal factor
h Specific enthalpy, kJ/kg
hc,c-a Convection heat loss coefficient between ambient and the cover, kW/m 2K
hr,c-a Radiation heat transfer coefficient for the glass cover
to the ambient, kW/m2K
hf Heat transfer coefficient of fluid inside the tube, kW/m 2K
hr,r-c Radiation heat transfer coefficient between the receiver tube
and the glass cover, kW/m2K
ṁ Mass flow rate, kg/s _Q: Heat, kW
s Specific entropy, kJ/kg K _S: Entropy, kW/K
S Solar irradiation, kW/m2
T Temperature, �C or K UL Overall heat loss coefficient, kW/m
2 K _W: Work, kW
U0 Overall heat transfer coefficient, kW/m 2 K
Greek Letters
η Efficiency
Subscripts
dest Destruction
gen Generation
190 Ö. Kizilkan et al.
i Inlet
o Outlet
u Useful
0 Dead state
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192 Ö. Kizilkan et al.
Chapter 16
Rainfall Trend Analysis in the Region of Curitiba Using Regional Climate Model Scenarios
Robinson Ploszai and Miriam Rita Moro Mine
Introduction
The climate change studies in hydrological time series have a great scientific and
practical importance in water management. In general, the water resources systems
are designed assuming that the hydrological data series (streamflow or precipita-
tion) are statistically stationary (Alexandre et al. 2010).
The operational management of water resources is predicted assuming the
hydrologic stationarity. According to Matalas (1997), the designers are uncertain
about how the global warming can be converted in a hydrologic non-stationarity
and how this non-stationarity could be incorporated into water resources
management.
In the context of climatic changes in hydrological time series, it is not possible to
assume whether these changes are related to anthropogenic causes (e.g., land uses
changes or greenhouse gas emissions) or to natural climate variability, which is a
consequence from multi annual or secular cycles in the Earth’s climate (Tucci 2002).
Applying a probabilistic method in a large hydrological time series (e.g.,
100 years or more with the minimum gaps or incorrect data), it is possible to
identify changes in the time series, even if these changes are cyclical or related to
trends. These changes do not distinguish the natural effects from anthropogenic
effects.
To detect trends in time series, several studies have been performed worldwide
(Coscarelli and Caloiero 2012; Li et al. 2011; Sayemuzzaman and Jha 2014;
Oguntunde et al. 2011; Wang et al. 2008; Liang et al. 2011; Stipp et al. 2013;
Fisch and Folhes 2006; Romano et al. 2011; Meschiatti et al. 2012; among others).
R. Ploszai (*) • M.R.M. Mine Federal University of Parana, PO Box 19011, 81531-990 Curitiba, PR, Brazil
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_16
193
According to these authors, the most efficient methods in trends detection are the
Mann Kendall and Seasonal Mann Kendall tests and linear regression.
Statistical methods in both time series: the measured monthly precipitation and
the rainfalls generated by Regional Climate Models (RCM) were applied. This
paper verifies whether the RCM simulations can reproduce the historical period
data and analyses precipitation trends through 2100 in the region of Curitiba to
develop tools that will allow safety measure criteria to be taken for water resources
management.
Methods
According to Kundzewicz and Robson (2000), before performing any statistical
analysis, such as the application of a test or a method, it is necessary to do the
Exploratory Data Analysis (EDA) on the preliminary data. These authors state that
an analysis trend study is incomplete if the EDA is not used.
The EDA consists in using graphics and other heuristic methods to explore,
understand and represent the information. Several methods are used to evaluate
trends in time series, such as histograms and your relation with the normal proba-
bility distribution, temporal and autocorrelation graphs, normality tests, and serial
independence tests and analysis of the smoothing curves (Kundzewicz and Robson
2000). Linear regression is a powerful tool to evaluate the existence of a secular
trend in hydrological variables. The linear regression method in this case is
represented by Eq. (16.1)
yt ¼ b1 � tþ b0 þ Et ð16:1Þ
where t is a time counter ðt ¼ 1, 2, . . . , nÞ; yt is the hydrological variable (precip- itation) on time t; b1 is the angular coefficient of the regression’s line; b0 is the linear coefficient of the regression’s line; and E assumes the errors of the regression. After assuming some hypothesis and that the error E is normally distributed, the param- eters b1 and b0 are estimated by Ordinary Least Squares, solving the Gauss’s normal equations (Johnson 1984).
Adopting the residuals of the linear regression as normally distributed, this
hypothesis can be tested using the t-test, well described in Sharma et al. (2000).
According to Alemaw and Chaoka (2002), another important tool to detect possible
trends in hydrological time series is the Rescaled Adjusted Partial Sums (RAPS)
method. According to these authors, the sum of a RAPS represented in a function Y
(t) is defined by Eq. (16.2).
Xk ¼ Xk t¼1
YðtÞ � Y SY
ð16:2Þ
194 R. Ploszai and M.R.M. Mine
where the value of k ¼ 1, 2, . . . , n. The variable Xk is the RAPS at limit k; Y(t) is the value of the variable at time t; Y is the mean of the sample values; SY is the
sample’s standard deviation; and k is the counter limit of the actual sum. The significance of RAPS analysis and EDA can be tested through the application of
statistical tests, such as a t-test and a Fisher-Snedecor test for annual analysis and
the Mann Whitney test and rho’s Spearman coefficient test for seasonal analysis. These tests are fully described in Tozzi (2014).
Other tools were used (statistical indexes), such as the Nash-Sutcliffe
(NS) coefficient, the index Root-Mean-square-Error (RMSE), and the determina-
tion coefficient (R2). All methods are well described by Moriasi et al. (2007),
Hyndman and Koehler (2006), and Naghettini and Pinto (2007), respectively. To
evaluate the significance of the time series, the mean, median, variance, standard
deviation, kurtosis excess, and asymmetry of the series under a confidence interval
of 95% were all estimated.
A common and practical issue in analysing hydrological time series consists in
finding statistical techniques to verify the occurrence of some variation along the
period (Buishand 1984). In order to do that, some statistical methods, such as the
Mann Kendall test and Seasonal Mann Kendall test, were applied to analyse trends
in hydrological time series.
The Mann Kendall and Seasonal Mann Kendall tests are largely used to verify
homogeneity in hydrological time series. According to Back (2001), Barros
et al. (2011), Buchir (2013), and Müller et al. (1998), the Mann Kendall test
application is the most powerful in analysing climatic changes from climatological
time series because it allows the beginning of the trend can be detected.
The Mann Kendall test consists in comparing each value in a chronological time
series with the residuals, always ordered on the time. Hence, the number of times
that the result terms are lower than the analysed terms is counted. The statistics of
the MK test (SMK) are given by Eq. (16.3).
SMK ¼ Xn j¼1
Xn i¼jþ1
signal Rj � Ri � � ð16:3Þ
where n is the number of observations; Ri is the previous observation; Rj is the latest
observation; i is the position of Ri at the previous time; j is the position of Rj at the
latest time. The signal is defined through conditions, as represented by Eq. (16.4)
signal Rj � Ri � � ¼ 1, if Rj � Ri > 00, if Rj � Ri ¼ 0
�1, if Rj � Ri < 0
8< : ð16:4Þ
It is possible to apply the Mann Kendall test to investigate trends on time series,
only if the series has shown serial independence. Therefore, the series observations
are tested to see if they are independent and identically distributed, in other words,
to check the hypothesis:
16 Rainfall Trend Analysis in the Region of Curitiba Using Regional Climate. . . 195
H0: The series observations are independent and identically distributed; H1: The
series observations have some trends along the period.
It is possible to show under a null hypothesis that S_MK is normally distributed
with null mean, according to Eq. (16.5). The statistic is calculated by Eq. (16.6)
EðSMKÞ ¼ 0 and VARðSMKÞ ¼ n� ðn� 1Þ � ð2nþ 5Þ 18
ð16:5Þ
MK ¼
SMK � 1ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi VAR SMKð Þ
p , if SMK > 0 0, if SMK ¼ 0
SMK þ 1ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi VAR SMKð Þ
p , if SMK < 0
8>>>>< >>>>:
ð16:6Þ
Even for values lower than 30, it is possible to use the statistics MK ¼ Z to do the test. In a bilateral test, the null hypothesis, H0, is rejected given a 95% significance
interval α, in the case of the quartile values Zα/2, pursuing a normal standard distribution, or MK � Zα=2.
The Seasonal Mann Kendall was proposed by Hirsch et al. (1982) and later was
improved by Hirsch and Slack (1984). It has been created due to the difficulties in
facing seasonality’s climate events. This test is an adaptation of the Mann Kendall’s test. It is an alternative to control the difficulties imposed by the high observational
seasonal variabilities (Buchir 2013). According to Fisch and Folhes (2006), this test
is largely recommended by the World Meteorological Organization (WMO) in
detecting trends or abrupt changes in climate time series.
According to Lettenmaier et al. (1994) and Blain (2011), in the case of the
monthly series, the MKS can be calculated, organizing the data into a matrix. The
columns are filled with the series values, and the factor Tj is initially estimated for
each month. Then, the statistics are calculated using the same assumptions: the null
hypothesis H0, is rejected for a significance interval α equal to 95%. This method is fully described in Stipp et al. (2013).
Study Area and Data
The region of this work is the Curitiba city, Parana State, Brazil. The pluviometric
station is located at Centro Politécnico, in the High Iguassu River basin. This station
was chosen because of its location and because it is considered as a key station in
south Brazil. The station has a good length of the observational time series, in other
words, up to 100 years of extension (1889–2013).
Curitiba is the capital and the main city of the Parana state. It is considered the
eighth largest city of Brazil with more than 1.75 million people living in the city
(IBGE 2013). According to INMET (2013) and Fill et al. (1999), Curitiba has a
subtropical wet climate, with average temperatures between 11 �C and 23 �C, in the
196 R. Ploszai and M.R.M. Mine
winter and summer, respectively. These temperatures can oscillate according to
each epoch of the year. The annual average precipitation is around 1400 mm in
Curitiba; and the average of rainy days is 164 days per year. The relative moisture
of the capital is around 80.7%.
The pluviometric station Curitiba is situated in the Guabirotuba neighbourhood
of Curitiba. The station’s coordinates are 25�270S and 49�140E, and the average altitude is around 924 m. This station is shown in Fig. 16.1.
The rainfall records and the RCM’s outputs are used in this work. The historical records of the Curitiba station are used to compare and verify if the RCM’s outputs can represent the rainfall records in Curitiba, in the period from 1961 to 2008. The
observational data were collected at the Hydrological Information System
(Hidroweb), held by ANA (National Waters Agency, in Portuguese).
The observed data and the precipitation scenarios were split into two groups:
(1) Historical period is the rainfall observed at the Curitiba hydrological station and
the precipitation scenarios generated by three RCM (ETA, PROMES and RCA1);
(2) Future period is only the precipitation generated by the RCM. Based on the
project, CLARIS LPB was identified as the most representative models for the
region, the ETA, PROMES and RCA1 (Mine et al. 2009).
For the preliminary analysis, the total of annual and monthly precipitation and
the maximum and minimum values of the monthly rainfalls of RCM’s outputs and observed records were used. After the most representative model for the Curitiba
region was identified, the annual and seasonal total rainfall in each period were
analysed.
Fig. 16.1 Location of the main rivers, capital and the pluviometric station Curitiba
16 Rainfall Trend Analysis in the Region of Curitiba Using Regional Climate. . . 197
Preliminary Analysis
Both the historical time series, as the series generated by the RCM, were analysed in
order to identify the most representative scenario for the region of Curitiba. First of
all, the frequency bias correction method was applied as presented in Saurral
(2010). After the bias correction was performed, the gaps were set up both in
historical time series, as in RCM’s outputs. There were found 75 months and 24 months of gaps in the historical time series and ETA series, respectively. The
years with gaps were disregarded because the historical time series were
1491 months long.
Using the frequency polygons it was observed that the ETA model generates
better-simulated series, after the bias correction. The series generated by the RCA1
model were not as satisfactory as the PROMES series, both shown in Fig. 16.2a.
The rainfall permanence curves are presented in Fig. 16.2b. The periods to con-
struct the curves were the same for the observed and each simulated series (histor-
ical period).
Figure 16.2b shows the permanence curves for all precipitations (simulated and
observed). From the curves’ analysis, it is possible to conclude that the PROMES model does not represent the historical observed series. The analysis of the scenario
generated by the RCA1 model has shown a satisfactory adjustment (observed and
simulated data curves), but the ETA model is the most representative.
To finalize the analysis of the precipitation scenarios obtained by RCM simula-
tions, the descriptive statistics of monthly precipitation series were computed.
Table 16.1 indicates the ETA scenario as the most representative for the region,
when comparing to observed rainfall (OBS).
Regarding the scenario generated by the ETA model, both the mean and median
between the two samples were so close. The other indicators such as standard
deviation, kurtosis excess, and the asymmetry coefficient resulted in close values
Fig. 16.2 (a, b) Frequency polygons and permanence curves for all scenarios and models
198 R. Ploszai and M.R.M. Mine
between the observed rainfall (OBS) and the ETA outputs. The ETA simulations
were not efficient in representing the minimum rainfall records but were efficient in
representing the maximum records of each month (Table 16.1).
From all the previous analysis, the ETA model has shown the best results,
resulting in its being adopted as the most representative for the region for the
next analysis.
Annual Analysis
The precipitation scenario generated by the ETA model in this section was split into
two precipitation scenarios: ETA01, representing the historical period, and ETA02,
representing the future period. The observed rainfalls at the pluviometric station
called Curitiba were represented by OBS.
The common period in the scenarios ETA01 and OBS is limited to December
2008. The initial point for both series is centred in January 1961. There are gaps in
the OBS and ETA series. Therefore, the series were limited in 2008. The ETA’s gaps correspond to a period of about 24 months: January 2009 to December 2010.
The future period represented by ETA02 corresponds to the interval: January 2012
to November 2099. The last month obtained by ETA simulations is
November 2099.
In order to precede an initial analysis of the annual precipitations, the descriptive
statistics of the three precipitation scenarios: OBS, ETA01 and ETA02, were
calculated, as follow the results in Table 16.2. Table 16.2 shows that the ETA01
and OBS series have almost the same mean values as well as almost the same
medians and the standard-deviation indexes.
Comparing the statistics between these two scenarios, OBS and ETA01, it is
clearly showed that both minimum and maximum values of ETA01 have higher
Table 16.1 Statistical indexes of monthly precipitation during the historical period from 1961 to 2008
Statistics OBS ETA PROMES RCA1
N (months of precipitation) 564 576 576 576
Mean 122.48 123.36 114.07 121.18
Median 114.35 114.09 103.36 107.56
Standard-deviation 76.29 76.62 87.28 82.52
Kurtosis excess 1.48 1.24 11.83 8.29
Asymmetry 1.00 0.91 2.51 2.02
Minimum 2.00 0.25 1.09 5.71
Maximum 473.80 498.71 833.36 685.61
Nash-Sutcliffe coefficient – �0.51 �0.77 �0.67 RMSE – 93.78 103.78 98.41
R2 – 0.06 0.05 0.06
16 Rainfall Trend Analysis in the Region of Curitiba Using Regional Climate. . . 199
values than those represented by scenario OBS, according to Table 16.2. The
ETA02 scenario showed an increase of three statistical indexes: mean, median,
and standard deviation. It is possible to conclude that there is an increasing trend in
precipitation in the region.
Below are presented the temporal graphs of mean and median, with a variation
of about 10 years. Following that are the graphs using the linear regressions for all
scenarios (Fig. 16.3). As shown in Fig. 16.3a, the historical series has shown an
increasing trend throughout its length, according to the linear regression line, which
is slightly positive from the series beginning (1889) to the end (2008). This trend
can be visualized through the angular coefficient of the equation generated by the
linear regression’s line (positive signal). The smoothing curves (mean and median variation around 10 years) have shown
a slightly increasing trend in the end of the hydrological series. Figure 16.3b shows
that, in the ETA01 scenario, the trend at the period decreases for the techniques
mentioned in the legend. The angular coefficient of the linear regression line has
shown a decreasing trend (negative signal).
Figure 16.3c depicts an increasing trend on scenario ETA02. Analysing the
smoothing functions and linear regression technique shows an increasing trend in
rainfall. The smoothing functions, such as mean and median variation, have shown
a slightly positive trend.
The test of the linear regression coefficient for the precipitation series of the
three scenarios (OBS, ETA01, and ETA02) was applied in order to identify the
trend significance. As described in Sharma et al. (2000), this test was applied and
compared to the critical values obtained from t-test tables for the pre-specified
freedom degrees.
The null hypothesis to a given significance level at α ¼ 5% is H0 : b ¼ 0, and b is the angular coefficient of the linear regression line. The test results (Table 16.3)
showed a trend both in ETA01 and in ETA02 scenarios. From the initial analysis of
the angular coefficient and the test applied to this coefficient, it was shown that
there is an increasing trend (positive) in ETA02, when in ETA01 there is a
decreasing trend (negative).
The results of the coefficient test (Table 16.3) have not shown significant trends
at observational series (OBS). As follows, the graphs using the RAPS method were
Table 16.2 Descriptive statistics of the annual
precipitation
Statistics OBS ETA01 ETA02
N (months of precipitation) 43 48 88
Mean 1467.19 1480.30 1789.49
Median 1473.70 1434.95 1780.11
Standard-deviation 294.24 287.97 370.52
Kurtosis excess �0.17 1.93 �0.38 Asymmetry �0.10 1.05 0.22 Minimum 765.50 994.99 950.49
Maximum 2071.20 2497.80 2603.94
200 R. Ploszai and M.R.M. Mine
elaborated. The RAPS was applied in order to identify possible trends in all
scenarios, represented in Fig. 16.4.
From the RAPS graphs, an abrupt change in the OBS scenario was observed
(Fig. 16.4a). This point shows a possible change in the mean (possible trend) in the
year 1952, represented in Fig. 16.4a by year 54. The same behaviour was perceived
in Fig. 16.4b and c as a result of abrupt changes observed in the years 1982 (year 22)
and 1995 (year 35), represented in Fig. 16.4b and c, respectively.
In analysing Fig. 16.4c, an abrupt change is perceived in 2056 (47). These
changes do not prove the existence of a trend in the series (abrupt changes), but
show that these characteristics must be proven through the statistical tests
Fig. 16.3 (a–c) Total annual precipitated for all scenarios
16 Rainfall Trend Analysis in the Region of Curitiba Using Regional Climate. . . 201
application. These tests can help us visualize and analyse the significance of the
abrupt changes.
In order to consolidate the results obtained by the RAPS method application, a
graph with the total annual precipitation throughout each series was elaborated. The
function cumulative curve is represented by Fig. 16.5 for all scenarios (Fill
et al. 2008).
In analysing Fig. 16.5, there were no significant trends perceived in the OBS
series. However, at the end of the period, a slight increase in precipitation was
observed in the region. The same does not occur in the ETA01 scenario, in which
Table 16.3 Hypothesis test results of the angular coefficient of the linear regression line
Scenario Regression line equations R2 coefficient t t (tab.) H0 Trend
OBS y¼ 1.17xþ 1362.00 0.02 1.37 1.99 Accept H0 No ETA01 y¼ -6.15xþ 1630.90 0.09 2.12 2.02 Reject H0 Yes ETA02 y¼ 3.93xþ 1613.60 0.07 2.63 1.99 Reject H0 Yes
0.02
0.01
−0.01
−0.02
−0.03
−0.04
0
0.025
0.02
0.01
0.005
0
−0.005
0.015
0 0 10 20 30 40 50
0 10 20 30 40 50 60 70 80 90
20
OBS Null Line Null LineETA01
Null LineETA02
40 60
Year Year
Year
R A
P S
0.01
0
−0.01
−0.02
−0.03
−0.04
R A
P S
R A
P S
a
c
b
80 100
Fig. 16.4 (a–c) RAPS of annual amount precipitated for all scenarios
202 R. Ploszai and M.R.M. Mine
were found several fluctuations through the line. It is possible to visualize in
Fig. 16.5 that an increasing trend occurs in the year 2056, year 35 in Fig. 16.5.
In order to verify the significance of these alterations, the series were submitted
for statistical tests. To apply the statistical tests, the series were split at the exact
point of the abrupt changes identification, detected in RAPS, Cumulative Curves,
and Mid-division analysis. The results of the test applications are shown in
Table 16.4.
The mid-division method was applied according to studies of Tozzi (2014). The
following statistical tests were applied: t-test, Fisher-Snedecor (F), Mann-Whitney
or Wilcoxon (U), and Spearman’s rho coefficient. The t-test and F test were applied to annual analysis, whereas the U and rho coefficient to seasonal analysis.
Table 16.4 shows the results of the statistical test applications, such as the t-test
and F-Snedecor test. The results in Table 16.4 show the total number of rejections
per accepts on tests application in the same year as the abrupt changes were
observed. For example, on the RAPS method in the 1952 and OBS scenario,
Fig. 16.5 Cumulative curves for all precipitation scenarios
Table 16.4 Statistical test results t and F for the annual analysis
Rejections per Accepts quantity
Method RAPS
Scenario OBS ETA01 ETA02
Year 1952 1992 1982 1995 2023 2028 2058
Result 1_1 0_2 0_2 0_2 2_0 0_2 1_1
Method Cumulative curves
Scenario OBS ETA01 ETA02
Year 1905 1925 1975 1980 2025 2030 2035
Result 0_2 0_2 1_1 0_2 1_1 0_2 1_1
Method Mid-division
Scenario OBS ETA01 ETA02
Year 1950 – 1985 – 2055 – –
Result 1_1 – 1_1 – 1_1 – –
H0 Accept Accept Reject
16 Rainfall Trend Analysis in the Region of Curitiba Using Regional Climate. . . 203
one rejection per one accept (1_1), was observed and on the RAPS method in the
2023 and ETA02 scenario, two rejections per null accept (2_0) were detected. In the
same way, the results of the Cumulative Curves and Mid-division analysis for all
years showed in Table 16.4 can be interpreted.
The results in Table 16.4 show the presence of no significant trends in the
historical series (OBS) and in scenario ETA01 due to the number of rejections
being lower than the number of accepts in both scenarios throughout the years.
In the ETA02 scenario, rejections were higher than accepts, showing a presence
of trends. In order to consolidate the obtained results at the previous analysis, the
powerful Mann Kendall (MK) test was applied for the total annual precipitation, as
shown in Table 16.5. The average, maximum, and minimum precipitations of each
year were analysed for a better understanding of the annual precipitation patterns,
as can be seen in Table 16.5.
The null hypothesis was accepted for a given significance level of 5% in all
cases studies for the OBS scenario. Therefore, no trend was detected in the
historical period, according to the results of the MK test. Both scenarios generated
by the ETA model have shown significant trends, showing a higher rejects rate due
to lower accepts rate, according to the results shown in Table 16.5. This indicates a
trend presence in the series generated by the ETA model (scenarios ETA01 and
ETA02).
From the annual analysis, it can be concluded that the rainfall has presented
trends in some tests and analysis applied to scenarios OBS and ETA01. In the
historical series, increasing trends were identified after the analysis of the smooth-
ing curves, regressions, coefficients, and the application of statistical tests. The MK
test application has shown the presence of significant trends.
Seasonal Analysis
After the annual analysis, the precipitation scenarios were submitted to a seasonal
analysis. This analysis has occurred observing the monthly amount precipitated, by
splitting these amounts in two and four seasons. Splitting the series in two seasons,
as performed by Tozzi (2014) and Fill et al. (2008), the summer series were
considered in the period between November and April. Consequently, the spring
series were considered in the period between May and October.
Table 16.5 Annual precipitation analysis—Mann
Kendall test (α¼ 5%) Accept H0: Z (tab.)¼ 1.96
Annual period
OBS ETA01 ETA02
Situation Situation Situation
Total Accept H0 Reject H0 Reject H0
Maximum Accept H0 Accept H0 Reject H0
Minimum Accept H0 Reject H0 Accept H0
Average Accept H0 Reject H0 Reject H0
Trend No Yes Yes
204 R. Ploszai and M.R.M. Mine
Trimestral rainfalls were analysed by splitting the series by seasons of the year:
summer (December to February), autumn (March to May), winter (June to August),
and spring (September to November). In both the semi-annual and trimestral series,
the total precipitation in the period was analysed. The same methods were applied
in annual analysis. The results of all analyses are summarized in Table 16.6
(next section).
Results and Discussions
From the previous analysis, significant trends for the application of some tests were
present in graphical analysis of some statistical indexes for all scenarios
(Table 16.6).
No increasing trend was detected in the observational series for the annual and
trimestral analysis for the winter and spring seasons. Just two analyses have shown
the presence of trends in the OBS scenario. The OBS scenario shows an increasing
trend on the warmest months because more analyses have shown increasing trends
(positive) in this scenario. All tests and methods showed that in the ETA01 scenario
there are some decreasing (negative) trends on seasons corresponding to the coldest
months of the year. For the hottest months, the ETA01 scenario shows that the
precipitation is increasing at most of the applied tests. Some exceptions were
detected in the ETA01 scenario analysis as described in the last half of Table 16.6.
Table 16.6 Summarized results of all analysis
Station Period OBS ETA01 ETA02
Annual – " (2) (3) # All " All SEM—Summer NOV–APR " (2) (3) (6) " All " All SEM—Winter MAY–OCT " (2) (3) (6) # All " (1) (2) (3) (6) TRIM—Summer DEC–FEB " (2) (3) (6) " All " (1) (2) (3) (5) (6) TRIM—Autumn MAR–MAY " (2) (3) (5) (6) " (2) (3) (6) " (1) (2) (3) (4) (6) TRIM—Winter JUN–AUG " (2) (3) # All " (1) (2) (3) TRIM—Spring SEP–NOV " (2) (3) # All " (1) (2) (3) Monthly – " (2) (3) (5) (6) # All " All (1) Descriptive statistics analysis
(2) Functions and regressions analysis
(3) Line’s angular coefficient analysis
(4) Line’s angular coefficient test
(5) t-test and Fisher-Snedecor test or Mann-Whitney and Spearman’s rho tests
(6) Mann Kendall and Seasonal Mann Kendall tests
Exceptions Except by maximum statistics higher than (due to OBS)
Except by maximum statistics lower than (due to OBS)
Descriptive statistics (all lowers due to OBS)
16 Rainfall Trend Analysis in the Region of Curitiba Using Regional Climate. . . 205
The studied methods were efficient in identifying trends in historical and sim-
ulated data series; however, the application of Mann Kendall and Seasonal Mann
Kendall tests have shown to be better suited for trends identification than linear
regression analysis and EDA. This fact can be seen in Table 16.6 results, which
shows trends in almost all annual and seasonal analyses performed by the MK and
SMK tests. It is not proved the significance of trends in some scenarios through the
analysis of the linear regression line, because of the significance tests results
(presented by number 4 in Table 16.6), have not appeared in many analyses,
showing no significant trends in these cases.
In Table 16.6, increasing trends (positive) are shown to occur in almost all tests
and analyses applied to the ETA02 scenario. The inflexion of the Cumulative Curve
occurs in the year 2056. The curve’s inflexion depicts an increasing trend in rainfall in the region of Curitiba in 2056 year (according to the ETA02 scenario and
considering the RCM’s uncertainties).
Conclusions
The performed analyses in both the historical period and future period have allowed
the conclusion that the scenarios generated by the ETA model have presented the
best results for the region of Curitiba. The initial analysis has presented this model
as a better representative than the others (PROMES and RCA1 scenarios). For trend
analysis, the ETA model was adopted to study the rainfalls in Curitiba until
November 2099. Based on these studies, the future projections studies were
performed.
From the annual analysis, it is shown that, in some tests applied, an increasing
trend in rainfall was identified. This increasing trend is observed as positive through
the diagram Cumulative Curves, statistical indexes, and the regression analysis. To
proceed the semi-annual analysis, the series were split in two seasons (summer and
winter), as did Tozzi (2014). It has verified the presence of positive trends in the
summer precipitation series, whereas the winter season results were not conclusive.
At trimestral analysis (splitting in the annual seasons), the presence of significant
trends in the summer season were observed. In other seasons (applying the statis-
tical tests), significant trends in the series were not detected. For a better under-
standing of the precipitation patterns, a monthly analysis was performed that has
shown trends both in historical series and in the series generated by the ETA model.
Summarizing the results, the ETA model has shown the best results for the
analysis of precipitation in the region of Curitiba. The rainfalls generated by this
model have shown an increase in monthly precipitation around 18%, since 2012.
Meanwhile, when comparing the increase of 18% of monthly rainfall with the
RCM’s uncertainties, it is possible to conclude that this is just an indicative about the increasing trends of rainfall in the region of Curitiba until 2100.
According to the last IPCC (2013) report, it is shown that rainfall trends for the
future scenario (presented as ETA02 in this paper) are increasing. Based on data
206 R. Ploszai and M.R.M. Mine
generated by this RCM, it is possible to predict that rainfall in the region will
increase, and that it is possible to take some preventive measures toward planning
and managing water resources.
Acknowledgements We acknowledge the Superior Teaching People Improving Coordination (CAPES, in Portuguese) for the support developed in this work. We also acknowledge the National
Waters Agency (ANA, in Portuguese) and the CLARIS LPB Project for the data available for
using.
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208 R. Ploszai and M.R.M. Mine
Chapter 17
Modelling of Wind Speed Using Artificial Neural Networks for University Campus of Burdur (Turkey)
Alper Kerem, €Onder Kizilkan, and Serdar Salman
Introduction
Energy plays a significant role in the socio-economic development of a country.
The level of prosperity can be evaluated by the amount of energy which is
consumed by a nation (Pishgar-Komleh et al. 2015). In parallel to the worldwide
growing population and emerging technologies, the demand for electricity has been
increasing every year. While the growing demand of energy causes rapid consump-
tion of energy the sources, mankind has been focused on alternative energy
resources. The growing energy demand, rapidly decreasing country’s fossil fuel reserves, day by day increasing oil import cost and environment degradation have
required to utilize renewable sources of energy like wind energy to generate
electricity (Khahro et al. 2014).
According to some researchers, the rest of oil reserves are 225.4 billion tons,
natural gas reserves are 208.4 trillion m3 and coal reserves are 860.94 billion tons in
the world. The lifetimes are estimated as 54 years for oil, 64 years for natural gas
and 112 years for coal (Koc and Senel 2013). In 2013, Turkey’s electricity installed capacity was 64,000.4 MW. This value has increased progressively and reached to
A. Kerem (*) Department of Electricity and Energy, K. Vocational High School,
Osmaniye Korkut Ata University, Osmaniye, Turkey
e-mail: [email protected]
Ö. Kizilkan
Department of Energy Systems Engineering, Faculty of Technology,
Süleyman Demirel University, Isparta, Turkey
e-mail: [email protected]
S. Salman
Department of Metallurgical and Materials Engineering, Faculty of Technology,
Marmara University, İstanbul, Turkey
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_17
209
68,719.1 MW in 2014 as seen from Fig. 17.1 (EMO 2014). In 2013, Turkey’s electricity consumption increased by 1.3% compared to the previous year, and
attained 24,484 GWh (Energy Institute 2014). Therefore, Turkey is strictly depen-
dent on imported energy at an exceeding rate of 70%. In order to provide the
supply-demand balance, it is obvious that Turkey’s current energy resources must be assessed and should be increased in number and capacity of the native power
plants.
It is known that the solar energy transferred to the earth corresponds to energy
generated from 200 billion tons of coal per year. The amount of this energy equals
to 20 thousand times of the total energy consumption of the world (Hayli 2001). For
this reason, it is clear that the sun is a powerful source of energy. Wind energy is an
indirect form of solar energy which occurs from temperature and pressure differ-
ence. Due to increasing energy demand and resulting environmental problems
during electricity generation, wind energy can be considered as an attractive and
alternative renewable energy resource (Shamshirband et al. 2014). Wind is a clean
energy source which is natural and inexhaustible (Mohandes et al. 2011). It is
environmentally friendly alternative energy source without releasing CO2 gas to the
environment like fossil fuels (Monfared et al. 2009). Actually, this situation is a
chance for geographic regions which have favorable winds. So, in recent years it
has been drawn attention for energy production from wind energy in all over the
world. According to the research for Turkey, the total potential of wind energy was
determined to be 48 GW, using the wind speed data of above 7 m/s (ETKB 2014).
However, the total power of the wind farms established in Turkey is 3512 MW
(EMO 2014). This power value constitutes about 7–8% of Turkey’s total wind energy potential. Thereby, it is seen that a great deal of wind energy potential is
waiting to be evaluated.
Fig. 17.1 Electric power installed capacity in Turkey (EMO 2014)
210 A. Kerem et al.
In order to determine the wind power potentials, it is very important to measure
long term wind speed characteristics. Instead of this, modelling of wind speeds
using small data sets can be a good alternative for long term data. However the
modeling of wind speed is not easy because of its nonlinear nature and multiple
input and outputs. The long-term estimation problem predicts long-term wind
speeds at a target site in order to estimate the wind energy potential of wind
turbines. In general, long term wind data over several years is not available at the
target site (Jung and Kwon 2013). For forecasting the long term statistics of wind
speed, some new models were used such as Artificial Neural Networks (ANNs).
During the past years there has been a substantial increase in the interest on the
ANNs. Researches have been applying the ANN method successfully in various
fields of mathematics, engineering, medicine, economics, meteorology, psychol-
ogy, neurology, in the prediction of mineral exploration sites, in electrical and
thermal load predictions and in adaptive and robotic control and many other sub-
jects (Bilgili et al. 2007).
Several researchers investigated design and modeling of wind speed, wind
direction, wind turbine analyses using Artificial Neural Networks. Ekonomou
et al. (2012) developed an artificial neural network (ANN) model which has the
ability to estimate the optimal number of wind turbines and the total produced
power in a wind farm. Jiang and Lu (2014) developed an improved elastic back-
propagation neural network method to forecast system frequency. The effectiveness
of the proposed method was verified using field data from a real wind farm in
Guangdong, China. Tagliaferri et al. (2015) proposed two methods for short term
forecasting of wind direction with the aim to provide input for tactic decisions
during yacht races. They used two methods which were based on artificial neural
networks (ANN) and support vector machines (SVM), respectively. Fadare (2010)
modelled the profile of wind speed in Nigeria using artificial neural network
(ANN). The used ANN model consisted of three-layered, feed-forward, back-
propagation network with different configurations, designed using the Neural
Toolbox for MATLAB. Jung and Kwon (2013) applied the artificial neural network
(ANN) to predict long-term wind speeds of a particular site, and to estimate the
annual energy production of wind turbines using the predicted wind speeds.
Oztopal (2006) presented weighting factors of surrounding stations necessary for
the prediction of a pivot station by an artificial neural network (ANN) technique. He
also compared the wind speed prediction results with measured values at a pivot
station. Pourmousavi Kani and Ardehali (2011) used artificial neural network
(ANN) and Markov chain (MC) methods to develop a new ANN–MC model for
forecasting wind speed in very short-term time scale. They predicted very short-
term wind speed in a few seconds using the data patterns for short-term (about an
hour) and very short-term (about minutes or seconds).
In this study, wind speed potential of a university campus located in Burdur,
Turkey is modelled using Artificial Neural Networks. For this aim, a wind energy
measurement station is assembled in Mehmet Akif Ersoy University İstiklal Cam-
pus and data measuring-monitoring was made for 12 months. The measured data
were modelled with artificial neural networks to predict the long term wind
17 Modelling of Wind Speed Using Artificial Neural Networks for University. . . 211
parameters. Feed-forward backpropagation learning algorithm is used for the anal-
ysis with different hidden neuron numbers.
Artificial Neural Networks (ANNs)
The modeling of nonlinear systems is difficult and success has been restricted to
restrictive classes of nonlinear systems. The major application of artificial neural
network (ANN) is that they tender the potential of a generic approach to the
modeling of nonlinear systems (Yıldız and Uzun 2015). ANNs learn from exam-
ples, called patterns. In other words, to train and test a neural network, input data
and corresponding output values are necessary. A neural network usually consists
of an input layer, a number of hidden layers and an output layer. ANNs have been
used in a broad range of applications including; pattern classification, function
approximation, optimization, and prediction (Cam et al. 2005). ANNs can be
trained to overcome the limitations of the conventional approaches to solve com-
plex problems that are difficult to model analytically (Bilgili et al. 2007).
Commonly neural networks are adjusted, or trained, so that a particular input
leads to a specific target output. Such a situation is shown in Fig. 17.2. There, the
network is adjusted, based on a comparison of the output and the target, until the
network output matches the target. Typically many such input/target pairs are used,
in this supervised learning, to train a network (Sencan 2007; Kizilkan 2011).
Different learning algorithms can be applied in order to train a network. How-
ever, it is not easy to guess the fastest one for a given problem, and the best one is
usually determined by trial and error. The most popular of them is the
backpropagation algorithm, which has different variants. Standard backpropagation
is a gradient descent algorithm, in which the network weights are moved along the
negative of the gradient of the performance function. The term backpropagation
refers to the manner in which the gradient is computed for nonlinear multilayer
networks (Sencan and Kalogirou 2005).
In Fig. 17.3, the general architecture of a neural network unit is shown. Each
artificial neural unit consists of inputs (xn), weights (Wn), summation function (R),
activation function (a) and outputs (y). The figure illustrates how the information is
processed through a single node. The node receives weighted activations of other
nodes through its incoming connections. First, these are added up (summation). The
result is then passed through an activation function, the outcome being the activa-
tion of the node. For each of the outgoing connections, this activation value is
multiplied by the specific weight and transferred to the next node (Kalogirou 2000).
212 A. Kerem et al.
Study Field and Data Collection
Before establishing wind turbines for electricity generation, some data should be
determined such as wind speed, wind frequency (the frequency of wind blowing),
wind direction, the average temperature, pressure, etc. (Hayli 2001; Pishgar-
Komleh et al. 2015). In order to achieve these data, it is important to do a feasibility
study at first. Then, wind measurement stations should be established by determin-
ing the most convenient points and the measurements should be made for at least
12 months. Afterwards, data should be recorded, stored and analyzed (Akova 2008;
Ozerdem and Turkeli 2005; Genc et al. 2005; Sahin 2004). The measurements must
be carried out with a great attention and evaluation since an error of 10% in the
measured wind speed causes an error of 30% in generated power (Akova 2008).
Furthermore, investments which excess of measured wind power capacity return to
idle capacity and lead to increase energy production costs (Akova 2008; Demirci
and Senlik 2009).
Taking into consideration of the above mentioned concerns, first the coordinates
of study field was determined carefully in order to determine the wind energy
potential of Mehmet Akif Ersoy University İstiklal Campus. Wind speeds were
monitored at different points on the land for every minute. In accordance with the
Fig. 17.2 Representation of neural networks
Fig. 17.3 General architecture of neural
network unit
17 Modelling of Wind Speed Using Artificial Neural Networks for University. . . 213
criteria included in the literature, the most efficient land-coordinate considered was
determined by GPS system. So, measuring station and stretching ropes’ foundation were established on 1313 m altitude and coordinates of UTM E 263254 and N
4173479 (Figs. 17.4 and 17.5).
After the determining of the best suitable study field, the tower was built. The
height of the tower was 63 m in total with 21 modules which were 3 m in height.
Then, the relevant sensors were installed on the tower (Fig. 17.6).
Measurement tower was fed by 20 W solar panel and 12 V batteries in order to
make the measurements without a connecting of public electricity grid. Measured
data were recorded by a data logger at every 10 min and transferred to the project
Fig. 17.4 Measuring station and stretching ropes’ groundbreaking shape (Kerem et al. 2014)
Fig. 17.5 3D image of the field work (to scale)
214 A. Kerem et al.
team via GSM modem. Tower and sensors were protected against lightning by
grounding line. Furthermore, an aircraft warning light was mounted on the top of
the tower for protecting the system from undesirable situations. Measurements were
made for heights of 61 m and 31 m for every 10 min. The measured data were wind
speed at 61 m and 31 m, wind direction, temperature, pressure and humidity. The
data used in this study were wind speed at different elevations (Figs. 17.7 and 17.8).
Application of ANNs
The ANN parameters such as, the number of neurons in the input, hidden and output
layers, network architecture, transfer function, learning algorithm, momentum
factor and learning rate are to be selected for developing an ANN model. Proper
data selection also plays a major role in the success of ANN architecture used. The
number of neurons in the input layer is usually equal to the number of parameters
that affect the system performance (Mohanraj et al. 2015). For modelling the wind
speed potential of the university campus, one input and one output with different
number of neurons were tested. The input parameter is the months and the output
parameters are monthly average wind speed data for 61 m and 31 m. The number of
neurons in hidden layer is selected to be in the range of 6–16 for determining the
best approach. Feed-forward backpropagation learning algorithm is used for
Fig. 17.6 Wind measuring station installation procedure
17 Modelling of Wind Speed Using Artificial Neural Networks for University. . . 215
learning algorithm with one hidden layer. Inputs and outputs are normalized
between the ranges of 0 and 1 by the equation below (Sozen et al. 2010).
dN ¼ 0:8� dact þ dmin dmax þ dmin
� � þ 0:1 ð17:1Þ
In above equation, d represents data, act represents actual, min and max repre-
sents minimum and maximum.
Levenberg–Marquardt (LM) algorithm is selected for the training function.
Gradient descent with momentum weight and bias learning function
(LEARNGDM) is selected to be the adaption learning function. Neurons in input
layer have no transfer function. Computer program is performed under MATLAB
environment using neural network toolbox. The training of the network is accom-
plished by adjusting the weights and is carried out through training sets and training
cycles (epochs). The goal of the learning procedure is to find the optimal set of
weights. The output of the network is compared with a desired response to produce
an error (Kizilkan 2011). The performance of the network is measured in terms of
the absolute fraction of variance (R2) and the root mean square error (RMSE). The
equations for these functions are given below (Akdag et al. 2009).
Aircraft Warning Light
Temperature and Humidity Sensor
Pressure Sensor and
Data Logger
Anemometer
Anemometer
63 m
61 m
30 m
3. 5
m
28 m
59 m
4 m
Direction Sensor
Direction Sensor
Fig. 17.7 Schematic illustration of the wind measuring station
216 A. Kerem et al.
R2 ¼ 1� X
i ti þ oið Þ2X i oið Þ2
ð17:2Þ
RMSE ¼ 1 i
X i ti þ oij j2
� �1=2 ð17:3Þ
In above equations, t is the target value, o is the output value and i is the number
of patterns.
Results and Discussion
For the long term forecasting of wind speed data for the university campus, ANNs is
successfully applied using different number of layers. For each wind speed data,
80% of data are used for training and 20% of data are used for testing the neural
network. Log-sig activation function is used and for this reason all data were
normalized between 0 and 1. In order to determine the output parameters, logistic
sigmoid (log-sig) transfer function used here is given by;
Fig. 17.8 Wind measuring station final form
17 Modelling of Wind Speed Using Artificial Neural Networks for University. . . 217
Fi ¼ 1 1þ e�Ei ð17:4Þ
where;
Et ¼ Xt n¼1
InWn1 þ bn ð17:5Þ
In the above equations for Ei, the first two values are the multiplication of the
input parameters (In) with their weights at location, and the last constant value (bn)
represents the bias term. The subscript i represents the number of hidden neuron
(Karatas et al. 2009). The training parameters of ANNs are given in Fig. 17.9.
The results of the training in terms of statistical error values such as R2 and
RMSE for different number of hidden layers are given in Table 17.1. As seen from
the table, the best approach which has minimum error is obtained using seven
neurons for predicting the monthly average wind speed at 61 m and 11 neurons for
predicting the monthly average wind speed at 31 m. The performance of training
and test sets of the established ANNmodel for the two cases are given in Figs. 17.10
and 17.11 for two cases. It must be noted that the results given in Figs. 17.10 and
17.11 are for the best approaches obtained from ANNs.
Figures 17.12 and 17.13 show comparisons of the actual data obtained from the
measurements and predicted data from the modelling of ANNs for the two cases. As
seen from the figures the actual and predicted data are very similar to each other and
the established ANNs models give very accurate modeling of the measured data
instead of setting up several measurements.
As a result, it is very obvious that with this methodology, prediction of wind
speed instead of making several measurements can be carried out in a very short
time periods with high accuracy. The major advantages of ANNs are the calculation
speed, learning capability and simplicity. Consequently, for the forecasting of long
term wind speeds, ANNs approach shows almost precise estimations.
Fig. 17.9 Training parameters of ANNs
218 A. Kerem et al.
Table 17.1 Statistical error values of the models
Wind speed at 61 m Wind speed at 31 m
R2 RMSE R2 RMSE
LM6 0.4843 0.146275 0.4265 0.150973
LM7 0.8908 0.057074 0.8687 0.052959
LM8 0.7297 0.077489 0.4086 0.163676
LM9 0.2617 0.224754 0.3126 0.212168
LM10 0.126 0.244656 0.0834 0.246077
LM11 0.8835 0.053905 0.9026 0.050677
LM12 0.4196 0.156515 0.4906 0.173811
LM13 0.1426 0.217326 0.2481 0.196354
LM14 0.4182 0.215233 0.2017 0.179746
LM15 0.3968 0.19915 0.3667 0.197422
LM16 0.804 0.092906 0.0409 0.259957
100
1
0.8
0.6
0.4
0.2
0
10−2
10−4
10−6
0 0 0.2
R2=0.8908
0.4 0.6 0.8 1 1 2 3 4 5 6
11 Epochs Predicted values
A ct
u al
v al
u es
Best Validation Performance is 0.0091834 at epoch 5
M ea
n S
q u
ar ed
E rr
o r
(m se
)
7 8 9 10
Train Validation Test Best
11
Fig. 17.10 Performance of training and test sets for modelling of average wind speed at 61 m (LM7)
100
10−2
10−4
10−6
10−8
M ea
n S
q u
ar ed
E rr
o r
(m se
)
0 1 2 3 4 5 6 10 Epochs
7 8 9 10
1
0.8
0.6
0.4
0.2
0 0 0.2
R2=0.9026
0.4 0.6 0.8 1
Predicted values
A ct
u al
v al
u es
Train Validation Test Best
Best Validation Performance is 0.010091 at epoch 4
Fig. 17.11 Performance of training and test sets for modelling of average wind speed at 31 m (LM11)
17 Modelling of Wind Speed Using Artificial Neural Networks for University. . . 219
Conclusions
Wind energy potential of Mehmet Akif Ersoy University campus was analyzed
using ANNs. In order to determine the wind energy potential, a measurement tower
which was 63 m in height was built up. Measurements were made for 12 months.
The ANNs were used for long term forecasting of wind speed data. For this aim,
80% of data were used for training while 20% of data were used for testing. The
results showed that the deviation between the actual values and predicted values
were within acceptable uncertainties. The best approaches were found using seven
neurons for predicting the wind speed at 61 m and 11 neurons for predicting wind
speed at 31 m while the R2 values for the models were found to be 89.08% and
90.26%, respectively. As a result, the established ANNs models exhibited almost
Fig. 17.12 Comparison of actual and predicted values for average wind speeds at 61 m
Fig. 17.13 Comparison of actual and predicted values for average wind speeds at 31 m
220 A. Kerem et al.
precise long-term wind speed estimations instead of setting up several
measurements.
Acknowledgement The authors gratefully acknowledge support of this research by West Med- iterranean Development Agency (BAKA, Project Number: TR61/13/DFD/036) and Mehmet Akif
Ersoy University Scientific Research Projects Commission (Project Number: 0212-Güdümlü-13).
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222 A. Kerem et al.
Chapter 18
Cultural Landscapes as a Means of Energy Reduction at Global Warming
Afroditi Venetsanou, Alexandros-Theodoros Venetsanos,
and Lena Mantziou
Introduction
Reflection Framework
During the twentieth century, unconditional development led to dramatic alteration
of climate and environmental balance on the planet. Similar is the fate of cultural
heritage, where the memory and the ecological balance have been also sacrificed to
the rapid and massive development. The need for rescue measures for the natural
and historic environment became a universal appeal.
International mobilizations, declarations and treaties such as UNESCO,
RAMSAR and UNEP recognize values in sensitive natural and anthropogenic
landscapes and identify institutional frameworks to protect them.
The above already reflects the change in mentality, the diametric shift in
ecological conception and interpretation: The dominance of humans on the nature,
expressed by the over exploitation of the environment is now gradually succeeded
from a symbiotic logic of human labour with the environment.
The expansionist perception to absorb new virgin landscapes, to cover and
expand the living needs is gradually succeeded from recovery and reuse of existing
A. Venetsanou (*) Chemical Engineering NTUA, Tatoiou 89, Athens 14564, Greece
e-mail: [email protected]
A.-T. Venetsanos
Mechanical Engineering NTUA, Tatoiou 89, Athens 14564, Greece
e-mail: [email protected]
L. Mantziou
Dr. Architect Eng. NTUA, Assistant professor, School of Architecture NTUA, Adamon 2,
Athens 14564, Greece
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_18
223
bio-landscapes and facilities. The strategic use of natural inventory, acts protective
on the existing ecosystem, contributes indirectly (in this way) to reduce global
warming in the spirit of the contemporary international positions on sustainability
and viability.
At the dawn of the new millennium the balance between climate change, culture
and economy are the main issues of international concern. More and more we
concord that these matters are interrelated and influence each other.
The need for reasonable development under environmental equilibrium is get-
ting clear. Also awareness, that the way to protect the natural and cultural heritage
is neither the exclusion nor a museum, but creating worth-living growth conditions.
The recovery and reuse of historic living spaces, with a view to environmental
sustainability generates the local prerequisites for a reversal of global warming.
This work is based on the position that the ecological development of cultural
landscapes will act as a significant leverage for environmental improvements and
contribute locally to address global warming. In particular it considers that a new
strategic utilization of the ecosystem must activate regeneration of the environment
and at the same time ensure cultural continuity, social service, human recreation.
Starting at the micro scale of a landscape, this reflection may be extended to the
global range, to redefine the actual energy and environmental needs of future
mankind.
Project Terminology, Clarifications and Limitations
The term “Cultural landscapes” applies to areas obtained from the combined work
of man and nature over the time. They are bearer of tangible and intangible values,
precious to the broader community and significant to the environmental balance.
We recognize that cultural landscapes:
1. May bloom due to the long-time toil of man,
2. May then decline due to neglect inattention or abandonment,
3. Are threatened mainly by uncontrolled or incompatible ecosystem development.
Cultural landscapes are systemic areas with particular characteristics and qual-
ities, distinct from the surrounding environment. Such cultural and ecological
clusters can be perceived as living organisms, which offer particular experiences.
They are spatially distributed around the globe. We recognize heterogeneous
contents in cultural landscapes, covering the whole range of human interventions
in the nature. They also vary widely in their size, ranging from small blocks to
extensive manmade interventions in the natural landscape (Fig. 18.1–18.4).
This paper argues that cultural landscapes are best protected and revived when
people live act and learn through them. A main question is: which modern inter-
vention in a cultural landscape could retrieve memories, bring wealth to future
generations and at the same time upgrade the environment and climate of the
region?
224 A. Venetsanou et al.
The issue of reducing the global warming is of particular importance in densely
built urban environment. Areas out of the densely populated urban tissue may also
indirectly affect the balance of the environment to the extent that they either
develop a polluting activity or belong to a global network of travellers’ destinations accessible over intensive commuting and transport.
Fig. 18.1 Oil platform, North Sea
Fig. 18.2 Wetlands, Amvrakikos Gulf
18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 225
Fig. 18.3 Historical City Centre, Athens
Fig. 18.4 “Forte Portuense”, Rome
226 A. Venetsanou et al.
Methodology
The study emphasizes to the analysis of individual components of cultural land-
scapes. The purpose is to enable a systemic study of ecological dependencies.
Examination of the contribution of cultural landscapes to the reduction of global
warming will take place for some representative landscapes organized for this
purpose in two sections:
1. Cultural landscapes outside the urban tissue [Oil platforms (Fig. 18.1), Wetlands
(Fig. 18.2)].
2. Cultural landscapes in densely built urban tissue (Historical City—Centre
(Fig. 18.3), Citadel (Fig. 18.4)].
Selection criteria for the proposed landscape sample have been so far: Spatial
planning, scale characteristics, function, historical context, accessibility, commu-
nication, inclusion into the surrounding ecosystem.
Theoretical basis of the investigation may consist of multiple approaches—
“readings” of cultural landscapes. The uniqueness of each landscape will be
gradually further recognized by means of the above framework.
Project work for each of the selected landscapes will comprise:
1. The claim of reuse or revival
2. Identification of the current situation
3. Intervention strategy
4. Contribution to reduction of global warming.
Valuation
Many environmental and culture values remain intangible for valuation methods
like the LCC. Therefore a more sophisticated valuation method based on the
“common good” balance Matrix of the GCE may be more applicable for the
purpose of this study.
This work’s “added value” is on a “change of the way to think of the Environ- ment” through anthropocentric proposals (reuse, awareness, and sustainability).
Such a contribution cannot be evaluated by quantitative measurements, or a solely
technical feasibility assessment today. The main Goal is rather to start a process of
"change of mentality" which may then "cultivate" further individual quantitative
targets and technical solutions.
Sample pictures below highlight different structural models of Cultural
Landscapes
18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 227
1. Cultural Landscapes Outside the Urban Tissue
1.1 Alternative use of oil platforms at the end of their service life for energy retain.
Opening Question
Could the alternative use of oil platforms at the end of their service life contribute to
retain energy?
Identification of the Cultural Landscape
In the UK continental shelf—an area of the North Sea with large resources of
hydrocarbons—there are over 600 offshore oil rigs and subsea installations, while
approximately half of them are over 15 years old and approaching the end of their
service life. According to the Oil & Gas UK Economic Report 2013, about
475 installations, 10,000 km of pipelines, 15 onshore terminals and 5000 wells
will eventually need to be decommissioned. Over the next 25 years,
decommissioning costs are estimated to be in the region of £31.5bn.
This issue is not limited to the UK but concerns every country having offshore
activity, because it triggers many environmental concerns relative to the required
energy, CO2 emissions and the ocean water contamination. At present, the common
decommissioning practice in case of fixed oil rigs is either to remove the hazardous
waste and topple them creating in this way artificial reefs, or to remove the topsides
by reverse installation of modules using heavy lift vessels and recycle them onshore
(Scottish Enterprise Energy Team 2008). As for the jackets they are cut into pieces
using diamond wire techniques before being transported onshore for recycling.
Regarding to the floating platforms, they are towed to the shore for scraping or
they sink.
According to the Institute of Petroleum both direct and indirect energy require-
ments for different decommissioning solutions are compared in Table 18.1. As
reference point has been set the required energy for toppling a platform, while the
rest alternatives are compared to this value.
However, there are also several alternatives for sustainable reusing the existing
facilities for non production purposes. More specifically, Wan Abdullah Zawawi
et al. (2014) have proposed viable possibilities including (a) offshore maintenance
and logistics bases, (b) sites for wind turbines, wave energy generating equipment
and(or) photovoltaic panels, (c) LNG terminals, (d) sites for aquaculture facilities,
(e) tourism attractions, (f) offshore research and training centres, and (g) bases for
search-and rescue operations.
228 A. Venetsanou et al.
Figure 18.5 shows a proposal designed byMorris Architects which won the 2008
Radical Innovation in Hospitality Awards for a self-sustaining and eco-friendly
hotel offshore. Figures 18.6 and 18.7 illustrate a conceptual design by Ku Yee Kee
and Hor Sue-Wern of a transformed abandoned oil rig into a modern city. This
proposal was one of the finalists of the Evolo’s 2011 Skyscraper Competition. The main idea is that a former oil rig could be inspected reinforced and converted into an
offshore accommodation building. Residents would live above the water level,
while underwater laboratories could be used for subsea observations. As for the
energy requirements of the building, they could be covered by wind turbines and
solar panels on the top of the structure and tidal turbines at the bottom.
At this point must be mentioned that the jackets of fixed platforms could be
transported to the shore and be used as frames for buildings after being properly
reinforced.
Table 18.1 Comparison of energy requirements for various decommissioning alternatives
Scenario
% of total energy (compared to
toppling as baseline)
A—Toppling (Baseline) 100
B—Partial ashore and partial in-situ 101
C—Partial removal with partial in-situ and creation of
reef in other location
106
D—Complete removal ashore 114
E—Complete removal to deep water 154
Source: ERT 1997, Page 11, Table 4
Fig. 18.5 Proposal by Morris Architects 2008 Radical Innovation in Hospitality
18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 229
Fig. 18.6 Design by Ku Yee Kee and Hor Sue-Wern—transformed abandoned oil rig into a modern city
Fig. 18.7 Cross-section model of Fig. 18.6
230 A. Venetsanou et al.
Summary
To sum up, reuse takes place when a component or a whole structure can be
reclaimed after the expiry of its lifespan for similar or different purpose compared
to the initial one instead of recycling or disposal. In this way, the embodied energy
is retained, and the environmental impacts are eliminated. Reusing existing facil-
ities potentially removes thousands of tons of steel from the waste stream and
reduces the input energy required for reprocessing or recycling. Reuse is an
important aspect of sustainability as the energy used for retrofit or refurbishment
is relatively small compared to the energy consumed by the recycling process.
1.2 A Gateway to the Amvrakikos Gulf
Opening Question
How would the invisible natural wealth of Amvrakikos Gulf reverse declining
economic progress of the region and help its residents to undertake ecological
actions for the sake of the ecosystem’s balance?
Identification of the Cultural Landscape
The Amvrakikos Gulf covers a wetland area of 400qm2, between Central Greece
and Epirus forming the “largest wetland system” of Greece, surrounded by moun-
tains with a narrow mouth to the open sea.
Wealthy cities grew since the ancient time in this region, such as Kassiopi,
Amvrakia (Arta), and Nikopolis. Testimonies of wealth are important archaeolog-
ical sites with outstanding monuments, like the Roman aqueduct of Nicopolis.
Ecosystem
The wealth of Amvrakikos is due to the double delta of the rivers Louros and
Arachthos, who, flowing into in the northern part of the bay, creates a true mosaic of
wetlands, the largest one in Mediterranean Europe. The biotope has been an
inexhaustible source of life for centuries nourishing both wild animals and birds
that find shelter here, as also humans who has learned to use and exploit it.
Riparian strip islands form the boundary between the bay waters and the lagoon
(Fig. 18.8). This linear “shell beach” is naturally formed by sediment concentra-
tions, and get interrupted by natural water mouths, communication channels that
continuously enrich the lagoons with saltwater. With the rivers causing aggrada-
tions and occasional flooding a network of freshwater is maintained in the lagoons,
18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 231
reaching the fish populations, revitalising them with spawn transferred from the
Ionian Sea’s saltwater.
Human Presence and Intervention
By the ancient times local residents have been taking advantage of the biotope.
Fishing methods in the lagoons have been based on the observation of the behaviour
of fish populations in various weather conditions (winds, moon phases), oceano-
graphic conditions (tides, currents), environmental conditions (water temperature,
salinity) and good knowledge of the biological dispersal of the species to and from
the lagoon. Based on this experience, the residents designed and implemented fish
traps and constructions such as fish pens, etc. Applying simple interventions they
transformed the brackish basins in natural fish farms. In passageways within the
islets special dams are installed, which allow water to pass through, but entrap fish
and crustaceans (Petrou and Mantziou 2014) (Fig. 18.9).
The life of the fishermen has its own distinctive features, since the management
of lagoons requires continuous human presence in site, serving for the several daily
tasks and fisheries, and also as custody of facilities, catch and fishing gear.
Today fishing in the lagoons has been streamlined. With the introduction of
modern fish pen facilities, empirical knowledge is now coupled with scientific one
for optimal results. With very few exceptions, these new permanent fish pen are
Fig. 18.8 Amvrakikos Gulf—Riparian strip islands form the boundary between the bay waters and the lagoon. [©Processing M. Petrou]
232 A. Venetsanou et al.
placed in the same locations and arranged in almost the same way as the former,
traditional ones.
Around the perimeter of the bay scattered villages and small towns (Vonitsa,
Amfilochia, Arta, Preveza) have been developed.
Today’s Picture—Ecosystem and Environmental Problems
Anthropogenic interventions like changes in river bed patterns, hydropower plant
dams and intensification of agriculture and farming have caused pollution of the bay
and the lagoons. Interventions in the morphology of the mouth of Amvrakikos as
the port of Preveza and a private marina in Aktion generated silting negatively
affecting the fluid dynamic equilibrium of the bay (Fig. 18.10).
The commercial port of Preveza, built in 1968 is nowadays a complex environ-
mental pollutant. The oversized scale of the port in combination with its location
reduces the cross section and the opening of the mouth of Ambrakikos to 46% of its
original size (from 740 m to 393 m). This increases the speed of Input—Output
currents in the bay which in turn increases risks of erosion of the coastal zone. The
port construction directly in the city’s traditional tissue in front of the castle has
altered the form of the city. Operations in the commercial harbour pollute with dust
and noise due to heavy vehicle movements, degrading the quality of life in the
historic city centre and the seafront (Kanioris et al. 2009).
Fig. 18.9 Amvrakikos Gulf—linear “shell beach”—In passageways within the islets special dams are installed [©Processing M. Petrou]
18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 233
Contamination led to lower fish populations and lower yields from fisheries.
Reduction of fishermen’ income brought a gradual disinterest for the profession, finally the new generation is rather willing to abandon the territory and find better
paying jobs elsewhere.
Ecological Reconstruction Proposal
The area has significant potential for environmental friendly activities. Efforts for
fishery and marine conservation are crucial, as they bring harmony and balance to
the ecosystem:
1. The proposal for a fishing tourism includes developing of fishing activities by
professional fishermen, aimed both for recreation tourism and for spreading the
alternative fishing culture in the country, as well for directly support the fisher-
men financially and stimulate the social web of the local communities.
2. The bipolar system of benefits resulting via the fishing tourism, with final
consumers (tourists) and service providers (fishermen) follows the requirements
of sustainable development.
3. The harmonic coexistence of fishermen and their natural environment through
the promotion and protection of natural, historical, cultural and traditional values
of the region complements the quality of life of residents who already enhanced
their incomes.
4. This new touristic segment is a unique model in the Greek territory.
Fig. 18.10 The port of Preveza and a marina in
Aktion reduce the cross
section and the opening of
the mouth of Ambrakikos
234 A. Venetsanou et al.
5. The non-existent road exits make the wetland ecosystem of Amvrakikos invis-
ible and difficult to reach. Therefore, it is proposed to set up a network of fishing
tourism activities, and mark up this action in waterfronts of cities on the
periphery and near the Gulf.
6. As a pilot project is proposed to create a gateway to the Amvrakikos at Preveza.
The choice of Preveza is due to the comparative advantage this city possesses,
given the multiple elements of natural and cultural heritage, and it’s European, national and local importance (Amvrakikos, Ancient Nicopolis, further ancient
and medieval castles and monuments).
Urban Planning Intervention a Gateway to the Amvrakikos Gulf on the Waterfront of Preveza
The seaside promenade will be extended over the entire long side of the historic city
centre, along which the port for sailing ships and yachts resides. On the southern
edge of the pedestrian esplanade a distinctive enlargement is formed, which meets
the sea front. During the early morning hours eve of fishing vessels may be
observed at this point, where fishermen conduct an informal catch market.
1. The Gateway to the Amvrakikos will be located in the plateau that penetrates the
sea, on the border of land and water.
2. The structure of the fish pens inspires the architecture proposal. The narrow
passage between two constructions, identifies the communication channel of two
different worlds and symbolizes the initiation of residents or visitors to the
invisible world of the fishermen.
3. The first construction constitutes a “floating” sloping square, orientated to the
historic city centre and the seafront promenade. The square offers viewings in
the town and the people’s motion at the seafront as well. At the same time it accommodates exhibitions and activities about the invisible wealth of
Amvrakikos (Fig. 18.11).
4. The second construction houses the fish market, auction, production and also
storage of Amvrakikos products like fish roe under showroom conditions.
5. At the end of the passageway the boat station for transfers to the lagoons will be
located.
Both residents of the city and visitors have the opportunity to tour the site and
learn through the implemented actions about flora and fauna in the heart of
Amvrakikos. By embarking on boats and touring the broader region, travellers
may discover the wealth of Amvrakikos and traditional ways of fishing that remain
alive over centuries.
18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 235
Effects on the Ecosystem
1. Restoring sustainable job prospects for the new generation prevents depopula-
tion of the country and the overconcentration of population in major urban
centres.
2. Fishing as labour dependent on the environmental balance generates the need for
conservation and a preservation consciousness, as respect to the ecological
balance.
3. The architectural configuration of Amvrakikos Gate makes the cultural area well
known publicly and contribute to a rise of visitors. It is so propagating the idea of
fishing and cultural tourism as a coexistence principle with nature also to be
applied in other similar natural habitats.
4. The ideal size and equilibrium of Amvrakikos which do not allow large indus-
trial scale interventions inspires a return to a small-scale balance.
5. The area proportions express the geological and physical properties of the
broader seaside region of the Greek landscape, this of southern Balkans, and
most coastal countries of the Mediterranean. In this region, where the climate
charges are less of industrial origin and more a result of urbanization, climate
preservation is primarily an issue of decentralization. By this reasoning, the
above proposal is a most possible direct interference against global warming in
the given broader area.
Fig. 18.11 “Floating” sloping square, orientated to the historic city centre and the seafront promenade [©Processing M. Petrou]
236 A. Venetsanou et al.
2. Cultural Landscapes Within the Dense Urban Tissue
2.1 Museum Clusters
Opening Question
How modern intervention in densely built historic centre may retrieve memories,
highlight wealth to future generations and at the same time upgrade the environ-
ment and climate of the region?
Identification of the Cultural Landscape
By the End off the twentieth century, modern metropolis became aware of their
potential to add value to their community by attempting the combined effort of
cultural, environmental and economic regeneration. Favourable field of experimen-
tation became the programmatic establishment of museums areas. The combined
investment in culture and the environment becomes eloquently in the planning of
museum clusters. The concentration of museums in a wide green area near the city
centre may be found in many large cities of today, like the National Mall in
Washington (Fig. 18.12), the Museumplein in Amsterdam, the Kunstareal in
Munich (Fig. 18.13), the Museumsufer in Frankfurt.
In the city of Athens, the project of unification of archaeological sites dilutes the
frontiers between the ancient, the neoclassical and modern city and creates the
Fig. 18.12 National Mall in Washington, DC. [©Processing L. Mantziou]
18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 237
Open Museum. The pedestrian network around the Acropolis was a corrective
move, which brought the archaeological sites close to the residents. The removal
of automotive from the shadow of the Holy Rock has beneficial effects on the
microclimate of the area and restored biodiversity in the city centre. The pedestria-
nization of D. Areopagitou—Ap. Pavlou, acts as a ‘patchwork’, which brings the archaeological sites close to the residents, upgrading public space of the city and the
quality of life for citizens and visitors.
Summary
These areas serve as oases in the urban tissue, away from the disturbance of the
automobile. The embellishing nature of the planted areas privileges cultural and
social activities who take place in these gardens, attracting citizens and visitors to
use their free time participating in cultural and naturalistic events.
Fig. 18.13 Kunstareal in Munich [©L. Mantziou]
238 A. Venetsanou et al.
2.2 Rome Community Ring—Forte Portuense
Opening Question
How can we transform an object of military architecture at a local Centre for
recreation and culture, capable to supply urban regeneration, to act beneficial to
the environment and the surrounding area also attracting both residents and
tourists?
Identification of the Cultural Landscape
The municipality of Rome in cooperation with the University La Sapienza and the
agency Progetto Forti initiated a dialogue about one of its precious treasures, the
fortress “Forte Portuense” in Rome. The issue emerged in winter 2014, with an
international architectural competition for the purpose of transformation of “Forte
Portuense” to a recreation area, supporting education and sport.
The fort was part of a larger defence system of fortresses and the artillery placed
in a ring of 4 km outside the ancient walls of the city of Rome. Located at the
entrance to the city, between the River Tiber and street Via Portuense. The Field is
defined by four concentric zones:
1. The nucleus the fort,
2. The dry trench,
3. The external peripheral free space, where are scattered building facilities, while
part is formed on inclined slopes with dense vegetation
4. The urban tissue.
Proposal
The first prize, (won from the Greek team pyrphoros), proposed the creation of an
urban oasis, through the restoration and enhancement of the landscape on the hill.
The overall design attempts to create a lung in densely built urban tissue and to
reunite the various levels of the fort with each other and the city (Fig. 18.14).
In particular, the study includes:
• The use of existing areas in the nucleus of the fort, for hosting mild recreational
activities and exhibitions.
• Hosting sporting activities in the ditch, with the provision of reversible
installations.
• The design of a network of paths on the hill, which combines existing landmarks
of the city and the new reference and orientation points.
• Placement of kindergarten facilities, centre for the elderly and community
services in the outer zone in close proximity to the city.
18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 239
Fig. 18.14 Forte Portuense Conceptual view, Topography, Section. First prize: team Pyrphoros: E. Ziova, C. Lazou, E. Karaoli, A. Rachioti, L.Mantziou (consultant)
240 A. Venetsanou et al.
• Taking advantage of the sloping ground to locate main building blocks under-
ground, thus highlight the landscape and the fort.
• Applying the principles of bioclimatic design with integration of passive heating
and cooling, opens space to the south and makes use of natural ventilation.
• Supports creation of local outbursts for external signalling and natural ventila-
tion of underground space.
• The redesign of the boundary between the study area and the “Via Portuense”,
with the creation of an extensive arcade, following the curve road line and filter
nuisance caused by automotive.
• The coverage of the arcade with photovoltaic panels to assemble energy
autonomy.
• The shaping of input square and reception to the fort with a gesture signifying
the contemporary image of the fort in the twenty-first century.
Conclusion and Suggestion
The examples introduced are representative for different types of cultural land-
scapes and all have as common reflection the reversing of the declining quality of
life. The various causes of decadence can be found in the exhaustion of life
expectancy (oil rigs), changes in living conditions over time (Roman castles), the
impulsive and hasty adoption of each contemporary siren.
The misplaced interventions in fragile ecosystems (Amvrakikos), the dissolution
of the urban fabric by the freedom of the motorisation, the oversized transportation
infrastructure, all require intensive actions in order to undo or correct wrong
decisions implemented so far.
The different proposals presented above shows a new consensus on the relation-
ship between human and their environment. They argue that the achievement of
(future) ecological balance presupposes changing mentalities that will result from a
combined cultural, aesthetic, economic and ecological intervention.
Already in the late twentieth century, the largest metropolises of the Western
world became aware that culture is a lever to pull the economy and try to add value
to their communities by attracting cultural tourism. In this context, the core of the
old city (inner city) is considered a “cultural object” and the heritage recognized as
urban resource. The preservation of the historic centre of the city goes along with a
new momentum for the internal urban regeneration and recovery of the material
stock. The development of the historic centre of the city, in terms of environmental
sensitivity assist the so-called urban growth without landscape consumption.
This paper proposes the conversion of deserted cultural landscapes in energy
oases. The term “urban oasis”, describes the improvement of environmental con-
ditions in the former busy urban environment. Deserted castles, museums areas
(museum clusters), automotive roads can potentially become urban oases and
contribute to the cultural, environmental and social regeneration of the city.
18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 241
It is a fact that human activities within the city in conjunction with the thermal
characteristics of urban areas and urban geometry, affect the quality of the air and
emit heat, increasing the local temperature, smog levels and humidity, with nega-
tive effects on the carbon footprint of urban buildings and the thermal comfort of
the residents. Energy upgrading of building stock, due to a marked reduction of
energy that can offer, is a requirement in modern societies. Till now, the energy
upgrade focused on interventions on individual buildings. The possibility to
develop green areas in densely built urban tissue is limited. Considering that free
spaces are expensive, another type of strategies are being sought to address the
urban heat island.
The new concept redefines the scope of energy upgrade, expands the study limits
beyond the enclosed space and captures the building unity—surroundings. The
building is not considered in isolation but as a whole with its surroundings. The new
approach seeks thermal discharge of the microenvironment. The strategy of urban
oases utilizes the stock material, serves the perception of preservation of the city
centre as a “cultural object”, goes along with a new momentum for the internal
urban regeneration and enhances biodiversity in the city.
Both within cities as also outside urban tissue, a defensive strategy is often
followed, which intervenes to reduce the symptom and is exhausted in quantitative
measurements. But there are significant hidden factors which are not currently
quantifiable—traceable and they affect global warming.
One of them is considered the material stock of abandoned structures, which
multiply in an uncontrolled rate and strongly raises the question of their mainte-
nance. Dismantling and removal is often not feasible due to the excessive cost and
energy consumption. Intangible values, like cultural memories or embodied energy,
suggest the strategy of reuse as a source of hope—a most efficient environmental
option. The energy upgrading of existing cultural landscapes will be founded on the
interdisciplinarity and will demonstrate synergy—in involvement of different fac-
tors and viewpoints—in a collective global climate regeneration effort.
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18 Cultural Landscapes as a Means of Energy Reduction at Global Warming 243
Part V
Energy Technologies and Their Effect on Global Warming
Solar Energy
Investigation of solar still performance and novel combination of solar energy with
methane reforming reactors and organic Rankine cycle for power generation.
Chapter 19
Solar-Driven Continuous Methane Reforming Reactor
M. Lange, J. Lapp, R. Rieping, L. de Oliveira, M. Roeb, and C. Sattler
Introduction
The world energy demand is covered mainly by the use of fossil fuels. Apart from
the direct use of fossil fuels, however, the use of synthetic (mainly liquid) fuels has
been attracting a lot of interest lately. Currently, synthetic fuels are produced at a
commercial scale from carbonaceous sources with low energy content, which are
upgraded at the expense of additional energy. This additional energy is also
obtained from the combustion of fossil fuels. In order to make the latter procedure
more attractive and environmentally friendlier, these processes could be combined
with a renewable energy source, such as solar energy.
Although there is an increase in the use of alternative energy vectors,
e.g. renewable electricity, the reliance on fossil fuels is still extensive. The main
advantage of liquid fuels when compared for example to electricity is their prompt
availability upon demand regardless of temporal or location-related restrictions.
The preservation of economic stability and growth creates the most significant
motive for industries to start pursuing environmentally friendlier energy vectors.
Existing technologies are further investigated and improved in order to minimize
CO2 production and renewable energy installations have started to appear with
higher frequency. An important step forward would be to employ solar energy, an
inexhaustible energy source, in order to produce synthetic fuels.
As a consequence, in the last decade an increased research activity could be
noted regarding the exploitation of the solar potential to produce Hydrogen or
synthesis gas (hydrogenþ carbon monoxide) through the dissociation of water and carbon dioxide (Ermanoski et al. 2014; Roeb et al. 2008, 2012; Muhich
M. Lange (*) • J. Lapp • R. Rieping • L. de Oliveira • M. Roeb • C. Sattler German Aerospace Center (DLR), Institute of Solar Research, Linder H€ohe, 51147 K€oln, Germany e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_19
249
et al. 2013). On one hand solar water-splitting is a totally renewable process with
zero greenhouse gas emissions, while on the other hand solar carbon dioxide
splitting utilizes CO2—amaterial which is currently characterized as an undesirable
waste—as a reactant to finally produce valuable solar fuels. However, these pro-
cesses have not yet reached the essential maturity for large-scale industrial
implementation.
A process that is considered to have one of the highest short term potential in
terms of technology and economics is solar reforming of methane (Agrafiotis
et al. 2014). With such an approach longer term carbon-neutral or carbon-free
energy solutions, such as water and carbon dioxide splitting with the aid of solar
energy for the production of solar fuels, can be given the required time to be
developed. Further, the feedstock natural gas may be replaced in the future by
biogas sources (Bereketidou and Goula 2012).
In this paper we propose a new reactor concept which acts as a solar receiver-
reactor and heat exchanger at the same time. This multi-use approach enables
continuous methane reforming and even night time operation is possible.
Concept
Several solar reactors for methane reforming have been developed and studied
previously (W€orner and Tamme 1998; Agrafiotis et al. 2014). The novelty of the proposed concept is its flexibility regarding the solar radiation. The key to this
flexibility lies in the receiver geometry. The core of the receiver consists of a
monolithic honeycomb structure with two different and separated sets of channels,
see Fig. 19.1.
For daytime operation, concentrated solar radiation is focused on the front face
of the monolith, heating it up to 900 �C. In one set of channels, the solar heat is used to run the endothermic reforming reaction. Steam reforming (19.1) and dry
reforming (19.2) or a mixture of both is possible (Rostrup-Nielsen 2002):
CH4 þ H2O ! 3H2 þ CO ΔH� 298K ¼ þ206 kj=mol ð19:1Þ CH4 þ CO2 ! 2H2 þ 2CO ΔH� 298K ¼ þ 247 kj=mol ð19:2Þ
In the other set of channels, heat is taken up by a heat transfer medium, which we
propose to be air. This heat transfer medium transfers the solar heat to a thermal
storage close to the reactor.
During nighttime operation, the air flow is reversed in order to transfer the heat
from the storage to the receiver. With this heat, the reforming reaction in the first set
of channels can be powered even without direct solar input.
A process flow diagram of the concept is shown in Fig. 19.2.
This new concept brings along the potential to reduce costs, because by contin-
uous operation all the downstream components can be reduced in size and thus
250 M. Lange et al.
Fig. 19.1 Concept drawing of novel receiver reactor monolithic structure
New Receiver- Reactor
Educts
Syngas
Heat Storage
Hot Air Concentrated Solar
Irradiation
Cold Air
Cold Air
New Receiver- Reactor
Educts
Syngas
Heat Storage
Hot Air
Cold Air
Cold Air
(H2 + CO)
(CH4 + H2O)
(CH4 + H2O)
(H2 + CO)
Fig. 19.2 Process scheme (top: on-sun operation mode; bottom: off-sun operation mode)
19 Solar-Driven Continuous Methane Reforming Reactor 251
costs. Additionally, less start-up and shut-down cycles will be necessary which is
beneficial from an operational as well as from a durability point of view.
Production of Monolith
As the monolith concept is novel, no standard production method is readily
available to create such a geometry. Therefore, a custom-made honeycomb was
produced. The production method, which is illustrated in Fig. 19.3, is explained in
the following.
First, a common honeycomb made from recrystallized silicon carbide (RSiC)
was acquired. Such pieces are extruded mainly for the automotive industry (cata-
lytic converters, diesel particulate filters). As the channel walls of the monolith
need to be very gas tight in order to avoid crossover flow between the two channel
types, the porous RSiC needs to be infiltrated with further silicon. Only then, the
channel walls are gas tight. However, the Si-infiltrated silicon carbide (SiSiC) is
extremely hard to machine. Therefore, before infiltration, the slots which are
necessary for the side inlet channels were cut into the RSiC piece. Then, infiltration
was carried out. After that, the monolith walls were coated with a Rhodium and
Al2O3 catalyst which is necessary for the reforming reaction. In a final step, the
slots which had been cut into the front and back of the monolith were closed with
ceramic glue and SiC-sticks.
Some pictures showing the real production steps are shown in Fig. 19.4.
Fig. 19.3 Production method of custom honeycomb (only upper half shown here, lower half is symmetric). (1) Extruded RSiC monolith, (2) cutting of slots, (3) infiltration to SiSiC, (4) catalyst coating and preparation for closing of slots, (5) closing of slots, (6) burning and removal of stick for closing of slots
252 M. Lange et al.
Experimental Set-up
The concept is currently being experimentally evaluated at the high flux solar
simulator of DLR, Cologne. The reactor during assembly is displayed in Fig. 19.5.
The solar simulator has a maximum power input of 20 kW. The simulator
consists of 10 xenon lamps which have a spectrum similar to the solar spectrum.
This solar-like concentrated radiation will be used to simulate the daytime opera-
tion. Half of the input energy will be used for the reforming reaction and the other
half will be taken up by the air stream.
A scheme of the experimental set-up is shown in Fig. 19.6.
This first test campaign focuses on only thermal characterization of the concept.
This way, a more sound characterization of the thermal behaviour of the system is
possible, because no heat of reaction distorts the thermal result. Further, valuable
information can be collected to decide how the reactor should be operated.
In the experimental setup, two gas heaters are included. The first one, which is
located upstream of the reactor in the reactants stream, is employed in order to
simulate heat recovery from the product gas stream. In a future plant, such heat
recovery would most likely be implemented. As real heat recovery with a heat
exchanger would reduce the flexibility of the set-up and thus also the scientific
output of the experiments, we decided to replace a real physical heat recovery by
Fig. 19.4 Steps of producing the monolith. (1) Slots in RSiC block, (2) SiSiC block, (3) closing of slots, (4) final geometry
19 Solar-Driven Continuous Methane Reforming Reactor 253
this first gas heater. The second gas heater is placed in the air stream before entering
the reactor. This heater enables to simulate nighttime operation. Again, we apply
this electrical heater instead of a heat storage in order to stay as flexible as possible,
in order to increase the scientific output and also to save expenses.
For the experimental campaign, the methodology called Design of Experiments
is applied. This method is based on statistical evaluation of the results. During the
experiments, not one factor at a time (OFAT) will be changed, but several
Fig. 19.5 Left: assembly of monolith in reactor shell, right: final design of reactor with glass window for solar input
Fig. 19.6 Experimental set-up for continuous methane reforming
254 M. Lange et al.
parameters (like mass flows, inlet temperatures and radiation) will be changed at
once. By statistical analysis, the results have a more general character than results
obtained with the OFAT method, because interactions between parameters can be
assessed.
Conclusion
A novel receiver reactor concept for continuous operation of solar thermochemical
processes has been proposed. The core of the concept is a honeycomb monolith
with two different sets of channels. One set of channels is used for a solar-powered
reaction, the other set of channels acts as a heat exchanger to take up heat during the
day and bring it back into the reactor at night.
As the monolith is not a standard part, it was custom made. The production
process was described. Further, the monolith is integrated into a reactor, which in
turn is integrated into an experimental set-up in a high flux solar simulator. In this
experimental set-up, it is possible to simulate daytime as well as night time
operation.
Acknowledgement The authors thank the German Ministry of Education and Research for funding this work within the project ContiSol (Contract Number 03SF0468). We also greatly
acknowledge the work of our colleagues and project partners Dr. Souzana Lorentzou and
Christodoulos Lekkos from Aerosol & Particle Technology Laboratory, CERTH-CPERI.
References
Agrafiotis, C., von Storch, H., Roeb, M., Sattler, C. (2014). Solar thermal reforming of methane
feedstocks for hydrogen and syngas production—A review. Renewable and Sustainable Energy Reviews, 29, 656–682.
Bereketidou, O. A., & Goula, M. A. (2012). Biogas reforming for syngas production over nickel
supported on ceria–alumina catalysts. Catalysis Today, 195(1), 93–100. Ermanoski, I., McDaniel, A. H. (2014). Solar hydrogen production with a metal oxide based
thermochemical cycle. DOE Annual Merit Review: 25. Muhich, C. L., Evanko, B. W., Weston, K. C., Lichty, P., Liang, X., Martinek, J. (2013). Efficient
generation of H2 by splitting water with an isothermal redox cycle. Science, 341(6145), 540–542.
Roeb, M., Neises, M., Monnerie, N., Call, F., Simon, H., Sattler, C. (2012). Materials-related
aspects of thermochemical water and carbon dioxide splitting: A review. Materials, 5(11), 2015–2054.
Roeb, M., Neises, M., Säck, J.-P., Rietbrock, P., Monnerie, N., Dersch, J. (2008). Operational
strategy of a two-step thermochemical process for solar hydrogen production. International Journal of Hydrogen Energy, 34(10), 4537–4545.
Rostrup-Nielsen, J. R. (2002). Syngas in perspective. Catalysis Today, 71(3–4), 243–247. W€orner, A., & Tamme, R. (1998). CO2 reforming of methane in a solar driven volumetric receiver-
reactor. Catalysis Today, 46, 165–174.
19 Solar-Driven Continuous Methane Reforming Reactor 255
Chapter 20
Specific Applications/Examples: Use of Solar Energy in Fishing: Community Initiatives
J. Vincent Jain and Satish Babu
Research Background
Any developmental project or research project without considering the climate
change factor will be incomplete. Indeed, ‘climate change has become the defining generational challenge for the international community.’ It is considered one of the biggest threats to our world today. The aftermath of today’s global condition, if not given due attention locally and globally, would harshly affect the young generation
and the generations to come and they won’t find the earth a better place to live. The significant rise in global temperature and human activities has worsened the
situation. Energy saving, conservation of water and minimization of emission of
CO2 help to balance the Global Warming.
Introduction
Fishery is an area where an alternative energy technology, products and its services
are needed to minimize the fossil fuel dependency which could save large amount
of energy, water and reduce carbon emission. Fishing is considered as the most
energy-intensive food production method in the world. In India, thousands of large-
and medium-size fishing boats—from trawlers and seiners to liners and
J.V. Jain (*) Association of Deep Sea Going Artisanal Fishermen, Shark Street, Thoothoor P.O.,
Kanyakumari District, Tamil Nadu, India
e-mail: [email protected]
S. Babu
ICFOSS, Technopark, Trivandrum, Kerala, India
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_20
257
gillnetters—depend primarily on one fossil fuel, diesel or kerosene. Large volumes
of energy and water are used to produce inputs for pre harvest and post harvest
activities. If we are able to use an alternate energy technology, products and its
services properly we could save large amount energy, water and avoid unnecessary
emission of CO2. There is scope to reduce CO2. by setting emission norms and
improving fuel efficiency of marine fishing boats.
Problem
An artisanal deep sea fisherman takes 15–20 days for a fishing voyage. A few
others take 25–30 days and more. During the voyage they have to keep the engine
running the engine for charging of the batteries. The engine keeps running
even they are not fishing. Some fishermen keep running the engine to prevent
restarting trouble. About 20–25% of fuel is used for the continuous operation of
the engine. The signal lights, navigational and safety equipments are operating with
the support of batteries in the boat. Many times fishermen have met with accidents
and have been unable to use the navigational and safety equipments because of
engine failure.
Community Initiatives
Though tapping solar energy for land-based applications is very popular, its use in
fisheries sector is uncommon. In India, the idea of using solar energy in fishing
boats was first initiated in the year 2010 by the Association of Deep Sea Going
Artisanal fishermen (ADSGAF), a fishermen organization based in Thoothoor,
Kanniyakumari District, Tamil Nadu, India.
The ADSGAF was established in 1992. It has 340 full-time members who are
engaged in long lining and gill-netting using small mechanized boats (15–21 m in
length) within the Indian Exclusive Economic Zone (EEZ). There are around 3400
fish workers and their dependents associated with the organization. There are
600 deep sea going fishing vessels in Thoothoor area that they fish all over the
Indian EEZ, which covers an area of 2.02 million sq. km. During 2009, the
members of ADSGAF raised the issue of increasing searching time for fish coupled
with rising fuel cost leading to decline in their income. The members also expressed
concerns about increasing cost of running the engine during idle time for lighting
and signalling requirements. It was found that fuel cost is accounting for about 70%
of the total operational costs.
Faced with this challenge and also considering the carbon footprints generated
by this fishery, the ADSGAF decided to experiment with the use of solar energy in
fishing vessels in 2010. Initially, the ADSGAF made a prototype boat (3 feet on
scale) equipped with solar panels and associated batteries etc and demonstrated its
258 J.V. Jain and S. Babu
operation and technical feasibility under laboratory conditions. In August 2012, the
ADSGAF further demonstrated the pilot-scale initiative in Chennai with the
involvement of the Bay of Bengal Programme, an Inter-Governmental Organisation
(BOBP-IGO) working in Bangladesh, India, Maldives and Sri Lanka.
Why Solar Energy
Solar energy is the cleanest, most abundant and renewable energy source available.
Today’s technology allows us to capture this power in several ways giving the
public and commercial entities flexible ways to employ both the heat and light of
the sun. Solar energy can be produced on a distributed basis, called distributed
generation, with equipment located on rooftops or on ground-mounted fixtures
close to where the energy is used. Large-scale concentrating solar power systems
can also produce energy at a central power plant.
Techno-Economic Assessments and Pilot Trials
The ADSGAF since then carried out a couple of techno-economic assessments
and pilot trials to measure the efficacy and viability of their venture in different
categories of fishing boats. It is found that while at sea the engine is run for several
hours at partial load to provide power for auxiliary activities such as lighting,
communication, navigation, signalling and on-board entertainment. Therefore,
if these services can be run by using alternative power sources there could be a
significant saving of fuel and this will improve the viability of the operation as well
as reduce the carbon footprints. From the pilot- scale trials, it is seen that switching
off the engine for 3 h can save 30 l of fuel a day and 7500 l per year. The potential
reduction of carbon dioxide emissions per year if the entire fleet switches off the
engine for three hours a day is estimated to be 117,000,00 kg (11,700 tonnes)
(refer Table 20.1). Therefore, solar power seems to be a viable alternative to reduce
fuel cost in fishing operations.
The size of the boat (Fig. 20.1) is 15.5 m length and 4.5 m width which undertake
a voyage of about 15 days. It operates long lines and gill nets. Four solar panels of
1 kW (250 W each) are fitted at the top of the wheel house of the boat. Presently
there are six such boats are in operation. The solar energy accumulated during the
day is able to light the bulbs/tube lights/focus lights and also charge/operate the
GPS, fish finder and the two VHF sets. Additionally, when required during night
time, the transistor batteries can also be charged.
Mr. Sunil who is the skipper of the vessel for the past 10 years told that he
is satisfied with the light while fishing and he never find trouble in starting
and re-starting the engine during the fishing voyage. Mr. Jose, a crew member
said, “Usually light in the boat will not be bright and need utmost care for removing
20 Specific Applications/Examples: Use of Solar Energy in Fishing. . . 259
the fish from the hooks and line. But solar energy fitted lights are bright
which enabled us to handle the fish and hooks and line without much stress. It
also saved considerable amount of time.” Mr. Salin, another crew said that they had
full lighting in their boat. The other fishing boats and ships passed over by them
gave a strange look because of the unusual brightness in their boat. He added that
usually they are stingy or miser in using lights during night because of the
recharging problem. But with the solar energy, they are encouraged to use the
lights for the whole nights. Mr. Sunil said that they could save approximately 320 l
of diesel in this voyage. Cost wise, they could save an amount of INR. 19,200
(320 l� INR. 60).
Table 20.1 The economics of using solar energy in fishing boats calculated from the Thoothoor experience
Sl.
No. Parameter Units Conversion
1. Number of fishing boats in Thoothoor 600
2. Fuel required to run engine for one hour 10 l
3. Extra running of engine ( mainly during night time) 03 h
4. Number of fishing days in one year 250
5. Cost of fuel- diesel per litre INR. 60 USD. 1
By switching off the engine for 3 h and running it on solar power:
6. Saving of fuel per year for 1 boat� 30 l� 250 fishing days 7500 l 7. Saving of fuel per year for 600 boats� 30 l� 250 fishing
days 45,00,000 l
8. Potential cash savings per year per boat (7500� INR. 60) INR. 4,50,000 USD. 7500 9. Potential cash savings per year for
600 boats� INR.4,50,000 INR. 27,00,000,00
USD. 45,000,00
10. Approximate cost for 1kw solar power plant including
modification of wheel house and other fitting charges
INR. 2,50,000 USD. 4167
11. Approximate cost for installing 1kw solar power plant each in 600 boats including modification of wheel house and other fitting charges INR. 2,50,000� 600
INR. 15,00,000,00
USD. 25,000,00
12. Net saving to a boat per year INR. 2,00,000 USD. 3333
13. Net saving to 600 boats INR. 12,00,000,00
USD. 19,998,00
Environmental benefits by reducing Carbon Emission:
14. Emission of CO2 per litre of diesel consumption 2.60 kg
15. Potential reduction in emission of CO2 (1 boat� 7500 l� 2.60 kg)
19,500 kg 19.5 ton
16. Potential reduction in emission of CO2 (600 boats� 7500 l� 2.60 kg)
117,000,00 kg 11,700 ton
260 J.V. Jain and S. Babu
Solar Power for Multi-Day Fishing Boats
This initiative was based on the successful trial and subsequent operation of solar
energy system in the deep sea fishing boats. Generally, fishermen carry charged
battery in boats for lights and for the operation of navigational and safety equip-
ments. Recharging will be a major problem for smaller boats. They need to run the
engine exclusively for recharging because while fishing, they do not run the engine.
Running the engine for recharging is highly expensive and affects the income. The
major expenditure in each fishing voyage is fuel. The department of fisheries,
Government of Tamil Nadu is supplying 250 l of kerosene for one month at the
cost of INR. 25 per litres. But, it is sufficient for only one voyage. The duration per
voyage is 5–6 days. They buy from the black market for their requirements and the
cost per litre varies from INR. 40 to INR. 45. It is expected that the solar energy
system will help them to save fuel cost and will be a boon to the community
(Fig. 20.2).
Fig. 20.1 Solar power equipped boat (funded by National Bank for Agriculture and Rural Development (NABARD))
20 Specific Applications/Examples: Use of Solar Energy in Fishing. . . 261
Solar Lanterns for Catamaran Fishermen and Fish Vending Women
The solar lantern uses solar energy and helps to reduce carbon emission and free
from the risk of fire. The emission of carbon in 1 litter kerosene is 3 kg. Solar
Lanterns are environmental friendly and can be used even in remote villages where
there is no electricity. Even in the urban areas people prefer a solar lantern as an
alternative during power cuts because of its simple mechanism. Photovoltaic cells
are solid-state semiconductor devices that convert Solar Energy into Electricity
(direct current). These Solar cells are connected in series or in parallel to obtain
desired output and are called solar modules. Solar lantern is a simple application of
solar photovoltaic technology, which has found good operations in rural regions
where the power supply is irregular. ADSGAF initiated to encourage the fish
vending women and Catamaran fishermen to use solar lanterns for their occupa-
tional operations.
Fish Vending Women use Candles
Generally fish vending women use candles or kerosene lamps at the fish markets.
These lights are not safe and not bright enough to use in the market. Poor quality
Fig. 20.2 Solar power equipped multi-day fishing boat
262 J.V. Jain and S. Babu
and irregular lighting blights lives. The light and the smoke from kerosene lamps
not only strains eyes but also release harmful carbon and also there is risk of fire
(Figs. 20.3 and 20.4).
Catamaran Fishermen Use Solar Lantern
Catamarans,1 those engage in fishing either at day or at night which operate
generally one man manually. During night they use kerosene lamps or gas lights
for handling fishing gears, overseeing the fishing accessories etc. The kerosene
lights don’t have brightness unlike the gas lights. The kerosene lights are not water proof (Fig. 20.5; Table 20.2).
Cost Benefit Analysis
No of working days in a year are 250 (Tables 20.3, 20.4, and 20.5).
Many types and designs of solar lanterns are available with a price range. They
are ideal for not only fish vendors or fishers but also good for farmers and other
vendors, and children to read and write. Solar lights can also be used at home as
light after the sunset. They are highly durable and having longer life than other
lanterns. Solar lanterns would be cheaper than kerosene in the long run but the short
Fig. 20.3 Fish vending women use candles
1 Catamaran is a fishing craft, made of logs of Albizzia falcataria timber lashed together with rope.
20 Specific Applications/Examples: Use of Solar Energy in Fishing. . . 263
Fig. 20.4 Fish vending women use solar lantern
Fig. 20.5 Solar lantern fitted catamaran
264 J.V. Jain and S. Babu
run cost is higher. There are no authorized gas filling stations and it is always a
problem to the fishermen for filling gas for every fishing voyage. The fishermen
may not be in hurry or may not be in worry in gas filling of every fishing voyage, if
they have solar lanterns. Solar lanterns are safe and easy to handle and no need to
pay recharging fee. We could eliminate unauthorized gas filing stations run by some
people in the villages.
Table 20.2 Gas lights, kerosene lamp and candle VS solar lanterns
Sl.
N
Problems identified in using of Gas lights, Kerosene
lamp and candle Merits of the use of solar lanterns
1 Harmful effects—breathing of smoke There is no harmful effect to
health
2 The brightness of candle/kerosene lamp is not
sufficient
The solar lanterns are brighter than
candle/kerosene lights
3 Can’t keep the candle/kerosene lamp when it is windy
Can keep the solar lanterns when it
is windy
4 Need utmost care in using Easy to handle
5 Risk of fire No risk
6 Non availability of gas/kerosene on time Can charge at all sunny days
7 Need to pay for candle, kerosene, and gas filling
charge every day
One time investment
8 Gas lights are water proof but corrosion No corrosion
Table 20.3 In the case of a fish vending woman who use
candle
Particulars INR USD
1 Candle expenditure per day 20 00.33
2 The total cost is (20� 250 days) 5000 83.00 3 The cost of 1 solar lantern is 1800 30.00
4 Total saving in an year 3200 53.00
Table 20.4 In the case of a Catamaran fisherman who use
Kerosene
Particulars INR USD
1 Kerosene expenditure per day 60 01.00
2 Total cost in an year (60� 250) 15,000 250.00 3 The cost of a solar lantern is 2800 46.70
4 Total savings in an year 12,200 203.30
Table 20.5 In the case of a Catamaran fisherman who
use gas
Particulars INR USD
1 Gas filling expenditure per day 70 01.17
2 Total cost in an year (70� 250) 17,500 291.70 3 The cost of a solar lantern is 2800 46.70
4 Total savings in an year 14,700 245.00
20 Specific Applications/Examples: Use of Solar Energy in Fishing. . . 265
Solar Powered Refrigerated Trucks for the Transportation of Fresh Fish
The dispersed and distant living population requires proper means for food preser-
vation and distribution without its spoilage. The existing food preservation and
transportation technology has developed sufficiently to preserve the wide variety of
foods for a considerable long time without losing the freshness. In the case of fish, a
highly perishable commodity needs best preservation and transportation to avoid
spoilage and to maintain freshness. This is significantly enhancing the costs—both
capital and operational. The ADSGAF has initiated a means of reducing the
operational expenses of refrigerated transport using solar power (Fig. 20.6).
Features
• Fuel not required for operation of the system
• Alternate system is arranged, if solar system fails
• Better reliability, simple and versatile
• Easy to operate
• Money and fuel saving
• Back up for night operation (Table 20.6).
Fig. 20.6 Solar powered refrigerated truck (funded by National Fisheries Development Board, Government of India)
266 J.V. Jain and S. Babu
The Larger Picture
India has a fleet size of 1,94,490 crafts comprising 72,559 (37.3%), mechanized
crafts, 71,313 (36.7%) motorized crafts and 50,618 (26%) non-mechanized crafts.2
It indicates that 1,43,872 (74%) of the fishing crafts depends on fossil fuel either on
diesel or kerosene. If 1 l of fuel is saved per day, the daily fuel saving will amount to
1,43,872 l (0.15 million) and reduction of carbon emission will amount to a total of
(1,43,872� 2.6) 3,74,067 kg (374 ton) day. Assuming that the Indian fishing fleet fishes for 250 days in a year, the total fuel saving will amount to 35.97 million litres
and the carbon reduction will amount to 9,35,167,50 kg (93,516 ton)
(3,74,067� 250 fishing days). The cash saving in a day will be INR. 8,63,232,0 (USD. 14,387,2) and in a year will be INR. 2,15,808,00,00 (USD. 35,968,00).
Ongoing Programme
Based on the immediate and future needs in the fisheries, the community
established a SIGHT3 under IEEE4 called Artisanal Deep Sea Fishers SIGHT.
The main objective of the SIGHT is to develop ideas, concepts, projects and
products with the help of existing scientific know-how, managerial efficacy and
engineering expertise and along with the traditional knowledge of fishermen.
Presently the ADSGAF is on the process of introducing solar powered OBM5 fitted
boats, solar powered small ice-making units and tricycles for fish vending women
and also establishing solar power charging stations.
Table 20.6 Description of solar powered refrigerated truck
Sl.No Particulars INR USD
1 Cost of Vehicle
Mahindra Mxi Truck Plus
5,23,000 8717
2 Cost of body building with PUF insulation 2,10,000 3500
3 Cost of refrigeration
Refrigerant-R134a
2,70,000 4500
4 Cost of solar system (1.5 KW)
Solar panels 250 W� 6 1,50,000 2500
5 Total 11,53,000 19,217
2As per the 2010 National Marine Fisheries Census conducted by the CMFRI, Kochi. 3 Special Interest Group on Humanitarian Technology. 4 Institute of Electrical and Electronic Engineers. 5 Out Board Motor.
20 Specific Applications/Examples: Use of Solar Energy in Fishing. . . 267
Suggestions
The initial investment cost of the solar power projects is high. People do not realize
the long term benefits. Hence it is necessary to organize intensive awareness
programmes to motivate the public to undertake investments in such projects.
Further the people have to be familiarised with the handling of solar power
equipments. There is need for conducting regular training sessions for handling
solar equipments. It is necessary to establish after sale services and also make
available solar power parts locally which are lacking today and which is one of the
major reasons for lack of interest using solar power systems. It is necessary to
increase the number of quality technicians in this field. It is also necessary to do
more study, experimentation and need sufficient funding to bring out right combi-
nation of goods and services in the fisheries.
Conclusion
From the energy consumption, sustainability and cost perspectives, there is an
urgent need for initiatives that reduce fuel consumption, substituting carbon-
based fuels with renewable alternatives. The initiatives taken by the community
that promote reducing the operating costs minimize dependency of fossil fuel and
minimize the carbon emission. Thus use and application of solar energy will not
only be saving fuel, money, time but also help to minimize the carbon emission
which is one of the major problems for global warming. This will lead to green
revolution in the fisheries sector.
Acknowledgment The authors acknowledge the contributions of Dr. Y.S. Yadava, Director and Mr. Prajdeep Mukherjee, Policy Analyst BOBP-IGO, Chennai, India, Mr. V. Vivekanandan, Direc-
tor, FishMARC, Trivandrum, India, Mr. Sebastian Mathew, Executive Secretary, International
Collective in Support of Fishworkers, Chennai, India, Dr. E. Vivekanandan, Emeritus Scientist,
CMFRI, Chennai, India, Mr. Sadhish Kumar, Project Head, Jagath Jothi Solar Energy Pvt Ltd,
Chennai, India, Mr. Vivek Dwivedi, Managing Director, BRIJ EXIM, Pune, India, Dr. Chinnappan
Gasper, Professor, Centre for Development Studies, Trivandrum, India and Dr. Teresa Shobana,
Professor, St. Jude’s College, Thoothoor, Tamil Nadu, India in the preparation of this paper. Special thanks to BOBP-IGO for providing advice and support to the initiatives taken by ADSGAF.
References
Department of Economic and Social Affairs, World Economic and Social Survey 2008: Over-
coming Economic Insecurity, E/2008/50/Rev.1, United Nations, New York, 2008.
Wilson, J. D. K. (1999). Fuel and financial savings for operators of small fishing vessels. FAO Fisheries Technical Papers, 383, 46.
Vivekanandan, E., Singh, V. V., & Kizhakudan, J. K. (2013). Carbon footprint by marine fishing
boats of India. CMFRI, India. Current Science, 105(3), 10 August 2013.
268 J.V. Jain and S. Babu
Chapter 21
Diagnostic of Sensors for Induction Machine Powered by Photovoltaic Generator Based on Fuzzy Logic Techniques
A. Amrane, A. Larabi, and A. Hamzaoui
Introduction
Many industrial applications require fault tolerance and continuity of service
(Benbouzid et al. 2007). This is due to the growing need to improve the availability
of systems. Therefore, strategies are defined in the early stages of design, to
facilitate fault detection, localization and reconfiguration of the order. For this,
several recent works (Green et al. 2003; Abolhassani and Toliyat 2009) deal with
fault tolerant control of electric drives.
In this article, we focus our study on the induction machine (IM), conventionally
designed for constant speed applications, has become, due to its simple, robustness
structure and the evolution of electronics power and control of the control vector
machine most commonly used for variable speed drives. This machine has the
advantage of being more robust and less expensive, with equal power, as other
machines. However, it has drawn backs. This allowed the opening of various lines
A. Amrane (*) Laboratory of Systems Electric and Industrial (LSEI), Faculty of Electronics and Informatics
(FEI), University of Science and Technology (USTHB), BP 32, EIAlia, Bab-Ezzouar, 16111
Algiers, Algeria
National School of Technology, National Road N 5 Z.I., Rouiba, 16013 Algiers, Algeria
e-mail: [email protected]
A. Larabi
Laboratory of Systems Electric and Industrial (LSEI), Faculty of Electronics and Informatics
(FEI), University of Science and Technology (USTHB), BP 32, EIAlia, Bab-Ezzouar, 16111
Algiers, Algeria
e-mail: [email protected]
A. Hamzaoui
CReSTIC of Troyes University of Reims Champagne Ardennes Troyes, Reims, France
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_21
269
of research on its control and power (Shoudao et al. 2004; Montanari et al. 2000;
Ouhrouche 2002).
We introduced in this work, an approach widely used for the detection and
isolation of faults based on the method of estimator (Chen and Patton 1999; Holtz
1996), the main components of a tolerant control strategy to defects (CTD) sensor.
It is divided into three stages: detection, isolation and reconfiguration.
A novel estimator schemes based on fuzzy logic algorithm for the speed estimation
where derived using Lyapunov’s stability theorem (Ouhrouche 2002; Amrane and Larabi 2012; Amrane et al. 2014). Several strategies have been proposed for the
estimation in the vectorial inductionmotor drives (Ouhrouche2002;Amrane andLarabi
2012; Amrane et al. 2013). Among these techniques, model reference adaptive systems
(MRAS) schemes are the most common strategies employed due to their relative
simplicity and low computational effort (Amrane andLarabi 2012;Amrane et al. 2013).
Can be seen, the majority of estimation schemes described in the literature for
MRAS observer employ a PI controller to generate the desired value. However, due
to the continuous variation in the machine parameters and the operating conditions,
in addition to the nonlinearities present in the inverter, the PI controllers may not be
able to provide the required performance. Not much attention has been devoted to
study other types of estimation scheme (Amrane and Larabi 2012; Amrane
et al. 2013; Larabi et al. 2013).
In this article, the performances of the diagnostic of sensors, the detection of
faults and the fuzzy estimation of speed for the induction machine are analyzed by
digital simulation. To achieve our objective, this paper is organized as follows.
Section “Introduction” presents the control of the asynchronous machine; the rest of
the paper is organized as follows. Sections “Control of Asynchronous Machines” and
“Sensorless Control of the Induction Machine” present the control of the IM and the
MRAS algorithm using to estimate the speed. Section “The Fuzzy Logic Adaptation”
depicts fuzzy logic algorithm for the estimation. Section “Modelisation and Control
of Generator Photovoltaique” provides and discusses the simulation results and
Section “Simulation Results” sketches some conclusions.
Control of Asynchronous Machines
Control Scheme of an Asynchronous Machine
Figure 21.1 shows a simplified block diagram illustrating the essential of our
control system. This system consists of a dc power source, a dc link filter, a voltage
source inverter, an induction motor, and same circuit of control system. The dc
power source converts the constant-frequency ac power to dc power by a three-
phase, full wave diode bridge rectifier; the dc voltage is smothered by a smoothing
capacitor dc link filter and then applied to a three-phase bridge inverter witch
converts dc power to variable voltage variable frequency ac power supply to the
motor. The two control parameters required are frequency and voltage, the fre-
quency command also generates the voltage command through a volts/hertz ratio.
270 A. Amrane et al.
Induction Machine Model
The considered system is an induction machine with a squirrel cage of three phases.
The state representation of the mathematical model of this machine can be
represented according to usual d-q axes, as follows (Ouhrouche 2002; Amrane
and Larabi 2012; Amrane et al. 2013, 2014; Ho and Yeh 2010)
d ids
dt ¼ 1= σ*Lsð Þ -Rsm* idsþ ωs*σ*Ls* iqsþ Lm
Lr*Trð Þ *φdr � �
d iqs
dt ¼ 1= σ*Lsð Þ -Rsm* iqs-ωs*σ*Ls* ids- Lm
Lr*Trð Þ *φqr � �
d φdr
dt ¼ Lm
Tr *ids-
1
Tr *φdrþ ωs� ωrð Þ*φqr
d φqr
dt ¼ Lm
Tr *iqs-
1
Tr *φqr� ωs� ωrð Þ*φdr
Cem ¼ P*Lm Tr
iqs*φdr-φqr*idsð Þ d Ωr
dt ¼ 1
Tr Cem-Cr-Kf*Ωrð Þ
ð21:1Þ
Indirect Field-Oriented Control of an Induction Machine
This technique consists in assimilating the behaviour of asynchronous machine to
the DC machine; this is for applications requiring raised dynamic performances
(Montanari et al. 2000; Amrane et al. 2013; Larabi et al. 2013; Louri et al. 2013).
The aim of such a control technique of the torque and a choice of the (d,q)
reference, in order to obtain a decoupling between the torque and the field. From
Machine powered by
photovoltaic generator
Sensor speed
+ - DC
Power source
DC/AC Convert
M
Control system
Fig. 21.1 Block diagram of control system
21 Diagnostic of Sensors for Induction Machine Powered by Photovoltaic. . . 271
equation system (21.1); the torque control is made on the components of current iq
and is. The electromagnetic torque depends only on component iq. It is a maximum
for a given current if we impose is¼ 0. Consequently the obtained torque is then proportional to the current of machine power supply as in case of separately excited
DC machine. The model given by Eqs. (21.1) is expressed as follows:
Vds ¼ σ*Ls* d ids dt
-1= σ*Lsð Þ -Rsm* idsþ ωs*σ*Ls* iqsþ Lm Lr*Trð Þ *ϕdr
� �
Vqs ¼ σ*Ls* d iqs dt
-1= σ*Lsð Þ -Rsm* iqs-ωs*σ*Ls* ids- Lm Lr*Trð Þ *ϕqr-ωr*
Lsr
Lr *ϕdr
� � d ϕdr
dt ¼ Lm
Tr *ids-
1
Tr *ϕdr
ωs ¼ Lm Tr
* iqs
ϕdr þ ωr
Cem ¼ P*Lm Tr
iqs*ϕdrð Þ d Ωr
dt ¼ 1
Tr Cem-Cr-Kf*Ωrð Þ
ð21:2Þ
It is noted that rotor flux depends only on the satatoric current is and iq, that the
electromagnetic couple depends only on the quadratic current iq.
Sensorless Control of the Induction Machine
The Structure of Model Reference Adaptive System MRAS
The aim of this technique of control is to replace the speed sensor by a speed
estimator. Into our study, we introduced a speed estimator of type MRAS (Model
Reference Adaptive System). The latest replace the mechanical sensor without
changing the dynamics of our machine.
The principle of the method MRAS speed estimation rests on the comparison of
the sizes obtained in two different ways. One model of such a method is the voltage
one (or stator equation) and the other is current model (or rotor equation); because
the voltage method doesn’t include rotor speed then it does not depend explicitly of speed (model of reference) and the other includes rotor speed (adjustable adaptive
model). Figure 21.2 illustrates the derived MRAS scheme for speed adaptation.
Reference Model
One uses the equations of the currents (21.2) of the IM, the current expressed in the
reference fixed to the stator. The two equations of the model of reference become:
272 A. Amrane et al.
d φαr
dt ¼ Lr
Lsr Vαs-σ*Ls*
diαs
dt -Rs *iαs
� � dφβr
dt ¼ Lr
Lsr Vβs-σ*Ls*
diβs
dt -Rs *iβs
� � ð21:3Þ
Adjustable Model
To establish the adaptive model, we expressed the current in the reference fixed to
the stator, the fluxes expressed with the rotor sizes in a reference αβ are:
d φαad
dt ¼ - 1
Tr φαadþ Lsr
Tr *iαs -P *Ωest*φβad
d φβad
dt ¼ - 1
Tr φαadþ Lsr
Tr *iβs -P *Ωest*φαad
ð21:4Þ
Adaptation Mechanism
The entry of an adaptive mechanism is activated by the error between the reference
field and adaptive field. By carrying out the difference between the reference model
and the adjustable model, we obtain the following system of equations which
govern the adaptive mechanism.
deα
dt deβ
dt
2 64
3 75 ¼ �
1
Lr �ω
ω � 1 Lr
2 64
3 75þ ω� ωadð Þ φαad
φβad
� � ð21:5Þ
The adaptation law chosen to ensure the convergence of ωad towards ω is:
Fig. 21.2 Structure of MRAS estimation of speed
21 Diagnostic of Sensors for Induction Machine Powered by Photovoltaic. . . 273
ωad ¼ Tp*δeþ Ti ðt 0
δe*dx ð21:6Þ
The adaptive mechanism has an integral proportional form:
ωest ¼ 1� P * Tp*eþ Ti
ð e*dt
� � ð21:7Þ
where Tp and Ti are positive gain.*
The Fuzzy Logic Adaptation
Control by Fuzzy Logic
Fuzzy logic technique makes it possible to control nonlinear systems and compli-
cated models (Amrane et al. 2013, 2014; Larabi et al. 2013). In fact, the calculation
of the parameters of the system is not necessary to carry out this control (Amrane
et al. 2013, 2014; Larabi et al. 2013).
On opposite of the adaptation of the traditional techniques; the fuzzy logic does
not treat a mathematical relations well defined, but uses inferences with a several
rules, being based on variables linguistic.
These inferences are treated by operators suitable for fuzzy logic (Amrane
et al. 2013, 2014; Larabi et al. 2013). Figure 21.3 shows the structure of a fuzzy
regulator with two input (X1 and X2) and one output (Xr).
So, we can note that the calculation of the control is carried out starting from
three fundamental stages: an interface of fuzzification; a mechanism of inference
(rules); and an interface of defuzzification.
The Fuzzification
The entries and exits are defined of the fuzzy are defined by membership functions
with 7, 5 or 3 sets. The various sets are characterized by standard designations
(Amrane and Larabi 2012; Amrane et al. 2013; Larabi et al. 2013):
X1 X2
Xr
FUZZY CONTROL
RULES DEFUZZIFICATIONFUZZIFICATION
Fig. 21.3 Functional diagram of the fuzzy control
274 A. Amrane et al.
Negative Big NB, Negative Medium NM, and Negative Small NS, Zero Z,
Positive Small PS, Positive Medium PM, Positive Big PB.
Inference Mechanism
It is well known that the realizations of the matrix of the rules are deduced by
experiment, the experiment of the human operators and rests on the analysis of the
system.
This analysis must take into an account the trajectory which one wants to give to
the system (Amrane and Larabi 2012; Amrane et al. 2013; Larabi et al. 2013).
The Defuzzification
By this stage; the return to the sets of real exit will be made. It is a question of
calculating, from the degrees of membership of all the sets variable of output, the
coordinate which corresponds with the value of this exit. Various methods are used
(Amrane and Larabi 2012; Amrane et al. 2013; Larabi et al. 2013).
The Fuzzy Logic Adaptation Mechanism Principle
The structure of the proposed PI controller used in the adaptation mechanism will
be replaced by a fuzzy logic controller as shown in Fig. 21.4.
In our work, we adopted seven sets for the two variables of input (En and dEn),
and a same number of sets for the variable of output dUn. The rules of the controller
can be presented in a matrix with seven sets known as matrix of inference shown in
Table 21.1.
In this article, the memberships function are chosen as the triangular type and
trapezoidal, and the method of reasoning is considered as the max-min method, the
UK3
Fuzzy contr oller
Z-1
E
K1
K2
Fig. 21.4 Synoptic diagram of a fuzzy adaptation
21 Diagnostic of Sensors for Induction Machine Powered by Photovoltaic. . . 275
defuzzification stage is done based on the gravity centre method, as it is frequently
quoted in the literature and because they requiring less time computing will be also
adopted in our work (Amrane et al. 2013, 2014; Larabi et al. 2013).
The Basic Rules of the Fuzzy Controller
The first step in the design of fuzzy controller is to generate fuzzy rules based on the
knowledge of the expert. According to the expert, three situations can be distin-
guished for the constant time estimation, above, around and below the reference
desired.
In our control, in order to determine the rules table that generates a command
that will be presented later Based on Fig. 21.5.
Modelisation and Control of Generator Photovoltaique
To profit from solar energy and to use it to power the IM, it is necessary to
understand the operation of this energy and optimize its use. In this way, we are
interested here, to describe the basic concepts of solar energy and the production of
electricity by the photovoltaic effect.
The connection of a generator PV to a load requires the adaptation of the
generator so that it functions with its maximum power, and then to provide the
maximum of energy delivered by the generator to the load, it is permanently
necessary to track the corresponding that called Maximum Power Point (MPP).
So, to provide this we try here to adapt the photovoltaic generator (PVG) to the
asynchronous machine. This adaptation between the source and the load is carried
out by the insertion of a converter DC-DC (chopper) controlled by a tracking
mechanism of Maximum Power Point. This method is known as MPPT (Ho and
Yeh 2010; Agrebi et al. 2006).
Table 21.1 The fuzzy rules (a regulator with five sets)
dUn
En
NG NP EZ PP PG
dEn NG NG NG NP NP EZ
NP NG NP NP EZ PP
EZ NP NP EZ PP PP
PP NP EZ PP PP PG
PG EZ PP PP PG PG
276 A. Amrane et al.
Model of a Generator Photovoltaic
The mathematical model of the physical process in (Ho and Yeh 2010; Agrebi
et al. 2006; Peng and Fukao 1994) a PV cell are given in figure (Fig. 21.6), known
under the name “two-diode model”, it is largely used in the literature. It is most
widespread because it gives the results closest to those obtained by a real GPV.
So, to obtain the wished values of the tensions and currents, the modules are
connected in series, parallel or parallel-series. The later association “parallel-
series” enables us to obtain the values of the tension and the desired current. The
characteristic equation of the system is given by the following relation:
I ¼ NP � IPh � NP � Is1 exp q NPV þ Ns � I � Rseð Þ½ � NsNPA1KT
� � � 1
� �
� NP � Is2 exp q NPV þ Ns � I � Rseð Þ½ � NsNPA2KT
� � � 1
� � � NPV þ Ns � I � Rseð Þ½ �
NsNPRPe
ð21:8Þ
With:
I and V: the current and the voltage of the photovoltaic cell.
q: the constant elementary charge.
Iph: the photocurrent produced.
K: the Boltzmann constant.
IS1 and IS2: the saturation currents of the diodes.
A1 and A2 factors of purity of diode (A1¼ 1 and A2¼ 2).
Reference
C1
P1
P2 P3
P4
P6
P5
C2
C3
C4
C5
C6
time
Polarities of E et dER e s p o n
Fig. 21.5 Temporal analysis of the rules of the regulator
21 Diagnostic of Sensors for Induction Machine Powered by Photovoltaic. . . 277
IPh ¼ IPh �� T¼298ð Þ � 1þ T� 298ð Þ � 5� 10�4
� with IPh
�� T¼298ð Þ ¼ 3:25 A
RS and RP: respectively resistance series and parallel resistance.
T: the absolute temperature �K.
IS1 ¼ K1T3e � Eg KT and IS2 ¼ K2T 52 e
� Eg KT
Eg: The energy band of the semi-conductor
K1¼ 1.2 A/Cm2 K3 and K2¼ 2.9 105/2 A/Cm2 K5/2
GPV Control
To convert solar energy with the best manner possible, it is essential to work in the
zone of maximum power of generator. In other words, they need to track the MPP in
order to maximize the power delivered to load by ordering converter DC/DC. There
are different control methods of tracking of the point of maximum power, based rest
on the generator power-tension characteristic (Ho and Yeh 2010; Agrebi
et al. 2006; Peng and Fukao 1994).
The approach of artificial fuzzy logic intelligence is implemented to improve the
performances of control and to track the point of maximum power, by the modelling
and the simulation of a controller containing fuzzy logic (FLC) (Fig. 21.7).
The fuzzy controller proposed has two variables of entries, the error E and the
variation of error CE, are expressed at a rate of sampling K. They are defined as
follows:
E kð Þ ¼ P kð Þ � P k� 1ð Þ V kð Þ � V k� 1ð Þ ð21:9Þ
CE kð Þ ¼ P kð Þ � P k� 1ð Þ
With: P (k) ET V (k): are respectively the power and the tension of PVG.
Once the two sizes of entry is calculated and converted into fuzzy linguistics
variable, the exit which is the variation of the cyclic report dα, as mentioned in table (Table 21.2), intended to control a chopper back-booster. The control rules must be
indicated so that the entry variable E must be always zero.
IID ID2 IRP
IPh D1 D2 RP V
Fig. 21.6 Model of solar cell
278 A. Amrane et al.
The synoptic diagram of the chain PV: Photovoltaic generator—Converters—
Induction Machine—Battery is given by Fig. 21.8.
Simulation Results
To diagnose the speed sensor, a MRAS estimator is used as an observer. Then, an
algorithm for selecting is used to enable the detection of defects and perform the
selection between the measured signals and the estimated signals.
So, to validate the performances of the MRAS, the proposed simulation of the
dynamic behaviour of the machine has been done using the MATLAB/SIMULINK
and that for the following conditions.
With, the value of the torque is fixed to zero and the field is fixed to 1 Wb. To
highlight the influence of speed variations and uncertainties, particularly those of
the control process, we gave reference speed of 100 rad/s (Fig. 21.9).
Afterwards, constant field and a reference speed Ωref¼ 100 rad/s, the field rotor field is fixed to 1 Wb, the initial values of the torque assumed by the machine is
zero, and between 1 s and 2.5 s, one will apply a nominal torque load (10 N.m)
(Fig. 21.10).
Finally, we will use our estimator to diagnose faults sensor for speed exceeds the
rated speed to a value of the torque is fixed to zero, the field is fixed to 1 Wb and the
initial values of the speed assumed by the machine is zero, and between 1 s and
2.5 s, we will apply variations (Fig. 21.11).
According to the simulation results we can say that the MRAS technique of
detection provides an effective solution to the problem of diagnostic. We can say
that our objective here has been successfully achieved.
Fig. 21.7 Structure of the fuzzy controller for the tracking of the PPM
Table 21.2 The fuzzy rules for algorithm MPPT
(a regulator with five sets) dα
En
NL NS Z PS PL
dEn NL Z Z PS NS NL
NS Z Z Z NS NL
Z PL PS Z NS NL
PS PL PS Z Z Z
PL PL PS NS Z Z
21 Diagnostic of Sensors for Induction Machine Powered by Photovoltaic. . . 279
The results presented on the previous figures, show that the dynamics of the flux
magnitude are presented can highlight the decoupling role of the flux controller
where the flux tracks its nominal value of 1.1 Wb for all speed ranges.
The MRAS observer has an advantage of avoiding integration of stator voltages,
which is of particular interest for hardware implementation. The proposed MRAS
strategy has been incorporated within the classical IM control system. Numerical
simulations are performed and shown good results for tricking the reference.
Implementation of the proposed algorithm can be used for the diagnostic issues
suitable for IM applications requiring high-performance.
Fig. 21.8 Total structure of the photovoltaic chain
0 0.5 1 1.5 2 2.5 3 -20
0
20
40
60
80
100
120
time(S)
s pe
ed (r
ad /s
Wsen
West
Fig. 21.9 Estimation of speed in the case of an indirect field oriented of the induction machine, speed reference (Wref), estimated speed (West) and speed with sensor (Wavec). With the torque is
fixed to zero and the field is fixed to 1 Wb and the speed fixed to 100 rad/s
280 A. Amrane et al.
s pe
ed (r
ad /s
0 0.5 1 1.5 2 2.5 3 -20
0
20
40
60
80
100
120
time(S)
Wsen West
Fig. 21.10 Estimation of speed in the case of an indirect field oriented of the induction machine, speed reference (Wref), estimated speed (West) and speed with sensor (Wavec). With the torque is
fixed to 10 N.m and the field is fixed to 1 Wb and the speed fixed to 100 rad/s
0 0.5 1 1.5 2 2.5 3 -50
0
50
100
150
200
time(S)
sp ee
d( ra
d/ s
Wsen West
Fig. 21.11 Estimation of speed in the case of an indirect field oriented of the induction machine, speed reference (Wref), estimated speed (West) and speed with sensor (Wavec). With the torque is
fixed to zero and the field is fixed to 1 Wb and between 1 s and 2.5 s, we will apply variations of
speed
21 Diagnostic of Sensors for Induction Machine Powered by Photovoltaic. . . 281
Conclusion
The work that we presented contributes to the analysis and the synthesis of a robust
diagnostic applied to the induction machine. The MRAS is employed for the
detection of the faults of sensor speed. The use of the fuzzy logic is a powerful
tool in realization of the robust and reliable diagnostic.
We have proposed a method for detection faults of sensor speed using the MRAS
and the fuzzy logic algorithm, to ensure a good diagnostic of induction machines.
The method proposed in this paper is applicable to a large category of induction
motor drives with a gradually varying load torque. The tests of robustness show
clearly that the performances of the diagnostic in the presence of estimator, type
MRAS, for the tracking the references is always fast. The validity of this method is
checked by several tests.
The results obtained show that the model suggested for the MRAS adapts
perfectly to all the diagnostic of the IM.
The next step of this work is the integration of a real induction motor and
estimator MRAS for testing the diagnostic is required for the practical case.
Annexes
The parameters of the induction machine cage used are shown below:
Rated power: 1.5 kw
Nominal voltage: 220/380 V
Rated power factor: 0.8.Rated
Speed: 1420 rev/min
Nominal frequency: 50 Hz
Stator resistance: 4.85Ω
Rotor resistance: 3.805Ω
Stator cyclic inductance: 0.274 H
Cyclic inductance of Rotor: 0.274 H
Cyclic mutual inductance: 0.258 H
Number of pole pairs: 2
Moment of Inertia: 0.031 Nm-s2/rad
Friction: 0.008 Nms/r
Nomenclature
Ls Stator inductance [H]
Lr Rotor inductance [H]
Lm Mutual magnetizing inductance
282 A. Amrane et al.
Lsr Mutual Inductance between the stator and rotor [H]
Kf Friction coefficient [N.s/rad]
J Total inertia [kg.m2]
P Number of pole pairs
ωs Synchronous Pulsation [rad/s] ωr Electrical angular Pulsation [rad/s] Cem Electromagnetic torque [N.m]
Cr Resistive torque [N.m]
Tr Rotor time constant [s]
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Chapter 22
Air Conditioning Based on Hydroxides with Solar Driving for Low GHG Emissions
R.J. Romero, S. Silva-Sotelo, Y.R. Galindo-Luna, C.V. Valdéz-Morales,
J. Ibarra-Bahena, A. Hdz-Jasso, and A. Rodrı́guez-Martı́nez
Introduction
There is a large amount of energy transformed in several ways. Ranging from the
clean use for the environment such as solar energy is the energy that is taken
directly from the sun, which with various processes is transformed into mechanical
energy and then transformed to power. Other clean energy to the environment is
nuclear energy, which is generated by reactions usually radioactive chemical
elements, this type of energy promises much but may be dangerous at the same
time; if that is not under controlled handled conditions. Some people do not
consider it as clean source of energy production due to highly toxic waste than
generates it.
Another clean energy is hydropower, which involves harnessing the potential
energy accumulated in the water to generate electricity, is a classic form of energy.
About 20% of the electricity used in the world comes from this source.
In the world today most of the energy used (60–70%) is generated by burning
fossil fuels, which have been generated over the years many waste from the
combustion of these have caused a negative impact to the environment to be the
main pollutants of this, the problem with the use of fossil fuels to generate energy is
not renewable, is that fewer and fewer of these fuels, and to use excessive release of
GHG and another contaminants.
According to International Energy Agency Moreover we have the domestic air
conditioners which take a very important role in the big cities and they generate
about 20–30% of the total to the urban emissions atmosphere.
R.J. Romero (*) • S. Silva-Sotelo • Y.R. Galindo-Luna • C.V. Valdéz-Morales J. Ibarra-Bahena • A. Hdz-Jasso • A. Rodrı́guez-Martı́nez
Centro de Investigaci�on en Ingenierı́a y Ciencias Aplicadas, Universidad Aut�onoma del Estado de Morelos, Av. Universidad 1001, Chamilpa 62209, Morelos, Mexico
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_22
285
OECD countries supplies almost 40% of primary energy in the world, but
consumption in the OECD are large as the population number. The OECD con-
sumption for 2012 was 3582 Mtoe from 8980 World’s total consumption. That is practically the 40% of the total. OECD renewable energies for 2012 were geother-
mal 32 Mtoe, hydropower 119 Mtoe and Solar + Tide +Wind energies 48 Mtoe.
These renewable balances are 5.5% of the OECD consumption. Biggest energy
consumption is based on oil. See Figs. 22.1, 22.2, and 22.3 taken from “2014 Key
World energy statistics” by International Energy Agency.
Solar Air Conditioning Proposal
Solar air conditioning is an old dream for technician from worldwide. A proposal
for solar absorption air conditioning for building space cooling is due to the
coincidence between the availability of maximum solar irradiance and the
Fig. 22.1 Regional total primary energy supplies at
2012 (© iea.org)
Fig. 22.2 World Final consumption at 2012 (© iea. org)
286 R.J. Romero et al.
maximum load for cooling, particularly in office buildings. According to average
solar irradiance, the solar potential is available to provide the energy for the
air conditioning. An earlier patent for this concept was realized by on 1977
(Kumm 1979).
Figure 22.4 shows the global potential for installation of solar systems. Solar air
conditioning systems were studied from 1957 as a recent review reports (Siddiqui
and Said 2015). However there are some limitations for the implementation of the
thermodynamic cycle.
Fig. 22.3 OECD Final consumption at 2012
Fig. 22.4 Global solar irradiance map (© 3tier.com)
22 Air Conditioning Based on Hydroxides with Solar Driving for Low GHG Emissions 287
Description of the Hydroxide Based Solar System
Conventional air conditioning requires mechanical vapor compression by fossil fuel
driven. Electrical power energy into the compressor unit causes a pressure increase
in a gaseous refrigerant (typically an HCFC) and then condenses this at higher
temperature level to deliver the exchanged energy al lower temperature level in the
evaporator; as Fig. 22.5 shows.
Space cooling absorption technology from 14 to 22 �C requires heat supply from 100 to 150 �C while hydroxide blend is used as working pair (Romero et al. 2000). Solar collectors to drive an air conditioning system must be concentrators, cylin-
drical parabolic concentrator and evacuated tube collectors to heat at generator
temperature requirements. Additionally, photovoltaic cells must be installed to
drive the centrifugal pumps.
A HBAC system basically consists of an evaporator, a condenser, a generator, an absorber and an economizer as shown in Fig. 22.6. A quantity of waste heat QGE is
added at a relatively high temperature TGE to the generator to vaporize the working fluid from the solution. The vaporized working fluid goes to the condenser, where it
is condensed delivering an amount of heat QCO at an intermediate temperature TCO. The liquid leaving the condenser passes through a valve to the evaporator where it is
evaporated by means of a quantity of heat QEV at a low temperature TEV producing the cooling effect. After this, the vaporized working fluid goes to the absorber
where it is absorbed by the solution coming from the generator, delivering an
amount of heat QAB at an intermediate temperature TAB. Finally, the solution leaving the absorber is pre-heated in the economizer and returns to the generator
starting the cycle again.
CO
EV
P
T
1
2
3
4
QEV
QCO
WC
Fossil Fuel Energy
Compressor device
Fig. 22.5 Conventional air conditioning system
288 R.J. Romero et al.
Heat Transfer Effectiveness
Heat transfer effectiveness is a function of three thermal parameters (George and
Srinivasa Murthy 1989):
η ¼ XAB � XGE XAB EQ � XGE ð22:1Þ
Economizer effectiveness has been analyzed into refined thermodynamic cycle
for some authors (Romero et al. 2000; Balghouthi et al. 2005; Fabrizio et al. 2014;
Siddiqui and Said 2015). The effect for the economizer causes an internal energy
recover from absorber to the generator.
Results
From mass and energy balances, the power into the heat transfer components is
calculated as follow:
QEV ¼ MEV HGE,V � HCO,Sð Þ ð22:2Þ QGE ¼ MGE,V HGE,V þMGE,S HGE ,S �MAB,S HVA,S ð22:3Þ
Fig. 22.6 Proposal hydroxide based thermodynamic cycle for solar air conditioning system
22 Air Conditioning Based on Hydroxides with Solar Driving for Low GHG Emissions 289
QCO ¼ MCO � HCO,S � HGE,V
� ð22:4Þ QAB ¼ MCOHEV ,V þMGE,SHGE,S �MAB ,SHAB,S ð22:5Þ
COP ¼ QEV Qsolar
ð22:6Þ
COP is a dimensionless parameter that indicates the ratio between useful energy
and inlet energy. This parameter allows the comparison between air conditioning
devices. For this case, the effectiveness of the components were calculated and the
values for each are ηEV¼ 0.9, ηGE¼ 0.8, ηAB¼ 0.75, ηCO¼ 0.7 and ηHX¼ 0.7. This mass and energy balance was computed with the following algorithm
(Fig. 22.7).
The energy for drive the centrifugal pump into the cycle is assumed that comes
from photovoltaic panels to avoid fossil fuel derived energy. That power was
calculated as 2% of the air conditioning power. That value is 350 W at 12 VCD.
Figure 22.8 show the HBAC’s COP as function of solar energy temperature for constant temperature in absorber and condenser component. The air conditioning
keeps an insulated space at 20 �C. An optimal ideal condition for the hydroxide based air conditioning system is noted in this figure. This optimal condition requires
solar energy at 125 �C for ambient temperature at 40 �C and the COP is 0.7 than indicates the CPC energy is 25 kW for a 17.5 kW of air cooling load.
Figure 22.9 show the modified HBAC’s COP as function of solar energy temperature as in previous figure. The modified COP was computed with the
shown component effectiveness. The behavior for both lines in Figs. 22.8 and
22.9 are the same. But there is a variation in the value for the optimal thermody-
namic conditions. Solar energy is required at 120 �C for ambient temperature at 40 �C but the calculated COP is 0.5 that means the CPC energy is 31 kW for 15.5 kW of air cooling at same room.
The CPC area for this solar energy panel is 20% larger than the ideal cycle, and
the air conditioning load is diminished 11% anyway. The non-ideal calculation
leads to solar engineers to precise areas to fossil fuel free air conditioning systems.
Unfortunately at 2010 the air conditionings powers were higher than 25 GW as
shown Fig. 22.10, and the associated CO2 emission are higher as well. Solar air
conditioning systems as the proposal and others may reduce the CO2 impact to 2050
(iea.org 2011). OECD countries dominate the market for space and water heating,
but not for cooling. China leads the world for annual installed capacity of solar
thermal systems and air conditioners devices.
Conclusion
Hydroxide based solar air conditioning may be a proposal for CO2 reduction at
2050. The entire system drives with solar energy from CPC and photovoltaic
panels. The effectiveness addition for calculation of air conditioning leads to
290 R.J. Romero et al.
User data
Inlet
TSurroundings TAir conditioning
TSolarAir
conditioning
load QEV
Start
Pressure calculation
P= P (T)
Concentration computing
X = X (T, P)
Enthalpies calculation
H = H (T, X)
Mass balance
M = F (H, Q)
Power balance
M = F (H, Q)
COP evaluation with and without h COP = f (hEV, hCO, hAB, hGE, hHX, QSolar, QEV)
End
hEV, hCO, hGE,
hAB, hHX
Fig. 22.7 Algorithm for calculation of powers and COP for proposal system
22 Air Conditioning Based on Hydroxides with Solar Driving for Low GHG Emissions 291
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0 20 40 60 80 100 120 140 160
CO P
(d im
en si
on le
ss )
Solar Energy Temperature (°C)
TCO = 50 °C TAB = 50 °C TEV = 10 °C Tamb = 40 °C T Air Conditioning = 20 °C
Fig. 22.8 HBAC’s COP as function of solar energy temperature for ideal cycle
0
0.1
0.2
0.3
0.4
0.5
0.6
0 20 40 60 80 100 120 140 160
Solar Energy Temperature (°C)
hEV = 0.9, hGE = 0.8, hAB = 0.75, hCO = 0.7 and hHX = 0.7
TCO = 50 °C TAB = 50 °C TEV = 10 °C Tamb = 40 °C T Air Conditioning = 20 °C
CO P
(d im
en si
on le
ss )
Fig. 22.9 Modified HBAC’s COP as function of solar energy temperature
292 R.J. Romero et al.
lower COP values. For two selected scenarios the air conditioning load for 17 kW
requires solar energy of 25 kW in an ideal thermodynamic cycle. For a non-ideal
scenario the hydroxides-based air conditioning load with same flow is just 15.5 kW
and solar energy of 31 kW. Due all energy in the HBAC is solar, there is not GHG
compared with conventional compression air conditioning.
Acknowledgement To CEMIE-Sol P09 and CB-167434 by CONACYT—Mexico.
Nomenclature
H Enthalpy, kJ/kg
M Flow, kg/s
P Pressure, Pa
Q Power, W
T Temperature, �C W Mechanical power, W
X Hidroxide concentration, kg/kg
Greek Letters
η Effectiveness, dimensionless
Subscripts
AB Absorber
CO Condenser
Fig. 22.10 Sales and solar thermal installations for air conditioning at 2010
22 Air Conditioning Based on Hydroxides with Solar Driving for Low GHG Emissions 293
EV Evaporator
GE Generator
HX Economizer
S Liquid solution
Solar Solar
V Vapour
References
Balghouthi, M., Hachemi Chahbani, M., & Guizani, A. (2005). Solar powered air conditioning as a
solution to reduce environmental pollution in Tunisia. Desalination, 185, 105–110. Fabrizio, E., Seguro, F., & Filippi, M. (2014). Integrated HVAC and DHW production systems for
zero energy buildings. Renewable and Sustainable Energy Reviews, 40, 515–541. George, J. M., & Srinivasa Murthy, S. (1989). Influence of absorber effectiveness on performance
of vapour absorption heat transformers. International Journal of Energy Research, 13, 629–638.
International Energy Agency. (2011). Technology roadmap energy-efficient buildings: Heating
and cooling equipment. https://www.iea.org/publications/freepublications/publication/build
ings_roadmap.pdf.
Kumm, E. L. (1979). U.S. Patent No. 4,151,721. Washington, DC: U.S. Patent and Trademark
Office.
Retrieved March 26, 2015 from http://www.3tier.com/en/support/resource-maps/.
Retrieved March 26, 2015, from http://www.iea.org.
Romero, R. J., Rivera, W., & Best, R. (2000). Comparison of the theoretical performance of a solar
air conditioning system operating with water/lithium bromide and an aqueous ternary hydrox-
ide. Solar Energy Materials and Solar Cells, 63, 387–399. Siddiqui, M. U., & Said, S. A. M. (2015). A review of solar powered absorption systems.
Renewable and Sustainable Energy Reviews, 42, 93–115.
294 R.J. Romero et al.
Chapter 23
Life Cycle Analysis as a Decision Criterion for the Implementation of Solar Photovoltaic Panels in as Northeast Brazil Hospital
Monica Carvalho, Danielle Bandeira de Mello Delgado, and Ricardo Chacartegui
Introduction
The environmental performance of products, services and processes has become
one of the key issues in today’s world, and it is important to examine ways in which negative effects on the environment are assessed. One of the reasons for undertak-
ing a Life Cycle Assessment (LCA) study is that there are growing concerns about a
variety of environmental issues expressed by public opinion, political bodies and
industry. Environmental concern may be related to the long-term resource base of
human societies or may be more health related or it may be a concern for the natural
environment as such (Baumann and Tillmann 2004). LCA is one of the tools that
can be used for such a purpose.
LCA can be defined as the “compilation and evaluation of the inputs, outputs and
potential environmental impacts of a product system throughout its life cycle”
(Guinee et al. 2001). The objective of LCA is to describe and evaluate the overall
environmental impacts of a certain action by analyzing all stages of the entire
process from raw materials supply, production, transport and energy generation to
recycling and disposal stages—following actual use, in other words, “from the
cradle to the grave” (WEC 2004). The environmental burden covers all types of
impacts upon the environment, including extraction of different types of resources,
emission of hazardous substances and different types of land use. The term
M. Carvalho (*) • D.B. de Mello Delgado Department of Renewable Energy Engineering, Center of Alternative and Renewable Energy,
Federal University of Paraı́ba, Caixa Postal 5115, Cidade Universitária, Jo~ao Pessoa 58051- 900, Paraı́ba, Brazil
e-mail: [email protected]; [email protected]
R. Chacartegui
Energy Engineering Department, University of Seville, Camino de los descubrimientos, s/n,
Seville 41092, Spain
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_23
295
‘product’ is taken in its broadest sense—including physical goods as well as services; it includes goods and services at both operational and strategic levels
(Guinee et al. 2001).
Energy use and its associated primary energy consumption and emissions are
important contributors to the life cycle impacts of many products and processes, as
well as to greenhouse gas inventories of entities, products, and countries. LCA can
be used to calculate the environmental loads (e.g., emissions of greenhouse gases)
associated with the consumption of units of energy (electricity, heat, coolth, for
instance). In this way, alternative systems may be ranked according to their
respective emissions of greenhouse gases. The advantage of analyzing full life
cycles as opposed to using only emission factors is that renewable and nuclear
systems with no direct (stack) emissions can be compared with systems based on
fossil fuel combustion (WEC 2004).
There are actually two innovations presented herein: (1) utilization of environ-
mental data in the objective function of a mathematical model for the optimization
of an energy supply system, and (2) application of the methodology to a hospital
located in Northeast Brazil. Regarding the state of LCA in Brazil, most of the
studies have been undertaken in the South and Southeast regions—therefore the
application to the Northeast region could help disseminate good practice. The
energy supply system is optimized through the solution of an optimization model
based on Mixed Integer Linear Programming (MILP). The optimization encom-
passes the configuration of the system simultaneously with the operational strategy,
providing an energy supply system with minimum environmental impacts. These
environmental impacts are associated with the production of each piece of equip-
ment installed plus the consumption of energy resources (natural gas, diesel,
biomass, etc.) to satisfy the energy demands of the consumer center.
Polygeneration System
The study case is a university hospital, with 420 beds, located in the city of Jo~ao Pessoa (Northeast Brazil). The energy demands considered were electricity (light-
ing and equipment), hot water (internal consumption of the hospital), steam (laun-
dry and sterilization) and coolth (a/c for comfort). Hospitals are good study cases
for optimization because they present regular, stable energy demands. The study
considered an entire operational year, subdivided into two representative days per
month (weekday and holiday/weekend), with 24 hourly periods each.
Real electricity data was provided by the hospital. Coolth, hot water and steam
demands were disaggregated through the utilization of climate data, degree-days
method, occupation and energy audit data (Erbs et al. 1983; Climaticus 4.2, 2005;
Nepote et al. 2009; Araújo 2004). The hospital presents the following annual energy
demands: 2791 MWh of electricity, 1947 MWh of hot water, 138 MWh of steam,
and 2309 MWh of coolth. Table 23.1 shows the energy demands for the hospital,
throughout the year.
296 M. Carvalho et al.
One of the major steps in Mixed Integer Programming is the definition of a
superstructure that represents all options available for equipment and energy
resources. Figure 23.1 depicts the superstructure of the energy supply system for
the hospital located in Jo~ao Pessoa, following the scheme of Carvalho and Millar (2012).
The available utilities were electricity (EE), diesel (DI), biomass (BM), Natural
gas (NG), steam (VA, 180 �C), hot water (HW, 90 �C), cooling water (CW, t0þ 5 �C), ambient air (t0�C), and chilled water (CO, 5 �C). A positive node denotes supply/production of energy and a negative node denotes consumption. The hori-
zontal lines represent the energy forms considered at the site, into which the
equipment (vertical lines) are connected to consume or produce energy.
Table 23.1 Energy demands of the hospital
Month representative day
nd (days/year)
Electricity Hot Water Steam Coolth
Total
MWh/day
Total
MWh/day
Total
MWh/day
Total
MWh/day
Jan wa 20 8538 3543 0.465 5961
Jan hb 11 6315 3543 0.233 4360
Feb w 19 9696 6436 0.465 6472
Feb h 9 6247 6436 0.233 4290
Mar w 20 9861 6436 0.465 8013
Mar h 11 7474 6436 0.233 5443
Apr w 20 9949 6436 0.465 7071
Apr h 10 7348 6436 0.233 4737
May w 20 8901 6436 0.465 7895
May h 11 6383 6436 0.233 5534
Jun w 19 7489 5032 0.465 7768
Jun h 11 6832 5032 0.233 5259
Jul w 20 6568 3881 0.465 5186
Jul h 11 6045 3881 0.233 3760
Aug w 20 5954 3881 0.465 7343
Aug h 11 4681 3881 0.233 4941
Sep w 21 6686 3881 0.465 7483
Sep h 9 4755 3881 0.233 5046
Oct w 20 8041 5284 0.465 8834
Oct h 11 5969 5284 0.233 6057
Nov w 20 9309 6436 0.465 8260
Nov h 10 6022 6436 0.233 5627
Dec w 20 1036 6436 0.465 5912
Dec h 11 7389 6436 0.233 3879
Σ MWh/year MWh/year MWh/year MWh/year Year 365 2791 1947 138 2309 aw¼weekday bh¼ holiday/weekend
23 Life Cycle Analysis as a Decision Criterion for the Implementation of Solar. . . 297
Table 23.2 shows the technical and economic characteristics of the equipment
that belong to the superstructure (Fig. 23.1). The rows indicate the technologies
available, and the columns indicate the energy resources. The coefficient in bold
indicates the flow that defines the productive capacity of the equipment, and
positive and negative coefficients, indicate, respectively, that an energy flow is
either produced or consumed. At the time of writing, 1 US$¼ 2.50 R$. The PV system is constituted by PV panels and inverters (electricity storage will
not be considered). Information was obtained from consultation to PV panel
(Kyocera 2014) and inverter (Santermo 2014) manufacturers. The cost of the
system was US$ 880/panel (including the cost for the panel, inverter, installation
materials, transportation and assembly). The area of each panel is 1.64 m2. The
maintenance costs are US$ 10/m2 per year. As the geographic latitude of the
municipality of Jo~ao Pessoa is 07�S, the inclination angle of the panels to be installed in the hospital must be 10�. Historic hourly radiation data (W/m2) were available from the CLIMATICUS database (2005).
Electricity was charged with an hour-seasonal tariff, presenting differentiated
tariffs for peak and off-peak periods: US$51.60/MWh for off-peak periods, and
between 18 h and 21 h the peak value was US$79.60/MWh. Steam demand was
considered constant during the period in which the sterilization central was open,
during 6 h and 20 h, in addition to the steam demand of a hot counter in the
restaurant, during lunch and supper times. The hot water demand presents two
contributions: laundry (operating between 8 h and 18 h), and the internal use of the
hospital (no interruptions). The tariff for natural gas (US$48/MWh—PBGAS 2013)
does not include hourly or seasonal differentiation, as is the case of diesel (US
$59.60/MWh). Due to the location of Jo~ao Pessoa, the biomass considered herein originates from sugar cane bagasse, and the final price was U$ 13.20/MWh (con-
sidering 15.40 MJ/kg dry matter and 0.787 dry matter/kg).
A lifetime of 15 years was considered for the system, with an interest rate of
10% y�1, obtaining a capital recovery factor of 0.13 yy�1. The system was
Electricity
Diesel
Biomass
Steam
Hot water, 90°C Cooling water, ambient + 5°C
Chilled water, 5°C
Ambient air
El ec
tri c g
rid im
po rt
+
Di es
el im
po rt
+
Bi om
as s i
m po
rt
+
-
Ga s
en gin
e
+
+
+
-
DI e
ng ine
+
+
VA b
oil er
+
HW b
oil er
-
+
BM b
oil er
+
-
EE b
oil er
+
-
DI b
oil er
+
1X A
bs C
hil ler
+
-
+
M ec
h Ch
ille r
+
-
+
Co oli
ng to
we r
-
-
+
VA /H
W H
X
+
-
HW /C
W H
X
+
-
Hospital demand
-
-
-
-
+
+
BM b
oil er
-
+
-
- Natural gas
Na tu
ra l g
as im
po rt
+
2X A
bs C
hil ler
+
+
-
- -
PV p
an els
+
El ec
tri c g
rid e
xp or
t
+-
Fig. 23.1 Superstructure illustrating all potential conversion pathways considered
298 M. Carvalho et al.
T a b le
2 3 .2
M at ri x o f te ch n ic al
p ro d u ct io n co ef fi ci en ts an d te ch n o lo g y d at a (C ar v al h o et
al . 2 0 1 4 )
T ec h n ic al
p ro d u ct io n co ef fi ci en ts
E q u ip m en t
N G
B M
D I
V A
H W
C W
A A
C O
E E
C o st
C IN
V
(1 0 3 U S $ )
C o st
O & M
(U S $ /M
W h )
N o m .
P o w er
P N O M
(M W )
G as
en g in e
�2 .6 3
1 .1 0
0 .4 5
1 1 8 5 .0 0
6 .0 0
0 .4 1
D ie se l en g in e
�2 .6 6
0 .8 0
0 .5 0
1 9 0 .8 0
6 .0 0
0 .3 6
S te am
b o il (B M )
�1 .4 0
1 2 0 .4 0
3 .2 0
0 .2 5
S te am
b o il (N
G )
�1 .1 8
1 2 1 .2 9
0 .8 9
0 .3 0
S te am
b o il (E E )
1 �1
.1 5
0 .4 0
0 .8 9
0 .1 5
H X
(V A -H
W )
�1 .1 0
1 3 .5 6
0 .8 9
0 .4 0
H o t w at er
b o il (B M )
�1 .2 5
1 2 5 .0 0
3 .2 0
0 .1 7
H o t w at er
b o il (N
G )
�1 .2 2
1 1 9 .7 2
0 .8 9
0 .3 0
H o t w at er
b o il (E E )
1 �1
.1 1
1 1 .2 8
0 .8 9
0 .1 5
H X
(H W -C W )
�1 .1 0
1 2 .9 6
0 .8 9
0 .4 0
A b s ch il (2 x )
�0 .7 7
1 .7 7
1 �0
.0 1
1 8 6 .0 8
4 .0 0
0 .4 6
A b s ch il (1 x )
�1 .3 2
2 .3 2
1 �0
.0 1
2 1 5 .8 8
4 .0 0
0 .4 9
M ec h an ic al
ch il le r
1 .2 1
1 �0
.2 1
5 8 .0 0
1 .7 7
0 .2 8
C o o li n g T o w er
�1 .0 0
1 �0
.0 2
1 1 .2 8
4 .0 0
1 .0 0
23 Life Cycle Analysis as a Decision Criterion for the Implementation of Solar. . . 299
designed to interact with the electric grid also through the export of autogenerated
electricity, considering the credit compensation scheme set out by BRASIL (2012).
In this energy compensation system, surplus generated electricity can be fed into
the distribution grid and registered as energy credits, which can be consumed in up
to 36 months. This special regime for electricity exports applies to photovoltaic-
and natural gas-produced electricity. Finally, the problem to be solved consists of
two simultaneous tasks: selection of the combination of technologies (type and
power installed) that are capable of meeting the energy demands of the hospital, and
establishment of the operation mode for all equipment installed, for each time
interval defined.
Life Cycle Analysis
It takes considerable effort to conduct an LCA study, exploring large industrial
systems, collecting and analyzing a great amount of environmental information
(Baumann and Tillmann 2004). A brief overview of the basic LCA process is
provided for context when interpreting the findings. A framework for LCA has
been standardized by the International Organization for Standardization (ISO) in
the ISO 14040 series (ISO 14040 2006; ISO 14044 2006). This LCA framework
consists of the following elements (Carvalho et al. 2011): (1) Goal and Scope
definition, which specifies the goal and intended use of the LCA and delineates
the assessment (system boundaries, function and flow, required data quality, tech-
nology and assessment parameters); (2) Life Cycle Inventory analysis (LCI), which
includes the collection of data on inputs and outputs for all processes in the product
system; (3) Life Cycle Impact Assessment (LCIA), which translates inventory data
on inputs and outputs into indicators about the product system’s potential impacts on the environment, human health, and availability of natural resources; and
(4) Interpretation, the phase where the results of the LCI and LCIA are interpreted
according to the goal of the study and where sensitivity and uncertainty analysis are
performed to qualify the results and conclusions.
Because of the potential impacts of global warming and its associated climate
change, greenhouse gases (GHG) were chosen to represent the environmental loads.
The more general category name climate change replaced the formerly used
greenhouse effect and global warming (Udo de Haes 2002). Because the average
tropospheric lifetime of all greenhouse gases, even of the relatively short-lived ones
(CH4, about 10 years), exceeds the tropospheric mixing time (about 1 year), it is not
important where the emissions occur. Climate change is therefore a truly global
impact category (Udo de Haes 2002).
Although the geographic scale of GHG emissions is global, special care must be
taken at the time of defining the LCA processes and data utilized, as the results will
vary greatly if, for example, different production methods and transportation are
used. This will result in a great difference in environmental loads if natural gas is
consumed in Spain (originating from Algeria, liquefied, transported in Liquefied
300 M. Carvalho et al.
Natural Gas carriers, and regasified before being distributed via pipelines) or
Canada (originating from the province of Alberta, transported and distributed in
pipelines).
The impact evaluation method chosen to represent the environmental loads was
the 2013 version of IPCC, which expresses environmental impacts in kg CO2-eq
after atmospheric emissions are quantified and multiplied by a conversion factor
(IPCC 2014). The reader is directed to IPCC (2014) for a more complete description
of the method. Software SimaPro v. 8.0.4 (PréConsultants 2015) was utilized for
the quantification of environmental impacts, and the database utilized was
EcoInvent version 3 (EcoInvent 2014).
Equipment
For each item present in the superstructure (Fig. 23.1), the environmental emissions
were calculated as the sum of the partial emissions for each stage (construction,
operation and maintenance, and dismantlement and disposal). Data on the material
composition of each piece of equipment were obtained after exhaustive and exten-
sive consultation of catalogues and manufacturers. Table 23.3 shows the main
material composition and CO2-eq emissions associated (COE).
The best available disposal scenario was considered for each material
(recycling), and all waste flows (lubricating oil, wastewater, Li-Br, etc.) received
adequate treatment before disposal. The exception was the gas engine, which in its
specific case considered reuse of materials by the manufacturer, resulting in the
impressive low emissions shown in Table 23.3. All recycling options also consid-
ered transportation to the recycling site, which significantly contributed to the final
emissions, as a distance of 2200 km was considered (the recycling site is located in
S~ao Paulo, Southeast Brazil).
Energy Utilities
Special care was taken to correctly adapt each existing process that would be
applicable to the optimization study herein presented. For the electricity mix, a
2014 average was considered (ONS 2014) for the state of Paraı́ba: hydro 48.04%,
thermoelectrical (oil) 44.58%, and eolic 7.38%. Considering these percentages, the
final emissions associated with the consumption of 1 kWh from the electric grid
were 0.580 kg CO2-eq. This figure is very different from the overall Brazilian
electricity mix, which presents a much lower carbon content.
For the sugar cane bagasse, the emissions were 0.147 kg CO2-eq/kWh. These
emissions already take into account the drying of the bagasse. For natural gas, the
emissions were 0.256 kg CO2-eq/kWh consumed, and for diesel, 0.319 kg CO2-eq/
kWh consumed. Please note that these emissions refer to the consumption of one
23 Life Cycle Analysis as a Decision Criterion for the Implementation of Solar. . . 301
energy unit of the utility; however, the optimization model will consider adequate
conversion (Table 23.2) to different energy forms. For example, the diesel gener-
ator will produce electricity at 0.848 kg CO2-eq/kWh, considering its electrical
efficiency (1/2.66¼ 37.6%). The system boundaries were defined as in Fig. 23.2, where the selfgenerated
electricity exported to the electric grid is evaluated at the same “environmental
impact” as the electricity imported from the grid, introducing the concept of
avoided emissions as the emissions avoided elsewhere by the production of elec-
tricity by the PV panels (avoiding the purchase of electricity from the grid).
Table 23.3 Main material composition of technologies and corresponding environmental emissions
Main material composition
COE
kg
CO2-eq
Gas engine Cast iron 1300 kg, Oil 540 kg, Low-alloyed steel 225 kg, PVC 5 kg,
Steel sheet 2 m2 3.53 102
Diesel engine Cast iron 3500 kg, Oil 1292 kg, Low-alloyed steel 300 kg, Rubber
50 kg, Copper 105 kg
6.98 106
Steam boil
(BM)
Chromium steel 1980 kg, Copper 50 kg, PVC 10 kg 2.73 103
Steam boil
(NG)
Rock wool 115 kg, Al sheet 14 m2, Stainless steel 980 kg,
low-alloyed steel 490 kg
2.23 106
Steam boil
(EE)
Rock wool 115 kg, Al sheet 14 m2, Stainless steel 980 kg,
low-alloyed steel 490 kg
2.23 106
HX (VA-HW) Fe-Ni-Cr alloy 94 kg, Epoxy resin 0.5 kg, Titanium dioxide 3 kg 1.50 103
Hot water boil
(BM)
Chromium steel 1980 kg, Copper 50 kg, PVC 10 kg 2.73 103
Hot water boil
(NG)
Rock wool 115 kg, Al sheet 14 m2, Stainless steel 980 kg,
low-alloyed steel 490 kg
2.23 106
Hot water boil
(EE)
Rock wool 115 kg, Al sheet 14 m2, Stainless steel 980 kg,
low-alloyed steel 490 kg
2.23 106
HX (HW-CW) Titanium dioxide 2 kg, Fe-Ni-Cr alloy 75 kg, Epoxy resin 0.5 kg 1.47 103
Absorption chil
(2x)
Li-Br 1600 kg, Stainless steel 7338 kg, Copper 30 kg, PVC 10 kg 2.47 105
Absorption chil
(1x)
Li-Br 2200 kg, Stainless steel 7418 kg, Copper 30 kg, PVC 10 kg 3.25 105
Mechanical
chiller
Polyurethane 30 kg, Stainless steel 2000 kg, Copper 30 kg, PVC
10 kg
1.39 104
Cooling Tower Glass fiber 2622 kg, Cast iron 200 kg, Copper 10 kg, PVC 10 kg,
Steel sheet 1 m2 9.71 103
PV panel PV panel 1.64 m2, Inverter 1, Copper 1.5 kg, PVC 0.125 kg, Steel
sheet 0.005 m2 7.80 103
302 M. Carvalho et al.
Optimization Model
A combinatorial optimization method, based on mathematical programming
(MILP), determines the optimal design and operation for the energy supply system.
The optimization model was implemented in LINGO 14.0 (2015), an optimization
tool that utilizes the combination of branch and bound and simplex methods in its
solution algorithm. The environmental objective function was the minimization of
the total annual impact (COtot):
Min COtot ¼ COfix þ COope ð23:1Þ
Where COfix referred to the impact associated with the installation of equipment,
and COope referred to the consumption of energy utilities to satisfy the energy
demands of the hospital. Then:
COfix ¼ fame Σi NEI ið Þ COE ið Þ þ PV½ � ð23:2Þ
where NEI(i) and COE(i) are, respectively, number of pieces of equipment installed
for technology i and the CO2 emissions for the production of each piece of
equipment. PV refers to the PV panels. The environmental amortization factor
fame allocates the global emissions throughout the lifetime of the system, and
was 0.10 y�1. Considering that the year was divided into d representative days, which were in
turn subdivided into h hours, (d,h) represented the hth hour of the dth representative day. The annual operation impact (COope), associated with the operation of the
system was expressed by:
Market
Electricity imports
Electricity exports
Diesel, biomass, natural gas
Polygeneration System
Energy demands
Electricity
Heat
Cooth
System boundaries
Steam
Fig. 23.2 Boundaries of the polygeneration system
23 Life Cycle Analysis as a Decision Criterion for the Implementation of Solar. . . 303
COope ¼ ΣdΣh COng Fng d; hð Þ þ COee Ep d; hð Þ � COee Es d; hð Þþ CObm Fbm d; hð Þ þ COdi Fdi d; hð Þ � �
ð23:3Þ
where CO refers to the emissions associated with the consumption of the different
utilities: ng (natural gas), ee (electricity), bm (biomass), and di (diesel). F refers to
the amount imported for each fuel, Ep refers to electricity imported from the grid
and Es refers to electricity exported to the grid (and therefore counted as avoided
emissions). Equations (23.1)–(23.3) can be changed to consider economic costs.
Capacity limits, production restrictions, and balance equations were enforced in the
optimization model.
Capacity limits: For each period (d,h) and for each technology i
POEði, d, hÞ � NEIðiÞ ∙PnomðiÞ ð23:4Þ
where POE(i,d,h) is the energy production of technology i in the period (d,h), and
Pnom is the nominal power of the equipment.
Production restrictions: For each period (d,h) and for cogeneration modules, the
production of energy was restricted to:
POE i; d; hð Þ ¼ NES i; d; hð Þ Pnom ið Þ withNOP i; d; hð Þ 2 0, 1, . . . , NEI ið Þf g ð23:5Þ
where NES(i,d,h) is the number of operational equipment of technology i in the
period (d,h). For each technology i, For each utility j,
UI i; j; d; hð Þ ¼ PC i; jð Þ POE i; d; hð Þ ð23:6Þ
where UI(i,j,d,h) is the energy flow of utility j interchanged with technology i in the
period (d,h) and PC(i,j) is the absolute value of the production coefficient
(Table 23.2).
Balance equations: For each period (d,h) and for each utility j:
Prod j; d; hð Þ � Cons j; d; hð Þ þ Imp j; d; hð Þ � Exp j; d; hð Þ� Waste j; d; hð Þ � Demand j; d; hð Þ ¼ 0 ð23:7Þ
Prodðj, d, hÞ ¼ ΣiXði, j, d, hÞ ∙YTUPði, jÞ withYTUPði, jÞ2f0, 1g ð23:8Þ Cons j; d; hð Þ ¼ ΣiX i; j; d; hð Þ YTUC i; jð Þ withYTUC i; jð Þ2 0; 1f g ð23:9Þ
Imp j; d; hð Þ � YUP jð Þ Cons j; d; hð Þ þ D j; d; hð Þð Þ withYUI jð Þ2 0; 1f g ð23:10Þ Exp j; d; hð Þ � YUS jð Þ Prod j; d; hð Þ with YUE jð Þ2 0; 1f g ð23:11Þ
Waste j; d; hð Þ � YUW jð Þ Prod j; d; hð Þ with YUW jð Þ2 0; 1f g ð23:12Þ
304 M. Carvalho et al.
Demand j; d; hð Þ � YUD jð Þ Prod j; d; hð Þ þ P j; d; hð Þð ÞwithYUD jð Þ 2 0; 1f g ð23:13Þ
YTUP(i,j) was 1 when technology i produced utility j. YTUC(i,j) was 1 when
technology i consumed utility j. Production (Prod), and Consumption (Cons)
corresponded to internal utility flows. Imports(Imp), Exports (Exp), Waste and
Demand correspond to the utility flows interchanged between the energy system
and the market environment. Binary variables YUI(j), YUE(j), YUW(j) and YUD
(j) indicated, respectively, the possibility of such interchanges.
Results and Discussion
The main criterion chosen to carry out the optimization of the energy supply system
was the total annual emissions (kg CO2-eq/year). Table 23.4 presents the results for
the optimizations carried out, considering that there are 200 PV panels available for
installation.
Table 23.4 presents three optimal solutions: economic and environmental opti-
mals, and a reference solution. The reference solution reflects the conventional way
of installing energy supply systems: restrictions were introduced within the opti-
mization model to prevent PV panels and biomass-driven equipment to be installed,
while also excluding the possibility of installing cogeneration modules and absorp-
tion chillers.
The reference solution installed hot water and steam boilers that operated on
natural gas, as well as one electrical boiler. All the electricity necessary to supply
the hospital was purchased directly from the grid. The cooling demand was met by
mechanical chillers. This solution presented the worst environmental emissions,
almost 40% higher than those of the environmental optimal.
When optimizing the system applying the economic criteria, the system took
advantage of the lower purchase cost of biomass and imported 2663 MWh/year for
this energy source to operate boilers. For the economic optimal, steam-hot water
heat exchangers, and exclusively mechanical chillers were installed. Electricity was
used to drive the mechanical chillers and auxiliary machinery in this system.
A very different configuration was obtained for the environmental optimal
(Fig. 23.3): a natural gas engine with heat recovery was installed for the production
of electricity. In Fig. 23.3, the installed equipment is shown in bold, while available
but not installed equipment are shown in gray. Only biomass boilers were installed
along with both types of heat exchangers (steam-hot water and hot water-
refrigeration water). Electricity was supplied to users by operating the gas engine
cogeneration module, by the production of the PV panels, and by purchasing a
small quantity from an outside electric power company. The environmental optimal
suggested that environmental benefits are realized through electricity exports.
Trigeneration was installed in this case, as the cold water for space cooling was
23 Life Cycle Analysis as a Decision Criterion for the Implementation of Solar. . . 305
Table 23.4 Minimum annual cost for the polygeneration system with 200 PV panels installed
Economic Optimal Reference systema CO2-eq optimal
Composition of system
Number (Installed
Power)
Number (Installed
Power)
Number (Installed
Power)
Gas engine 0 (0 MW) – (0 MW) 1 (0.41 MW)
Diesel engine 0 (0 MW) – (0 MW) 0 (0 MW)
Steam boiler (NG) 0 (0 MW) 1 (0.300 MW) 0 (0 MW)
Steam boiler (BM) 1 (0.250 MW) 0 (0 MW) 1 (0.25 MW)
Steam boiler (EE) 0 (0 MW) 0 (0 MW) 0 (0 MW)
Heat exchanger
(VA-HW)
1 (0.400 MW) 1 (0.400 MW) 1 (0.40 MW)
Hot water boiler (NG) 0 (0 MW) 1 (0.300 MW) 0 (0 MW)
Hot water boiler (BM) 2 (0.340 MW) 0 (0 MW) 1 (0.17 MW)
Hot water boiler (EE) 1 (0.150 MW) 1 (0.150 MW) 0 (0 MW)
Heat exchanger
(HW-CW)
0 (0 MW) 0 (0 MW) 1 (0.40 MW)
Double-effect absorp-
tion chiller
0 (0 MW) 0 (0 MW) 0 (0 MW)
Single-effect absorp-
tion chiller
0 (0 MW) 0 (0 MW) 1 (0.49 MW)
Mechanical chiller 3 (0.810 MW) 3 (0.810 MW) 3 (0.81 MW)
Cooling tower 1 (1.000 MW) 1 (1.000 MW) 2 (2.00 MW)
Photovoltaic panels 200 units – 200 units
Electricity imports 3244 MWh/year 4281 MWh/year 297 MWh/year
Electricity produced by
PV panels
129 MWh/year – 129 MWh/year
Electricity credits – – 760 MWh/year
Natural gas imports – 1528 MWh/year 9554 MWh/year
Diesel imports – – –
Biomass imports 2663 MWh/year – 281 MWh/year
Initial investment in
equipment
US$ 587,089 US$ 374,670 US$ 1,022,892
Annual cost of elec-
tricity imports
US$/
year
180,489 US$/
year
233,979 US$/
year
15,342
Annual credit with
electricity exports
US$/
year
– US$/
year
– US$/
year
43,488
Annual cost of natural
gas imports
US$/
year
– US$/
year
73,335 US$/
year
458,576
Annual cost of diesel
imports
US$/
year
– US$/
year
– US$/
year
–
Annual cost of biomass
imports
US$/
year
35,150 US$/
year
– US$/
year
3708
Operation and Mainte-
nance costs
US$/
year
21,813 US$/
year
16,716 US$/
year
53,519
Annual cost of
equipmentb US$/
year
76,322 US$/
year
48,707 US$/
year
132,976
TOTAL annual cost US$/
year
331,774 US$/
year
372,758 US$/
year
620,633
(continued)
306 M. Carvalho et al.
supplied by the single effect absorption chiller and mechanical chillers. Surplus
not-consumed cogenerated heat was disposed of through heat exchangers. This
result was not totally unexpected as trigeneration systems have long been seen as
good alternatives to reduce emissions; however, the potential to reduce emissions
depends also on the electricity mix supplied to the system.
Distributed energy resource systems have been recognized as an
environmentally-friendly in comparison with conventional energy systems, as
mentioned by Ren et al. (2010); these systems can employ combined heat and
power systems, PV systems, etc. and help address global environmental problems.
Saner et al. (2014) optimized the energy supply for a Swiss building considering
greenhouse gas emissions and particulate matter formation, with a drastic shift from
fossil fuel-dominated system to a biomass-dominated system. You (2012) and
Carvalho et al. (2011) have obtained divergent solutions when optimizing from
economic and environmental perspectives, corroborating the results obtained
herein.
Table 23.4 (continued)
Economic Optimal Reference systema CO2-eq optimal
Composition of system
Number (Installed
Power)
Number (Installed
Power)
Number (Installed
Power)
CO2 emissions for
equipment only
kg CO2-
eq/year
3,851,100 kg CO2-
eq/year
2,291,100 kg CO2-
eq/year
1,954,903
CO2-eq emissions for
electricity imports
kg CO2-
eq/year
1,881,711 kg CO2-
eq/year
2,482,917 kg CO2-
eq/year
172,222
CO2-eq emissions for
electricity exports
kg CO2-
eq/year
– kg CO2-
eq/year
– kg CO2-
eq/year
441,039
CO2-eq emissions for
natural gas imports
kg CO2-
eq/year
– kg CO2-
eq/year
391,230 kg CO2-
eq/year
2,445,736
CO2-eq emissions for
diesel imports
kg CO2-
eq/year
– kg CO2-
eq/year
– kg CO2-
eq/year
–
CO2-eq emissions for
biomass imports
kg CO2-
eq/year
391,448 kg CO2-
eq/year
– kg CO2-
eq/year
41,296
CO2-eq emissions for
equipmentb kg CO2-
eq/year
385,110 kg CO2-
eq/year
674,291 kg CO2-
eq/year
195,490
TOTAL annual CO2-eq
emissions
kg CO2-
eq/year
2,658,269 kg CO2-
eq/year
3,548,438 kg CO2-
eq/year
2,557,232
aCarvalho et al. (2014) bLifetime of system 15 years, interest rate 10%/year
23 Life Cycle Analysis as a Decision Criterion for the Implementation of Solar. . . 307
Conclusions
A progressive change has been observed in recent years: consumers, and society in
general, are starting to evolve towards a more environmentally-friendly conscience.
This conscience, along with restrictions on the emissions of environmental impacts,
have in turn changed how optimal solutions are obtained. Initially optimal solutions
were based exclusively on economic aspects. Nowadays, environmental aspects are
beginning to be introduced in optimizations, either as a main objective or as part of
the objective (which could include energy efficiency or economic terms).
This manuscript explained the incorporation of environmental information in an
optimization model for the energy supply of a hospital located in Northeast Brazil.
The Life Cycle Assessment methodology was applied for the quantification of
environmental loads, expressed by the emissions of CO2-eq (IPCC methodology).
Environmental data was introduced into the linear programming model, which
determined the equipment to be installed and how to operate each technology, in
order to satisfy the energy demands of the hospital. The optimal solution also
provided all energy, economic, and environmental flows.
The environmental optimal solution suggested that trigeneration is the best
option to minimize the environmental loads produced by the energy supply system.
Natural gas was imported from the grid to drive the gas engine, which produced hot
water and electricity to meet the energy requirements of the hospital. PV panels
produced electricity, and biomass was imported for hot water and steam boilers. A
single-effect absorption chiller utilized part of the cogenerated heat to produce
coolth. Mechanical chillers helped with the production of coolth also. This optimal
solution took advantage of the electricity exports to achieve higher rates of avoided
emissions, and realize environmental benefits to lower the overall emissions of the
system.
+
+
+
-
+
+
+
-
+
+
+
-
+ +
-
+
-
+
+
-
+
+
-
+
-
-
+
+
-
+
-
-
-
-
-
+
-
+
-
-+
+
+
-
- -+ 297 129 3592 2791
138
1947
2309
281
9554 9554
3951
1616
86
69
195
139
8 333 125
1047
1841
793
1849
1516
1
1 1027
6239 933
6239
+ 760
- Electricity
Diesel
Biomass
Steam
Hot water, 90°C Cooling water, ambient + 5°C
Ambient air
Natural gas
El ec
tri c g
rid im
po rt
Di es
el im
po rt
Bi om
as s i
m po
rt
Ga s
en gin
e
DI e
ng ine
VA b
oil er
HW b
oil er
BM b
oil er
EE b
oil er
DI b
oil er
1X A
bs C
hil ler
M ec
h Ch
ille r
Co oli
ng to
we r
VA /H
W H
X
HW /C
W H
X
BM b
oil er
Na tu
ra l g
as im
po rt
2X A
bs C
hil ler
PV p
an els
El ec
tri c g
rid e
xp or
t
Hospital demand
Fig. 23.3 Optimal environmental system annual flows (MWh/year)
308 M. Carvalho et al.
The optimization carried out herein was based on the emission on greenhouse
gases (IPCC 2014). Future works could include the consideration of a different,
perhaps more global, impact assessment method for the calculation of environmen-
tal impacts. This would likely provide a different result and help verify the effect of
utilizing a more wider perspective in the optimization. Also, sensitivity analyses
could verify whether the configuration varies when different electricity mixes are
applied (different regions present different mixes). The high emissions associated
with the purchase of electricity could have a considerable effect on the configura-
tion of the system, as the municipality of Jo~ao Pessoa counts with the largest thermal plant in the world (oil-based engines).
Acknowledgments The authors wish to acknowledge the support of the National Council for Scientific and Technological Development (CNPq), through project n� 475879/2013-9.
References
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310 M. Carvalho et al.
Part VI
Energy Technologies and Their Effect on Global Warming
Green Buildings Technology
Available technologies and numerical investigation tools for buildings performance
optimization
Chapter 24
Energy Conservation Through Sunrays Reflecting Coating on Buildings
Imre Benk€o
Introduction
Sun reflecting coating materials are used in ambient temperature applications
(under 80 �C) such as walls, roofs, heat shields, etc. where thermal radiation is a dominant mechanism of heat transfer. Thus there is a real need for data concerning
the radiative properties of such materials.
The determination of the emissivity of coating materials is not straightforward
mater. Severe practical difficulties arise in connection with the measurement of test
specimen surface temperature using thermocouples embedded just below the sur-
face. It is extremely difficult to achieve uniformity of temperature over the surface
of a coated specimen operating at sunshine and it is probably for this reason that the
calorimetric method of emissivity measurement has not found favor in the case of
such materials and attention has instead been concentrated on radiometric tech-
niques as IR-imagery, too. But in the case of practical approach, the use of
IR-imagery gives a direct temperature difference between the coated and uncoated
surfaces resulting a lower emissivity of the coating.
Method of Examination
The measuring method consists of two successive steps. In the first step IR-imaging
equipment, which viewed the speciment at right angle to the surface of the sample,
received both the radiation emitted by the speciment and the sun radiation reflected
I. Benk€o (*) Faculty of Mechanical Engineering, Budapest University of Technology and Economics,
H-1112 Budapest, Cirmos u.1., Hungary
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_24
315
from it. In the second step, after getting to the thermal steady state, shielded the
sample from the sunshine, the IR-imaging equipment received only the radiation
emitted by the nonuniform heated coated and uncoated sides of the specimen (that
is the ‘own radiation’). The special feature of the arrangement used in this case was a heat shield
mounted on rotating arm. The shield consisted of a plate backed by insulating
material. The shield was designed to fit over the surface of the specimen without
touching it, held in position by a spring.
The arrangement was designed so that when the specimen reached thermal
equilibrium on the sunshine, the shield could then be quickly swung on the rotating
arm, thus shielding the specimen from the sunshine and allowing only the own
radiant an convective heat transfer to take place. Measurement was terminated after
about 4–6 s (Figs. 24.1 and 24.2).
In the case of each measurements it was possible to vary the angle of view of the
measuring equipment with respect to the normal to the surface of the speciment (see
Fig. 24.3). A well defined distribution of emissivity as a function of the quality of
Radio waves
Infrared raysSunlight
X-rays
Gamma rays
Ultra- violet waves
1 m
750 nm
380 nm
750
chloro. A absorbs 450-670 (A) chloro. B absorbs 450-650 (B)
400-550 carotenoids absorbs
chlorophyl reflects: 500
Chlorophyl
chlorophyl B (P680)
A (P700)
400
700
650
600
550
500
450
400 380
1 nm
Wavelength
Fig. 24.1 Visible light and electromagnetic spectrum of pigments and absorption spectra
316 I. Benk€o
the specimen has been also presented for the coated and uncoated surfaces (see
Figs. 24.5 and 24.6). The average value of the emissivity for these surfaces can be
calculated by histographical method.
Theoretical Basis of the Direct Comparative Method
The IR-radiation of different samples was examined under practical conditions, in
direct sunshine. The half of the each sample was coated by selective coating and the
other half was uncoated (Fig. 24.4). Infrared radiation emitted by the surfaces was
measured by AGEMA thermal imaging equipment with a special method.
As indicated before, the arrangement for the ‘direct’ method of emissivity measurement consists of a relatively small heated specimen having a surface
temperature Tw within a large environment which is at uniform temperature Te .
The specimen is assumed to be opaque to thermal radiation.
The sunshine radiation views a given target area on the specimen surface in the
normal direction or at some angle θ to the normal. In the second step of the examination, the solar radiation absorbed by the specimen is transferred to the
environment by emission and convective heat transfer.
Thus
q s θð Þ :ε θ;Tð Þ ¼ ε θ;Tð Þ:σ: Tw4 � Tc4 � �þ 2:α Tð Þ: Tw � Tcð Þ ð24:1Þ
Fig. 24.2 Spectral values of the reflectivity of AL-CHR coating
24 Energy Conservation Through Sunrays Reflecting Coating on Buildings 317
Here σ is the Stefan-Boltzmann constant, α is the coefficient of heat transfer in the heated specimen surface and q•s(θ) intensity of direct sunshine radiation in direction θ.
From Eq. (24.1) it follows that
Fig. 24.3 Experimental arrangement for steady state and shielded measurements of emissivity
Fig. 24.4 A sample (Pace_04) of a slate roof
318 I. Benk€o
ε θ;Tð Þ: ¼ 2:α Tð Þ: Tw � Tcð Þ= q s θð Þ þ σ: Tc4 � Tw4 � � � ð24:2Þ
Noting that according to Kirchhoff’s Low applied to total values of absorbtivity a (θ,T) and emissivity
a θ;Tð Þ ¼ ε θ;Tð Þ ð24:3Þ
Comparison of Surfaces with Different Emissivities
The surface emissivity of the coating was compared with that of specimen material.
In Figs. 24.5 and 24.6 on the thermogram are two quadrangles marked for which
temperature distribution was computed. The temperature difference between the
area coated with SRC-coating and the uncoated surface shows that the SRC-coating
directly decreases the IR-emissivity of the material. Numerical values for the
temperature represent the so called’ effective black body temperature (at thermal imaging equipment’s ε¼ 1).
Equation between temperature and emissivity ratios comes from the next
equality
σ:T14:ε1 ¼ σ: T24:ε2 ð24:4Þ
Fig. 24.5 IV-thermogram of a sample of Fig. 24.4 on direct sunshine
24 Energy Conservation Through Sunrays Reflecting Coating on Buildings 319
So from Eq. (24.4), it follows that
ε1=ε2 ¼ T2=T1ð Þ4: ð24:5Þ
Presentation of Results
The results are presented in the form of:
(a) A plot of spectral reflectivity of SRC-coating as a function of wavelength of
the radiation (Fig. 24.2).
(b) IR-thermograms (Figs. 24.5 and 24.6) and table (Tables 24.1 and 24.2) of
sample for presenting the thermal effects of different material/coating couples.
(c) Four plots of equilibrium temperature and intensity of ‘heat gain’ of different wall structures versus emissivity of surfaces, intensity of direct sunshine,
coefficient of heat transfer and environmental temperature (Figs. 24.7, 24.8,
24.9, and 24.10).
Fig. 24.6 IV-thermogram of a sample of Fig. 24.4 shielded from sunshine
320 I. Benk€o
Table 24.1 Technical data of AL-CHR (ALUMA-
CHRON) elastomeric roof/
wall coating
Wet material
Metallic aluminium: 6%
Pigments: 2%
Nonvolatile liquid elastomer: 23%
Dry to complete: 3 days
Solids by volume: 48%
Flashpoint of solvent: 40 �C Application temperature: 5–49 �C Wet film thickness: 1 L/sq m, 1 mm
Cured coating
Elongation at 25 �C: 400% Elongation at 0 �C:200% Return after elongation: >95%
U.V. reflection, white: 90%
Light gray: 70%
Colors: <40%
U.V. resistance: excellent
I.R. emissivity:
At low temperature, 2 6 μm: 0.5 0.7 I.R. reflectance:
At sunshine: 0.4 2.4 μm: 0.45 0.48 Dry film thickness: 1 L/sq m: 388 μm Dry film weight: 1 L/sq m: 372 g/sq m
Re-coat interval: normally 10 years or more
Table 24.2 Collection of histographical data of IR-thermograms (Figs. 24.5 and 24.6) for comparison of a specimen (Fig. 24.4) on direct (s) sunshine and shielded (t) conditions: slate
roof/SRC_04
On the right: slate roof Temperature, �C On the left (Pace_04) temperature values, �C On sunshine (s) Shielded (t) Spot on the other side 36.2 31.8
Dir x/y 95/31 95/31
max 41.9 30.3
min 37.9 27.0
avg 39.4 29.2
med 39.2 29.2
sdev 0.7 0.6
skew 0.8 0.7
Ncal, pixel 1794 2420
Fmax, pixels 248 521
24 Energy Conservation Through Sunrays Reflecting Coating on Buildings 321
Applications in the Thermotechnique of Buildings
The factors affecting the infrared radiation of building surfaces and low tempera-
ture industrial equipment have not been widely enough studied. As far as building
construction is concerned, the infrared radiation emissivity of walls has been
Fig. 24.7 Equilibrium temperatures of a wall
structure (rt denotes the
thermal resistance of wall
structure) against
coefficient of heat transfer
Fig. 24.8 Equilibrium temperatures of a wall
structure (rt¼ 0.7 K m2/W) versus intensity of direct
sunshine radiation
322 I. Benk€o
regarded as an unchangeable factor basically dependent upon the temperature and
quality of their material.
The research was based on different elastometric roof coatings
(e.g. SRC-coatings), commercialized on name ‘ALUMA-CHRON’ (Data Specs of PACE Products International, Inc.), which are available also in Hungary
(MULTITREND Ltd.). The special coating is liquid-applied and cures the surface.
It is applied to forming single, tough, seem-free rubberized roof/wall membrane.
From thermal point of view the coating is a double function membrane: it saves
energy years-round, as it lowers interior temperatures in summer and its low
emissivity slows heat loss in winter.
Fig. 24.9 Values and differential ratios of
equilibrium temperatures of
wall structure vs emissivity
Fig. 24.10 Intensity of ‘heat gain’ of wall structure vs emissivity
24 Energy Conservation Through Sunrays Reflecting Coating on Buildings 323
ALUMA-CHRON’s Properties
Materials of buildings have generally good heat radiation properties, but from
energy management and building physics point of view this fact is not always
convenient. Some coating materials, e.g. ALUMA-CRON (further on: AL-CHR)
have good properties: their emissivity is considerably lower that of the material
onto which they are applied. This paper gives an account only for the infrared
emissivity decreasing effect of SRC-coating.
Performance Characteristics
AL-CHR is an elastomeric roof/wall coating available in different colours. It is
liquid-applied and it perfectly conforms to shapes. It is an economical, practical
alternative to total roof replacement. This rubberized coating provides excellent
resistance to both chemical and weather deterioration. Extensive elongation and
nearly 100% recovery allows the coating to stretch to meet changing weather
requirements as the roof expands and contracts.
AL-CHR remains flexible. It will not become rigid, crack or peel even at
temperatures of �40 �C and it keeps in heat stability under +82 �C.
Basic Uses of AL-CHR Coating
One-coat AL-CHR waterproofs, rustproofs, seal leaks, saves energy, deadens sound
of metal roofs and stretches to accommodate all sudden temperature changes
without breaking.
It restores and protects aged metal, asphalt shingles, sealed and unglazed tile and
felt (with stabilized asphalt) roofs.
It can recoat vinyl, chlorinated rubber, and epoxy coatings.
It was originally designed to fill the need for a coloured roof and tank membrane
that could handle unusual contours and steep slopes. It proved so effective that it
now is used to coat all types of roofs, tanks, silos, and stucco or masonry sidewall
where appearance, whether resistance and corrosion control are essential.
324 I. Benk€o
Role of Pigment in Sun’s Rays Utilization
Coloured pigments in living cells trap light. Light and pigments are vital to
important biological processes. There is an essential difference between chloro-
phyll molecules and the other pigments (e.g. in coat of animals): chlorophyll
participates in photosynthesis as well as giving a green leaf its colour.
Visible light and the electromagnetic spectrum. We are constantly bathed by
electromagnetic energy, from radio waves to infrared rays (heat), X-rays, and
gamma rays. Each category has a range of energies measured in oscillating waves
of specific lengths. Only the small portion of the entire electromagnetic spectrum
with wavelengths in the range 380–750 nm is visible to us as white light that can be
broken into coloured light, each colour with different wavelengths. The shorter the
wavelength, the more energetic the wave, the longer the wavelength, the less
energetic
Pigments and Absorption Spectra
The colours we see in a given object depend on which wavelengths of light the
pigments in that object absorb and which are reflected back to our because all
wavelengths are reflected. Black pigment in a coat absorbs light throughout the
whole colour spectrum and reflect nothing. Thus, it looks black to us. A leaf
contains chlorophyll-‘a’, which absorbs most strongly around 450 and 670 nm, and chlorophyll-‘b’, which absorbs most strongly around 490 and 650 nm; green light in the 500 nm range is reflected, and thus the leaf looks green. The peelings of
fruit often contain carotenoids, which absorb, wavelengths from 400 to about
550 nm and reflect back red, yellow and orange light. Because a leaf often contains
both kinds of chlorophyll plus carotenoid, its pigments can absorb and use for
photosynthesis most of the wavelengths of visible light that strike it. However
plants, algae and other autrophs use less than one percent of the energy of sunlight
in photosynthesis.
In the techniques, the spectral reflectivity of a special (Al-CHR) coating in
function of wavelength of the radiation (between 200–600 nm) is approx.
r¼ 0.5–0.7. The content of this coating is 22% pigments, 6% metallic aluminium and 23%
non-volatile liquid elastomer and lowers exterior temperature of walls of dwelling
in summer by about 5–10 K, so decreasing incoming heat of structures by some
33–38%. It slows infrared radiation heat loss by some 35–40% in winter (Data
Specs of PACE Products International, Inc.).
24 Energy Conservation Through Sunrays Reflecting Coating on Buildings 325
Results
The sunshine radiation of different samples was examined under practical condi-
tions, in direct sunshine (Benko and Kiss 1977; Benko 1981; Benko 2008). Infrared
radiation was measured by AGEMA thermal imaging equipment with a special
method. The temperature field of specimen’s surface was measured by thermocou- ples, too, in some control points (Benko 1992). The thermal imaging equipment
shows the non-uniformity of the temperature field of the specimen surface.
Conclusions
SRC coating lowers exterior temperature of wall in summer by about 5–10 �C, so decreasing incoming heat of structure by some 33–38%. It slows infrared radiated
heat loss by some 35–40% in winter (Benko 1992).
References
Benko, I., & Kiss, L. I. (1977). The struggle of mankind to ensure a comfortable thermal
environment. In The River Valley as a focus of interdisciplinary research; proceedings of the international conference to Commemorate Maupertuis’ expedition to the River Tornio, Northern Finland, 1736–1737, Oulu, Finland, 1977, p. 8.
Benko, I., Kiss, L. I. (1981). Effects of isolation and integration on the development of systems. In
Proceedings of the international conference: The Archipelago as a focus for interdisciplinary research, Turku, Finland, 1978 (pp. 49–68). Karachi: Hamdan Foundation Pakistan.
Benko, I. (1981). Possibilities of utilising renewable energy sources (Vol. 25, No. 1). Periodica
Polytechnica, Mech. Eng., Budapest, Hungary, pp. 67–86.
Benko, I. (1992). Examination of low emissivity coatings by infrared .imagery Advanced Infrared
Technology and Applications. Firenze: Grafiche Troya Publ., 1992, pp. 185–197 and 1993,
pp. 255–270.
Benko, I. (2003). The role of exergy and entropy in thermal engineering applications. In The 1st international exergy, energy and environment symposium (IEEES-1) (p. 81), Izmir, Turkey.
Benko, I. (2008). Thermal behaviour and entropy of living organisms through examples. In
Proceedings of the 2nd WSEAS/IASME international conference on energy planning, energy saving, environmental education (EPESE’08) (pp. 19–24), Corfu, Greece, October 26–28, 2008.
COEC. (1981). The solar handbook. Denver, CO: COEC. Data Specs of PACE Products International, Inc.
MULTITREND Ltd., H-1031 Budapest, Zahony u. 13., Hungary.
Postlethwait, J. H., & Hopson, J. L. (1989). The Nature of Life. New York: McGraw-Hill. Rostvik, H. N. (1992). The sunshine revolution. Stavanger, Norway: SUNLAB Publ.
326 I. Benk€o
Chapter 25
Comparison of Heating and Cooling Loads of a Typical Building with TRNSYS and eQUEST
E. Bellos, C. Tzivanidis, A. Kouvari, and K.A. Antonopoulos
Introduction
Building energy consumption is a very important parameter in the design especially
in our days with the increasing rate in the electricity cost. More specifically, the
energy consumption has increased about 50% the last years (Development Ministry
2009) in residential houses. In Europe a typical house with an average household
occupation of 2.5 persons consumes 14.2 kWh daily (http://www.mpoweruk.com/
electricity_demand.htm) and the yearly electricity consumptions is about 60 TWh
in Greece (http://en.wikipedia.org/wiki/List_of_countries_by_electricity_con-
sumption). It is obvious that energy consumption is a very important issue which
influences on our society and the new life-style. Building energy consumption for
heating and cooling is a great proportion of the total energy used. So, the knowledge
of this energy is able to create more efficient houses and systems in order to
optimize them. More specifically, by calculating with accuracy the heating and
cooling loads of a house, an optimum HVAC is able to be selected which leads to
lower electricity and fuel consumption.
It is important to find ways to lower the energy consumption of a building. For
this reason a wide variety of building energy simulation programs have been
developed, enhanced and are in use. So building designers today can use those
programs to optimize the design to reduce the heating, cooling loads and electrical
loads of the building. Some of the programs that are used worldwide on the market
either purchase or as free software are:
E. Bellos (*) • C. Tzivanidis • A. Kouvari • K.A. Antonopoulos Department of Thermal Engineering, National Technical University of Athens, Zografou,
Heroon Polytechniou 9, 15780 Athens, Greece
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_25
327
DOE-2, Equest, EnergyPlus, ESP-r, ECOTECT, DeST, TRNSYS, BLAST,
TRACE, HEED, Hap, Energy Express, BSim, Ener-Win, DOE-2.1E (Han
et al. 2014; Crwley et al. 2008).
Some studies of the building performance with simulation tools are presented
below. Xing et al. (2014) used eQuest to simulate the energy performance of an
existing four-star hotel in Tianjin, China. Terziotti et al. modelled a seasonal solar
thermal energy building with TRNSYS 16 (Terziotti et al. 2011). The combination
of ESP-r and TRNSYS is applied on a case study of a low-energy building serviced
by a solar-thermal and PV/t system (Beausoleil-Morrison et al. 2012).
Also many comparisons between these programs have been made by many
researchers. TRNSYS and Energy Plus were compared for a single module with
100 m2 of floor area for two Italian climatic conditions and the results had a
difference of approximately 10% (Gasparella and Pernigotto 2012). A comparison
between the energy analysis model established for building by eQuest and the
actual energy consumption (IPMVP method D), for an actual office building in
Taiwan was made and the final results had errors from 0.5% to 27% (Kea
et al. 2013). Zhu et al. (2013) made a comparison for loads with EnergyPlus,
DeST and DOE-2.1E. Finally, Brahme et al. (2009) compared the three more
known programs which are Equest, Energy Plus TRNSYS. According this com-
parison, eQuest is the easiest tool to use but it has a limited number of choices in
simulated systems, EnergyPlus is able to model many net zero energy technologies
with an easy way but the lack of a friendly interface is an important drawback and
TRNSYS has the greater variety in simulations but learning this program has larger
difficulties.
In our study, a comparison between eQuest and TRNSYS is made in order to
predict how close the results of these programs are. A typical building is analyzed
and parametric analyses made by changing the main parameters that influences on
heating and cooling loads.
Simulation Data
In order to make a realistic comparison the same building was developed in the two
programs and the yearly loads was calculated for the same case studies. Typical
building parameters have been selected in order to make general results. The
analysis is made for a building in Athens and the meteorological data was taken
from data bases.
Examined Building
The characteristics of the analyzed building are given in following tables
(Tables 25.1–25.3).
328 E. Bellos et al.
After these parameters it is important to refer the structural components and their
properties. Table 25.2 gives the u-value of the external walls, of the roof and of the
ground.
The values are close to each other but there are differences because every
simulation tool uses different materials. Table 25.3 gives the analytical structure
of all the components in eQuest.
In TRNSYS similar structures was selected in order to have similar u-values and
thermal masses. Now it is important to state other differences between theses
simulation tools. Another difference is in lighting strategy. TRNSYS lighting
system is depended from outside the solar irradiation level but the eQuest has an
indoor system. There are two photo sensors per zone which each one controls 50%
of lights. Each photo sensor is located 0.76 m height above the floor and 33% of
zone depth, which is 3.3 m from East and West wall. Also, it is important to state
that the exact location of every window in the respect wall is influences the results
in the eQuest and for the reason the windows are located in the center of the wall in
every case.
Finally it is important to say that TRNSYS calculated the theoretical loads of the
building when eQuest calculates the electrical consumption of the heat pumps that
Table 25.1 Building parameters
Parameter Value Parameter Value
Area 100 m2 Specific gains 14 W/m2 K
Height 3 m Occupants density 0.1 person/m2
East glass double-2 m2 Specific light 10 W/m2
West glass double-2 m2 Infiltration rate 1.12 changes per hour
South glass double-4 m2 Rotation 0� (walls in four directions) Shading coefficient 70% Insulation conductivity 0.035 W/m K
Table 25.2 U for structural components
Program External walls U (W m2 K)
Roof
U (W m2 K)
Ground
U (W m2 K)
eQuest 0.39 0.37 0.30
TRNSYS 0.38 0.39 0.29
Table 25.3 Layers of structural components
Wall
construction
Thickness
(cm)
Roof
construction
Thickness
(cm)
Ground
construction
Thickness
(cm)
ComBrick 10.15 Conc LW
30 lb
5.09 LightSoil, Damp 0.31
Polystyrene 7.62 Blt-UpRoof 0.95 Conc HW 140 lb 3.05
ComBrick 10.15 Polystyrene 7.62 Polystyrene 12.19
– Conc HW
140 lb
15.24 –
25 Comparison of Heating and Cooling Loads of a Typical Building with TRNSYS. . . 329
operates in the house. By setting the coefficient of performance equal to 1, the
electrical consumption is the same as the heating and the cooling load respectively.
So, TRNSYS calculates the loads with a direct way and the loads can be calculated
from eQuest by an indirect way. This is may lead to differences in the final results.
A last main difference of the programs is that TRNSYS uses the S.I. system but
the eQuest uses English Units.
Results
In this section the results of the simulations are presented and the comparison of the
energy tools is made. First of all the results of the main case are given and after
parametric analyses are presented.
Main Case Comparison
The yearly cooling and heating loads for the analyzed building were calculated
analytically and are presented in Fig. 25.1.
It is shown that the heating loads are close to each other for all months, except
January where TRNSYS gives greater loads. It is also important to say that eQuest
does not give heating loads for October and May. This can be explained because the
accuracy of eQuest is lower than TRNSYS, and the very low loads are taken as zero
(Fig. 25.2).
It is obvious that the results of the programs are similar with low differences. The
months April to July, TRNSYS gives greater loads but on the August and on the
September eQuest calculated greater cooling loads (Table 25.4).
The above table presents the yearly cooling and heating loads which calculated
from the two programs. It is shown that TRNSYS gives greater loads of about 5%.
This difference is acceptable and can be explained by the small differences between
the programs. These differences are related to the way that the two programs
calculate the loads and in the used materials. TRNSYS calculates the exact load
in every case in order to keep the temperature in the desire level while Equest uses
standard equipment which covers the loads. Moreover, eQuest uses a library for the
building materials but TRNSYS gives the choice of selecting the material proper-
ties in every case.
Parametric Study
In this section parametric diagrams are given in order to compare the two programs
for different cases. The parameters that changes are the following:
330 E. Bellos et al.
• Infiltration rate
• Building orientation
• Insulation thickness
• Windows area
Fig. 25.1 Monthly heating loads of the building
Fig. 25.2 Monthly cooling loads of the building
Table 25.4 Comparison of loads
Programs TRNSYS eQuest Difference
Heating 3318 3150 5.06%
Cooling 4627 4400 4.91%
25 Comparison of Heating and Cooling Loads of a Typical Building with TRNSYS. . . 331
Infiltration Rate
The infiltration rate of a building is very important and influences on the loads a lot.
So the parametric analysis for this is of a high importance (Figs. 25.3 and 25.4).
From Fig. 25.3 it is shown that heating loads has an increasing rate for greater
values of infiltration. On the other hand, the cooling load is lower in the cases of
greater infiltration rate. A simple explanation for these results is that the summer
heat from windows is stored in the inside air and the more air changes help fresh and
colder air to get into the house. It is obvious that the two programs give similar
results with low differences.
Building Orientation
The orientation of the building is able to influence on the loads because of the
existence on the windows. For example, a south window let greater amount of solar
irradiation to through into the house compared to a north window. Figures 25.5 and
25.6 present the heating and cooling loads for a full reverse of the building, from
�180� to þ180�. Low differences between the programs are observed from Figs. 25.5 and 25.6.
The curves are not symmetrical to the vertical line to 0�, because the East and the West irradiation is not the same. The minimum heating load is achieved when the
south wall azimuth is 0� because of the large window is located in this wall and in this case it lets the solar irradiation to through into the house with the greatest way.
On the other hand, the cooling load in this case is the maximum, because of the high
irradiation leads to a great cooling load.
Fig. 25.3 Heating loads for different infiltration rate
332 E. Bellos et al.
Fig. 25.4 Cooling loads for different infiltration rate
Fig. 25.5 Heating loads for different building orientation
Fig. 25.6 Cooling loads for different building orientation
25 Comparison of Heating and Cooling Loads of a Typical Building with TRNSYS. . . 333
Insulation Thickness
The existence of insulation is the most important parameter for the load reduction
and especially for the heating load. The thickness of this layer is an optimization
issue and it is analyzed in the following schemes (Fig. 25.7).
Figure 25.8 shows that the higher thickness of insulation lead to lower heating
energy consumption, but after 8 cm, the influence on the loads is very low.
TRNSYS and eQuest give similar results according the curves and while the
thickness is greater, the curves come very close to each other. On the other hand,
the cooling energy consumption has a strange behavior. More specifically, the
eQuest simulation proves that the greater insulation is beneficial for the building
load, by decreasing them when TRNSYS shows that the insulation layer increases
these. The values for cooling does not differs a lot as values, but the derivative of
the one is negative and of the other positive. A possible explanation is that the two
programs make the energy balance of the building with different way.
Windows Area
The existence of windows in a building changes a lot the heating and the cooling
loads. The windows let the solar energy through into the house, which means that
the indoor air is getting warmer. Simultaneously, the U-value of the windows is
greater than the wall, fact that leads to high losses in the night. The following
diagrams assume the building performance for different values of total windows
area. It is important to say that the 50% of the total windows area is located to the
south wall, the 25% to the east and the other 25% to the west (Figs. 25.9 and
25.10).
Fig. 25.7 Heating loads for different insulation layer thickness
334 E. Bellos et al.
The above diagrams show that the two programs give similar result, with the
heating load to be lower for a higher windows area and the cooling load has the
reverse behavior. The climate of Athens explains these results because of the high
summer irradiation level in the summer increases the cooling loads when greater
windows are put in the building.
Table 25.5 gives the men differences between the two energy tools for all study
cases.
Table 25.5 shows all the results by giving the mean differences between pro-
grams for the all cases. The main case, which is about the firstly building, which
Fig. 25.8 Cooling loads for different insulation layer thickness
Fig. 25.9 Heating loads for different Windows Area
25 Comparison of Heating and Cooling Loads of a Typical Building with TRNSYS. . . 335
examined, gives differences of about 5% in cooling and heating loads which is
acceptable. The difference in the orientation change is in the same proportion; while
in the other cases differences of 10–15% are observed. Finally the mean difference
of the heating load is about 10% and in the cooling 8%, assuming all the cases of
our analysis.
Conclusions
In this analysis two very known simulation tools for energy calculations in build-
ings are compared in order to validate the one from the other. The differences were
low which shows that the results are similar in the majority of the cases. More
specifically:
• It is important to state that the way that the loads are calculated are different
because of TRNSYS calculates the theoretical load every moment in order to
keep the desired temperature while eQUEST uses a heat pump system to satisfy
the preferable inside temperature.
Fig. 25.10 Cooling loads for different Windows Area
Table 25.5 Final comparison for all the studied cases
Case Heating difference (%) Heating difference (%)
Main case 5.06 4.91
Infiltration rate 11.00 13.36
Orientation 6.54 3.65
Insulation thickness 15.89 8.76
Windows area 12.61 9.24
Mean value of all the cases 10.22 7.98
336 E. Bellos et al.
• The results of this analysis are easily generated because in every parameter
typical and usual values have been selected which match with the real
constructions.
• In the main case, the difference of the loads in the two programs is very low,
about 5%.
• In other parametric cases, greater differences of about 10–15% are observed.
• It is important to state that the heating loads have greater differences between the
two programs compared to the differences in cooling loads with 10% and 8%
respectively.
• In all cases, the derivative of the curves is the same except from Fig. 25.8, which
shows the cooling energy consumption for different thickness of the insulation
layer. TRNSYS gives greater cooling load for greater thickness, while eQuest
has the gives results.
• The main conclusion of this comparison is that the two programs can be
validated by this analysis and the small difference can be explained by the
different way that the programs cover the heating and cooling loads. So the
two programs use different approximations in order to predict the loads of the
building.
• Finally it is important to state that TRNSYS is able to calculate the building
loads with greater accuracy because the material properties are able to be fully
determined by the user and calculate the exact value of the loads. So, to make a
more realistic approach for the Greek environmental conditions, TRNSYS is the
suitable choice.
References
Beausoleil-Morrison, I., Kummert, M., Macdonald, F., Jost, R., McDowell, T., & Ferguson,
A. (2012). Demonstration of the new ESP-r and TRNSYS co-simulator for modeling solar buildings, Energy Procedia, 30, 505–514.
Brahme, R., O’Neill, Z., Sisson, W., & Otto, K. (2009). Using existing whole building energy tools for designing net-zero energy buildings—Challenges and workarounds. In Eleventh interna- tional IBPSA conference, Glasgow, Scotland.
Crwley, D. B., Hand, J. W., Kummert, M., & Griffith, B. T. (2008). Contrasting the capabilities of building performance simulation programs, Building and Environment, 43(4), 661–673.
Development Ministry. (2009). The Greek energy system. Gasparella, A., & Pernigotto, G. (2012). Extensive comparative analysis of two building energy
simulation codes for southern Europe climates: Heating and cooling energy needs and peak loads calculation in TRNSYS and EnergyPlus, International High Performance Buildings Conference, 3556, Purdue.
Han, Y., Liu, X., & Chang, L. (2014). Comparison of software for building energy simulation.
Journal of Chemical and Pharmaceutical Research, 6(3), 467–471. http://en.wikipedia.org/wiki/List_of_countries_by_electricity_consumption
http://www.mpoweruk.com/electricity_demand.htm.
Kea, M.-T., Yeh, C.-H., & Jian, J.-T. (2013). Analysis of building energy consumption parameters and energy savings measurement and verification by applying eQUEST software, Energy and Buildings, 61, 100–107.
25 Comparison of Heating and Cooling Loads of a Typical Building with TRNSYS. . . 337
Terziotti, L. T., Sweet, M. L., & McLeskey Jr., J. T. (2011). Modeling seasonal solar thermal energy storage in a large urban residential building using TRNSYS 16, Energy and Buildings, 45, 28–31.
Xing, J., Ren, P., & Ling, J. (2014). Analysis of energy efficiency retrofit scheme for hotel buildings usingeQuest software: A case study from Tianjin, China. www.elsevier.com/locate/enbuild.
Zhu, D., Hong, T., Yan, D., & Wang, C. (2013). A detailed loads comparison of three building
energy modeling programs: EnergyPlus, DeST and DOE 2.1E. Building Simulation.
338 E. Bellos et al.
Chapter 26
Optimum Insulation Thickness for Cooling Applications Through Exergy Analysis and Environmental Methods
Beyza Nur Daldal, _Ibrahim Sarıo�glu, Gülcan €Ozel Erol, Emin Açıkkalp, and Hasan Yamık
Introduction
In Turkey, heating and cooling applications constitute 80% of the total energy
consumption in the buildings. Also, the building sector is the second largest energy
consumer thus it is an important area for improving of energy savings and effi-
ciency (Dombaycı 2009).
Energy is basic for humankind and it one of the most important parts of the
sustainable development, however, environmental problems becomes a really seri-
ous problem, while energy needs increases. Until recently, energy conversion
systems has been only designed and improved by using the economic and efficiency
parameters. However, environmental impact analysis has gain importance with the
increasing environmental problems such as global warming, natural resource
depletion and climate changes in recent years. It is shown that some new design
and improvement parameters that provide us evaluation for environmental impact
are an obligation for the energy conversion systems. Some countries have already
obligated the environmental impact assessment with laws (Dasdemir 2011).
In the literature, there are many study about optimum insulation thickness for
cooling and heating applications (Gürel and Dasdemir 2011; Dagıdır 2011;Arslan
et. all 2010; Kurekci 2016). They are used energy, exergy and economic analysis
for determining optimum insulation thickness for different cooling applications. In
this study, it presented a novel method that combined environmental impact and the
exergy analysis to determine the optimum insulation thickness is performed. Cal-
culations are carried out for two insulation materials and wall types.
B.N. Daldal (*) • İ. Sarıo�glu • G. Özel Erol • E. Açıkkalp • H. Yamık Department of Mechanical and Manufacturing Engineering, Faculty of Engineering, Bilecik
S.E. University, Bilecik, Turkey
e-mail: [email protected]; [email protected]; [email protected];
[email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_26
339
Modeling and Analysis
In this study, exergy analysis is combined with the environmental impact analysis
for determining the optimum insulation thickness for the cooling applications. Ambi-
ent temperature is assumed as 313 K and the indoor temperature is assumed as 295 K.
Electricity is used as fuel for the cooling system (air conditioner). Optimum insula-
tion thickness is investigated for two different wall and two different insulation
materials. The investigated walls are illustrated in Fig. 26.1. All calculations are
conducted for the unit wall area and annual process (Table 26.1).Please check the
renumbering of figures/tables/equations and their citations, and correct if necessary.
equation 26.4 have been deleted and the other equatins have revised.
Annual cooling loss in unit area (kJ/m2-year) from the wall is calculated as
follow (Cengel 1998):
q ¼ 0:024ðCDDÞU ð26:1Þ
where CDD is cooling degree-days (�C.day), and U is heat transfer coefficient (W/m K). Annual energy need (kJ/m2-year) for the unit wall area is calculated as
following (Cengel and Boles 2006):
E ¼ 0:024ðCDDÞU COP
ð26:2Þ
Annual exergy loss (kJ/m2-year) is defined as (Cengel and Boles 2006):
Exloss ¼ 0:024ðCDDÞU COP
1� To Ti
! ð26:3Þ
where Ti is the indoor temperature (K) and To is the ambient temperature (K). COP is the coefficient of the performance for the cooling system. Heat transfer
coefficient (W/m K) for no-insulation and insulation wall conditions are shown in
Eqs. (26.4) and (26.5) respectively (Cengel 1998).
Fig. 26.1 Schematic of the investigated system for wall I (a) and wall II (b)
340 B.N. Daldal et al.
Unins ¼ 1 Ri þ Rw þ Ro ¼
1
R ð26:4Þ
Uins ¼ 1 Ri þ Rw þ Ro þ Rins ¼
1
Rþ x=k ð26:5Þ
Environmental impact function of the system (mPts/m2-year) is;
BT ¼ ðbf :ExlossÞ þ ðbins:ρ:xÞ ð26:6Þ
where bf is the environmental impact of the electricity (mPts/kWh), bins is the environmental impact of the insulation materials (mPts/ kg), ρ is the density of the insulation materials and x is the insulation thickness. CO2 emission is given in the environmental impact of the electricity. The net saving of the environmental impact
(mPts/m2-year) is;
S ¼ ðbf :ExlossÞ þ ðbins:ρ:xÞ
ins
� ðbf :ExlossÞnins ð26:7Þ
The net saving of the exergy loss (kJ/m2-year) is;
SEx ¼ Exlossð Þnins � Exlossð Þins ð26:8Þ
The optimum insulation thickness is calculated by taking the derivative of BT and set equal to zero. Data used in calculations can be seen in Table 26.2.
Table 26.1 Properties of walls (TS 825) used in this study
Wall types
Thickness
(m)
Thermal
conductivity (W/m K)
Overall heat transfer
coefficient (W/m2 K)
Heat
resistance
(m2 K/W)
Wall I 1.572 0.636
External
plaster
0.03 1.40
Internal
plaster
0.02 0.87
Horizontal
coring brick
0.19 0.45
Wall II 1.772 0.564
External
plaster
0.03 1.60
Internal
plaster
0.02 1
Gasconcrete 0.25 0.16
26 Optimum Insulation Thickness for Cooling Applications Through Exergy. . . 341
Results and Discussion
In this study, environmental impact analysis is combined with exergy analysis for
determining the optimum insulation thickness of a building wall. The rockwool and
glasswool are used as insulation material for the analysis. Wall I and wall II are the
investigated systems which are the most commonly used wall arrangements in
Turkey.
In Fig. 26.2a and b, variations of the total environmental impact and the net
savings of the environmental impact with insulation thickness for the glasswool are
shown for wall I and II. As appears in the graphics, initially the environmental
impact decreases dramatically and achieves a minimum point called the optimum
point. After the optimum point, it starts to increase in small steps. When glasswool
is used as the insulation material for wall 1 and 2, optimum points are calculated as
0.052 m and 0.054 m respectively. While the environmental impact decreases until
the optimum point, the net savings of the environmental impact increases contin-
uously. At optimum points for wall I and II, environmental impact points are
determined as 11.67 and 11.88 mPts/m2-year respectively.
In Fig. 26.3a and b, change of the exergy loss and the net exergy savings
according to the insulation thickness from the wall 1 and 2 is illustrated. Exergy
losses decreases with insulation thickness. At optimum points exery loss decreases
by 60.8% and 74.95% compared with the no insulation conditions. In Fig. 26.4a
and b, the variations of the total environmental effect and the net savings of the
environmental impact with insulation thickness for the rockwool are shown for wall
I and II. When the rockwool is used as the insulation material for wall I and II,
optimum points are calculated as 0.01 m and 0.015 m respectively. At these points,
the environmental impact of the system reaches its minimum. Rockwool has
relatively lower optimum points than the glasswool.
Table 26.2 Parameters used in calculations
Parameter Unit Value
Heat conduction coefficient (Izocam 2013) W/m K
Rockwool 0.04
Glasswool 0.032
Environmental impact point mpts/kg
Rockwool (Eco-indicator 99 2014) 4.2
Glasswool (Eco-indicator 99 2014) 2.1
Electricity (Eco-indicator 95 2014) 27
Mean temperature for heating period �C 22 Heating degree day (Dombaycı 2009) �C-days 661 COP (Dasdemir 2011) 2.4
Density of insulation material kg/m3
Rockwool (Dombaycı 2009) 105
Glasswool (Dombaycı 2009) 45
342 B.N. Daldal et al.
0.00 0.02 0.04 0.06 0.08 0.10 10
12
14
16
18
20
22
24
26
a
b
BT S
E nv
iro nm
en ta
l i m
pa ct
(m P
ts /m
2 - ye
ar )
E nv
iro nm
en ta
l i m
pa ct
(m P
ts /m
2 - ye
ar )
0
2
4
6
8
10 T
he net environm ental saving (m
P ts/m
2-year)
10
12
14
16
18
20
22
24
26
28
insulation thickness (m)
T he net environm
ental saving (m P
ts/m 2-year)
0.00 0.02 0.04 0.06 0.08 0.10
BT S
insulation thickness (m)
0
2
4
6
8
10
Fig. 26.2 Change of the environmental impact and
the net saving with
insulation thickness for
glasswool, (a) wall I, (b) wall II
0.00 0.02 0.04 0.06 0.08 0.10 -0.1
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
SEx Exloss
insulation thickness (m)
T he
n et
e xe
rg y
lo ss
s av
in g
(k J/
m 2 -
ye ar
)
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
E xergy loss (kJ/m
2-year)
0.00 0.02 0.04 0.06 0.08 0.10 -0.1
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0a b
SEx Ex
loss
insulation thickness (m)
T he
n et
e xe
rg y
lo ss
s av
in g
(k J/
m 2 -
ye ar
)
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
1.1
E xergy loss (kJ/m
2-year)
Fig. 26.3 Change of the exergy loss and the net exergy loss saving with insulation thickness for glasswool, (a) wall I, (b) wall II
In Fig. 26.5a and b, the change of the exergy loss and the net exergy saving of the
optimum insulation thickness are presented for wall I and II. Using the rockwool as
insulation material it cause to decrease the exergy saving from the wall I and II by
17% and 40% compared with the no insulation conditions
0.00 0.02 0.04 0.06 0.08 0.10 15
20
25
30
35
40
45
50
BT S
insulation thickness (m)
E nv
iro nm
en ta
l i m
pa ct
( m
P ts
/m 2 -
ye ar
) E
nv iro
nm en
ta l i
m pa
ct (
m P
ts /m
2 - ye
ar )
0
10
20
30
40
50 The net environm ental saving (m
P ts/m
2-year) T
he net environm ental saving (m
P ts/m
2-year)
0.00 0.02 0.04 0.06 0.08 0.10 20
25
30
35
40
45
50
insulation thickness (m)
0
10
20
30
40
BT S
a
b
Fig. 26.4 Change of the environmental impact and
the net saving with
insulation thickness for
rockwool, (a) wall I, (b) wall II
344 B.N. Daldal et al.
Conclusions
In this study, exergy based environmental impact analysis is used to determine the
optimum insulation thickness for cooling applications. As mentioned above, global
warming has gained attention in recent decades and buildings have an important
effect on energy consumption and environmental issues. Some important results
obtained from the analysis can be listed as follows:
• Environmental impacts decrease according to the optimum insulation thickness.
• For the rockwool, optimum points are as 0.052 m and 0.054 m for wall I and II
respectively.
• For the glasswool, optimum points are as 0.01 m and 0.015 m for wall I and II
respectively.
• At optimum points exergy savings increase considerably compared with the no
insulation conditions.
We get more efficient, less energy consumption and more environmental in the
optimum insulation thickness.
According to these results, the environmental effects should be investigated as
well as the economic effects to provide sustainable development.
Nomenclature
b Environmental impact point, mPts/kg-mPts/kWh
B Environmental impact rate associated with exergy, mPts
CDD Cooling degree-days, �C.day COP Coefficient of performance for the cooling system
E Annual energy need for unit wall area, kJ/m2-year
0.00 0.02 0.04 0.06 0.08 0.10 -0.1
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8 a b
SEx Exloss
insulation thickness (m)
T he
n et
e xe
rg y
lo ss
s av
in g
(k J/
m 2 -
ye ar
)
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
E xergy loss (kJ/m
2-year)
0.00 0.02 0.04 0.06 0.08 0.10
0.0
0.2
0.4
0.6
0.8 SEx Exloss
insulation thickness (m)
T he
n et
e xe
rg y
lo ss
s av
in g
(k J/
m 2 -
ye ar
)
0.2
0.4
0.6
0.8
1.0
E xergy loss (kJ/m
2-year)
Fig. 26.5 Change of the exergy loss and the net exergy loss saving with insulation thickness for rockwool, (a) wall I, (b) wall II
26 Optimum Insulation Thickness for Cooling Applications Through Exergy. . . 345
El Annual electricity consumption for unit wall area, kJ/m2year
Ex Annual heat exergy, kJ/m2-year
k Thermal conductivity, W/m K
q Annual heat loss for unit wall area, kJ/m2-year
R Heat resistance, K/W
S Annual net saving of environmental impact, mPts/m2-year
SEx Annual net saving of the exergy loss, kJ/m2-year
T Temperature, �C or K U Heat transfer coefficient, W/K
x Insulation thickness, m
Subscripts
o Ambient
f Fuel
i Indoor
ins Insulation
loss Loss
nins No-insulation
T Total
w composition
Greek Letter
ρ Density, kg/m3
References
Arslan, O., Ozgur, M. A., Yıldızay H. D., Kose, R., (2010). Fuel Effects on Optimum Insulation
Thickness: An Exergitic Approach, Energy Sources, Part A, 32, 128–147.
Cengel, Y. A. (1998). Heat transfer: A practical approach (1st ed.). Hightstown: McGraw-Hill. Cengel, Y. A., & Boles, M. A. (2006). Thermodynamics an engineering approach (5th ed.).
Hightstown: McGraw-Hill.
Dagıdır, C., (2011). Determination of Optimum Insulation Thickness by Considering Solar
Radiation in Buildings of Warm Climate Regions, M. Sc Thesis, Graduate School of Applied
and Natural Sciences, Süleyman Demirel University, Isparta, TURKEY.
Dasdemir, A. (2011). Heating and cooling applications energy saving of optimum thickness and
the effect of the flue gas emission M. Sc Thesis, Graduate School of Applied and Natural
Sciences, Karabuk University, Karabuk, TURKEY.
Dombaycı, Ö. A. (2009). Degree-days maps of Turkey for various base temperatures. Energy, 34, 1807–1812.
Goedkoop, M., & Spriensma, R. (2014, March). The Eco-indicator 99: A damage oriented method
for life cycle impact assessment. Methodology report, 2000, Amersfoort, Netherlands. http://
www.pre.nl.
346 B.N. Daldal et al.
Gürel, A. E., Dasdemir, A. (2011). Economical and Environmental Effects of Thermal Insulation
Thickness in Four Different Climatic Regions of Turkey, International Journal of Renewable
Energy Research, Vol.1 , No.1, 1–10.
Kurekci, N.A., (2016). Determination of optimum insulation thickness for building walls by using
heating and cooling degree-day values of all Turkey’s provincial centers, Energy and Build- ings, 118, 197–213.
Retrieved March 2013 from http://www.izocam.com.tr/tr-tr/urunler/yalitim-malzemeleri.aspx.
The Eco-indicator 95. (2014, March). http://www.pre-sustainability.com/eco-indicator-95-final-
report, http://www.pre.nl.
Turkish Standards Institution (TSE). (1998). TS 825: Thermal insulation in buildings. Ankara, Turkey: TSE Publications.
26 Optimum Insulation Thickness for Cooling Applications Through Exergy. . . 347
Chapter 27
Novel Tungsten Bronze Nanoparticles for Shielding Near Infrared Ray and Decreasing CO2 Emission
Tsugio Sato, Chong-shen Guo, and Shu Yin
Introduction
Recently, much attention has been attracted for the smart windows to reduce the
energy consumption for air conditioning, and, thereby, to decrease the carbon
dioxide emission by shielding the heat-ray from the sunlight into the room in
summer, and from the room to the outside in winter for automobiles, buildings,
etc. In case of the smart window, the high transparency of visible light and high
shielding ability of NIR light are required. In order to cut off the heat-rays, the
shielding of the near infrared light by the electronic plasma is used (Kreibig and
Vollmer 1995). Namely, the electronic plasma frequency (Wp) of the conductive
materials is expressed by Eq. (27.1)
Wp 2 ¼ 4πne2=m ð27:1Þ
where n is free electron density and m is electronic mass. It is known that the
electromagnetic wave with the lower frequency than plasma frequency is not able
to pass the plasma. Therefore, it is possible to shield the near infrared rays by
controlling the free electron density of the conductive materials. In addition, it is
well known that the scattering of lights by the particles greatly changes depending
on the particle size, and nano particles less than 20 nm in diameter are quite
transparent, since the Rayleigh scattering intensity (s) is proportional to the particle
size (d) to the six power as shown by Eq. (27.2).
T. Sato (*) • C.-s. Guo • S. Yin Institute of Multidisciplinary Research for Advanced Materials, Tohoku University,
2-1-1 Katahira, Aoba-ku, Sendai 980-8577, Japan
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_27
349
s ¼ Kd6=λ4 ð27:2Þ
Nowadays, the thin films of various nanosized conductive compounds such as
silver (Kreibig and Vollmer 1995), indium tin oxides (ITO) (Yang et al. 2009), etc.
are widely used as solar filters (Okada et al. 2003; Hammarberg and Roos 2003;
Adachi and Miratsu 2010; Takeda et al. 1998), however, the performances of the
these materials are not satisfactory. We focused the attention on the hexagonal
tungsten bronze compounds with the chemical formula of MxWO3 consisting of the
mixed valence of W6þ and W5þ, where M is alkali metal ion which locates in the space of the WO3 layer. The free electron density of tungsten bronze can be
controlled by controlling the amounts of Mþ. There are lots of tungsten bronze compounds, but the cesium tungsten bronze shows the most excellent chemical
stability because of the adequate ionic size matched with the space size in the WO3 layer. Takeda and Adachi (2007) prepared cesium tungsten bronze nanoparticles for
near infrared light shielding by the solid state reaction under severe reaction
conditions, such as hydrogen gas atmosphere above 800 �C, followed by energy consuming milling process. Now, we tried the direct fabrication of the cesium
tungsten bronze nanocrystals by solvothermal reaction under mild conditions.
Experimental
In a typical experiment, after dissolving desired amounts of WCl6 and CsOH in
ethanol separately, both solutions were added into the ethanol and acetic acid mixed
solution to precipitate amorphous gel precursor, followed by solvothermal reactions
at a desired temperature to form CsxWO3 nanocrystals by the dissolution-
crystallization mechanism. In order to evaluate NIR shielding performance, the
product was dispersed in a collodion-ethanol mixed solution, and then, coated on a
quartz glass by a doctor-blade method using an applicator of 12.5 μm film thickness.
Results and Discussion
Figures 27.1 and 27.2 shows the X-ray diffraction patterns of the products obtained
in (a) pure ethanol and (b) 90 vol.% ethanol-10 vol.% acetic acid mixture at 240 �C. Both samples consisted of the single phase of the hexagonal cesium tungsten
bronze, but the morphology was greatly different. It can be seen that the irregularly
agglomerated large particles were formed in pure ethanol. In contrast, the samples
synthesized in 10 vol.% acetic acid contained ethanol solution consisted of well-
dispersed rod-like nanoparticles with about 15 nm in diameter and 50 nm in length.
350 T. Sato et al.
By increasing the acetic acid content up to 40 vol.%, the size of nanorods could be
decreased, but the agglomeration of particles proceeded.
Table 27.1 shows the Cs/W atomic ratio and CsxWO3 yield in ethanol mixed
with various amounts of acetic acids. It can be seen that the Cs/W atomic ratio and
CsxWO3 yield in pure ethanol were quite low, but Cs/W atomic ratio increased to
almost 0.33, which is the ideal value of tungsten bronze structure, and CsxWO3 yield increased to nearly 100% by adding acetic acid.
In order to confirm the reaction mechanism to promote the formation of tungsten
bronze by adding carboxylic acid, the chemical compositions of the reaction
solutions after solvothermal reaction were analyzed by NMR. It was found that
the peaks corresponding to not only the ethanol and acetic acid which were used as
starting solvents, but also ethyl acetate and diethyl ether were determined. These
Ref, Cs0.32WO3
2 q Cuka /deg 10 20 30 40 50 60
a
b
70 80
Fig. 27.1 XRD patterns of samples synthesized in (a) pure ethanol and (b) 90 vol. % ethanol-10 vol.% acetic
acid mixed solutions at
240 �C for 20 h (reference: Cs0.32WO3, JCPDS
No. 831334)
Fig. 27.2 Scanning electron micrographs of samples synthesized in (a) pure ethanol and (b) 90 vol.% ethanol-10 vol.% acetic acid mixed solutions at 240 �C for 20 h with a nominal Cs/W atomic ratio of 0.5
27 Novel Tungsten Bronze Nanoparticles for Shielding Near Infrared Ray. . . 351
results indicate that the esterification and etherification shown by Eqs. (27.3) and
(27.4) proceeded during the solvothermal reaction, and water generated by these
reactions played an important role to form CsxWO3 nanocrystals.
CH3CH2OH þ CH3COOH ¼ CH3CH2OOCCH3 þ H2O Esterificationð Þ ð27:3Þ
2CH3CH2OH ¼ CH3CH2OCH2CH3 þ H2O Etherificationð Þ ð27:4Þ
It is considered that water promotes the hydrolysis of WCl6, and ethanol pro-
motes the reduction of W6þ to W5þ to form CsxWO3. In case of pure ethanol, due to the low reaction rate of the dehydration condensation reaction of ethanol to
generate water, the rate of CsxWO3 formation is slow. By adding acetic acid in
ethanol, the rate of water generation increases, therefore, the formation of CsxWO3 was promoted. When excess amount of acetic acid is added in ethanol, the water-
releasing rate becomes too high to proceed the agglomeration. Therefore, the
optimum acetic acid content exists to form well dispersed nanocrystals of
Cs0.33WO3.
By the XPS analysis, it was confirmed that tungsten trioxide (WO3) consisted of
only W6þ, but cesium tungsten bronze crystal (CsxWO3) consisted of the mixed valences of W6þ and W5þ as shown in Fig. 27.3.
Transmittance spectra of CsxWO3 particles synthesized in (a) pure ethanol
(b) 90 vol.% ethanol-10 vol.% acetic acid, (c) 80 vol.% ethanol-20 vol.% acetic
acid, (d) 60 vol.% ethanol-40 vol.% acetic acid solutions at 240 �C for 20 h with Cs/W atomic ratio of 0.5 and (e) WO3 particles are shown in Fig. 27.4. As-expected,
tungsten trioxide (WO3) consisted of only W 6þ did not show NIR shielding
ability, but CsxWO3 consisted of the mixed valences of W 6þ and W5þ showed
NIR-shielding ability, where the NIR-shielding ability greatly changed depending
on the reaction conditions, indicating that well dispersed nanocrystals of CsxWO3 showed excellent heat ray shielding performance.
In order to confirm the heat-ray shielding performance of CsxWO3, the simulated
experiments were carried out by a 50 W Halogen lamp radiating to three boxes
sealed by quartz glass, CsxWO3 coated quartz glass and ITO glass. The tempera-
tures in the boxes after 1 h irradiation are listed in Table 27.2. It can be seen that the
temperature in the box covered by a quartz glass increased up to 34.2 �C after 1 h irradiation. The temperature increment could be depressed by using an ITO glass,
Table 27.1 Cs/W atomic ratio and CsxWO3 yield in
ethanol mixed with various
amounts of acetic acids
CH3COOH
content/vol.% Cs/W atomic ratio CsxWO3 yield/%
0 0.26 65.1
10 0.31 90.0
20 0.32 96.2
40 0.29 95.5
352 T. Sato et al.
WO3
40 39 38 37
Binding Energy/eV
36 35 34 33
CSxWO3
W6+ W5+ W5+W6+
Fig. 27.3 W4f core-level XPS spectra of CsxWO3 nanorods prepared in 90 vol.
% ethanol-20 vol.% acetic
acid mixed solution at
240 �C for 20 h with Cs/W atomic ratio of 0.5 and WO3
UV VIS NIR lights
300
0
20
40
60
80
100
600 900 1200
(e)
(a)
(d)
(c)
(b)
Wavelength/nm
T ra
n sm
it ta
n ce
/%
1500 1800 2100 2400
Fig. 27.4 Transmittance spectra of CsxWO3 particles synthesized in (a) pure ethanol (b) 90 vol.% ethanol-10 vol.% acetic acid, (c) 80 vol.% ethanol-20 vol.% acetic acid, (d) 60 vol.% ethanol- 40 vol.% acetic acid solutions at 240 �C for 20 h with Cs/W atomic ratio of 0.5 and (e) WO3 particles
Table 27.2 Temperatures in the boxes covered by quartz
glass, ITO glass and CsxWO3 coated quartz glass after 1 h
irradiation by a 50 W
halogen lamp
Box Temperature/�C Quartz glass 34.2
ITO glass 30.0
CsxWO3 coated quartz glass 24.4
Temperature before irradiation: 20.0
27 Novel Tungsten Bronze Nanoparticles for Shielding Near Infrared Ray. . . 353
but still caused a remarkable increase in temperature up to 30.0 �C. In contrast, the temperature increment was limited to 24.4 �C by using a Cs0.32WO3 coated quartz glass, indicating the excellent heat-ray shielding performance of the CsxWO3 nanocrystals.
Conclusions
From the present results, following conclusions may be drawn. (1) The CsxWO3 nanocrystals were successfully synthesized by solvothermal process. (2) The well
dispersed CsxWO3 nanocrystals showed the excellent NIR shielding ability as well
as high transmittance in the visible light range.
References
Adachi, K., & Miratsu, M. (2010). Absorption and scattering of near-infrared light by dispersed
lanthanum hexaboride nanoparticles for solar control filters. Journal of Materials Research, 25, 510–521.
Hammarberg, E., & Roos, A. (2003). Antireflection treatment of low-emitting glazings for energy
efficient windows with high visible transmittance. Thin Solid Films, 442, 222–226. Kreibig, U., & Vollmer, M. (1995). Optical properties of metal clusters. In J. P. Toennies (Ed.),
Springer series in materials science (Vol. 25). New York: Springer. Okada, M., Yamada, Y., Jin, P., Tazawa, M., & Yoshimura, K. (2003). Fabrication of
multifunctional coating which combines low-e property and visible-light-responsive
photocatalytic activity. Thin Solid Films, 442, 217–221. Takeda, H., & Adachi, K. (2007). New infrared absorption of tungsten oxide nanoparticle
dispersions. Journal of American Ceramic Society, 90, 4059–4061. Takeda, H., Otsuka, Y., Kuno, H., & Adachi, K. (1998). Coating solution for a heat-ray shielding
film and a process for forming a heat-ray shielding film by employing the same. US Patent
No. 5,840,364.
Yang, L. L., Ge, D., Wei, H., He, F., & He, X. D. (2009). Morphology and characterization of ITO-
Ag-ITO films on fibers by layer-by-layer method. Applied Surface Science, 255, 8197–8201.
354 T. Sato et al.
Chapter 28
Modelling of a Solar Assisted Floor Heating System with TRNSYS
E. Bellos, C. Tzivanidis, A. Prassas, and K.A. Antonopoulos
Introduction
Energy consumption in buildings has a very important role with a proportion of
40% of the total energy in Europe. Especially energy consumption for heating and
cooling is responsible for 70% of building consumption which is a great percentage
(European Environment Agency 2010). More specifically, the specific heating
consumption for typical buildings varies from 15 kWh/m2 year to 100 kWh/m2
year (Asimakopoulos et al. 2012; Theodoridou et al. 2011). In order to cover this
load, many technologies are used and this research field evolves rapidly. Solar
energy utilization is very beneficial because of the zero operating cost and is able to
cover great loads in countries with high irradiation level as Greece. With a solar
potential of 1600 kWh/m2 year in Athens (Fantidis et al. 2013; Kouremenos
et al. 1985), the solar energy exploitation is a feasible solution for covering the
building heating loads.
Simultaneously, underfloor heating systems are a heating technology which is
used with an increasing rate because provide to occupants more satisfactory indoor
micro-climate (Gao et al. 2011). The first steps of this technology were in Germany
in 1970s in commercial buildings (David 1984) and in data centers of high heat and
fewer people (Sodec and Craig 1990). Nowadays, the 50% if the new constructed
Europe buildings uses this technology (Kilkis et al. 1994) because underfloor
heating systems reduces the seasonal heating about 18% (Ghali 2007) and improve
the thermal comfort conditions inside the buildings (Inard et al. 1998).
Many analyses have been done in this area, Alajmi and El-Amer developed an
underfloor-air-distribution system and proved that this system saves energy
E. Bellos (*) • C. Tzivanidis • A. Prassas • K.A. Antonopoulos Department of Thermal Engineering, National Technical University of Athens,
Zografou, Heroon Polytechniou 9, 15780 Athens, Greece
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_28
355
compared to ceiling-based air distribution (Alajmi and El-Amer 2010). Other
studies prove the improvements in thermal comfort conditions by using an
underfloor heating system (Myhren and Holmberg 2008; Sekhar and Ching 2002;
Hasan et al. 2009). Zhai et al. (2009) studied the design and performance of the
solar-powered floor heating system in for a typical building. Badran and Hamdan
made a theoretical and an experimental study for under-floor heating system using
solar collectors and solar pond. They finally proved that the system with solar
collector is 7% more efficient than the solar pond system (Badran and Hamdan
2004). In other studies, Athienitis made a numerical model to predict the underfloor
heating load under high solar gain and conclude that controllers should be used in
order the floor temperature does not exceed the comfort limits (Athienitis 1994).
Al-Khalayleh et al. in a theoretical investigation of an underfloor heating system
coupled with solar collectors proved that solar energy is able to cover the heating
load sufficiently (Al-Khalayleh et al. 1999).
In this study the solar energy utilization is analyzed for heating a typical building
with an underfloor heating system. The combination of these is suitable for Greek
high solar potential and leads to an optimum performance. The simulation is done
by commercial software TRNSYS which uses an active layer to simulate the
underfloor heating system.
General Information
In this paragraph the building description, the underfloor system modelling and the
basic mathematical equations are presented in order to make the next analysis
feasible.
Examined Building
The building of this study is a cubic building with double glass windows in south,
east and west direction. The characteristics of the building are presented in
Table 28.1. Simultaneously the specific loads of the building are presented in the
same table.
The structure and the composition of outer walls influence on the thermal
behavior of the building. Table 28.2 presents the material properties which have
the default TRNSYS values.
The building consists of four outer same walls and a roof without having internal
walls. The roof of the building has three layers; the outer is cement with 20 cm
thickness, the intermediate is insulation of 8 cm thickness and the inner plaster of
1.5 cm thickness with a U-value equal to 0.439 W/m2 K. The outer wall is a five
layer wall with the following materials: 1.5 cm plaster, 12 cm brick, 6 cm insula-
tion, 12 cm brick and 1.5 cm plaster with a U-value equal to 0.510 W/m2 K.
356 E. Bellos et al.
The ground contains the heating pipes inside the concrete layer and also has
insulation layer of 8 cm with U-Value about 0.314 W/m2 K.
For thermal comfort conditions, the daily temperature should be greater than
22 �C which means that a control system is used to determine the operation of the heating system. The minimum theoretical heating energy to cover this thermal
comfort condition is about 5020 kWh which was calculated by TRNSYS.
Active Layer (Underfloor Heating System)
The underfloor heating system is inserted in the ground of the building as an active
layer which exchanges data with other system components. The hot water flows
inside the tubes giving heating in the house and let the house with a lower
temperature. There is a thermostat which controls when there is heating need.
Figure 28.1 shows the TRNSYS environment which related with the underfloor
heating.
In this window the parameters of the active layer are determined in order to take
data for the hot water temperature and mass flow rate. Also, the minimum desired
inlet mass flow rate is given which is a very important parameter. This parameter
determines the segmentation of the area for the underfloor system. In this figure, the
specific mass flow rate of 3 kg/h m2 separates the area in four segments as it is
shown in Fig. 28.2. By changing this parameter, the area segmentation changes in
order to improve the system operation.
Table 28.3 gives the main parameters for the tubes of the heating system.
These values are the default TRNSYS values and are realistic according the
bibliography for building cases.
Table 28.1 Building parameters
Parameter Value Parameter Value
City Athens Specific gains 14 W/m2 K
Area 100 m2 Occupants density 0.1 person/m2
Height 3 m Specific light 10 W/m2
East glass 3 m2 Infiltration rate 1 change per hour
West glass 3 m2 Thermal capacitance 720 kJ/K
South glass 6 m2 hout 17.8 W/m 2 K
Shading coefficient 70% hin 3.1 W/m 2 K
Table 28.2 Properties of structural materials
Material k (W/m K) Cp (kJ/kg K) ρ (kg/m3) Brick 0.89 1.0 1800
Plaster 1.39 1.0 2000
Insulation 0.04 0.8 40
Concrete 7.10 0.8 2400
28 Modelling of a Solar Assisted Floor Heating System with TRNSYS 357
Fig. 28.1 TRNSYS active layer environment
Fig. 28.2 Floor segmentation with four different loops. The red line shows the hot water inlet flow and the blue line the return flow (Color figure online)
358 E. Bellos et al.
Mathematical Equations
The basic equations which describe the analyzed case are presented and explained
in this section. These equations are related with the solar collectors, the system
energy balance, the auxiliary heater and the building.
Building
The thermal resistance of the structural components is given from the next
equation:
R ¼ XN j¼1
L
k
� � j
þ 1 hin
þ 1 hout
ð28:1Þ
U ¼ 1 R
ð28:2Þ
where N is the number of layers of every structural component.
The heating load of the house is approximately given from the next equation
(28.3):
Qheating ¼ ms � Cp � T Bin � T Bout � � ð28:3Þ
where Cp is the specific heat capacity of water which was taken 4.19 kJ/kg K.
Flat Plate Collectors
The following equations are the basic equations for the useful collector energy and
for the collector efficiency.
Qu ¼ _mc � Cp � Tf ,o � Tf , i � � ð28:4Þ
Table 28.3 Properties of piping
Parameter Value
Pipe wall conductivity 0.35 W/m K
Pipe spacing 0.2 m
Pipe outside diameter 2 cm
Pipe wall thickness 2 mm
Liquid specific thermal capacity 4.19 kJ/kg K
28 Modelling of a Solar Assisted Floor Heating System with TRNSYS 359
η ¼ Qu Ac � GT ð28:5Þ
η ¼ FR ταð Þ � FRUL � Tf , i � Tamb GT
� � ð28:6Þ
Storage Tank
A simple energy balance in the storage tank is given below:
Qsource ¼ Qload þ Qloss ð28:7Þ
where source is the collectors, load the heat to the building and loss the radiant
losses to the environment.
Auxiliary Heater
The auxiliary heater operation is described from Eqs. (28.8) and (28.9):
QA:H: � QA:H:,max ð28:8Þ QA:H: ¼ min QA:H:,max,ms � Cp � Tset � Tlð Þ
� � ð28:9Þ
Other System Parameters
The next equation is a simple energy balance in the total system
Qu þ QA:H: � Qloss � Qheating ð28:10Þ
The following equation gives the solar cover of the system for heating need:
f ¼ 1� QA:H: Qheating
ð28:11Þ
The last equation shows the temperature set value in the mixer and in the
auxiliary heater. This is a function of the ambient temperature and gives acceptable
results. It was able to use a constant value of 40–45 �C, but this relation leads the system to use warmer water in the colder days which covers better the heating
loads.
Tset ¼ 50� Tamb 2
ð28:12Þ
360 E. Bellos et al.
System Description
The total system is simulated with TRNSYS which is able to make a dynamic
simulation. The months from November to April are simulated because in these
months there is heating need according the simulation results. The heating is given
from the solar collectors and from an auxiliary heater and the goal is to maximize
the solar cover in order reduce the operation cost of this system. Figure 28.3 shows
the analyzed system.
The red line shows the hot water which flows in the flat plate collectors and is
stored in the tank, while the blue line shows the water stream which flows in the
underfloor heating system. More specifically, the water leaves the storage tank and
goes to auxiliary heater. After the heater this flow goes into the house and when it
leaves the house piping it returns to the storage tank. In the case that the temperature
of the water which goes to the house is great, this is mixed with the return of the
house in order to reduce the inlet temperature and to protect the piping from
destroying. It is important to say that there are different thermostats which control
the system and the heater operation in order to reduce the heater energy usage.
Controller 1
Controller 2 Heater
Mixer
Tempering Valve
Pump-2 Storage Tank
Collectors
Pump Building
Q
Fig. 28.3 Basic components of the analyzed system
28 Modelling of a Solar Assisted Floor Heating System with TRNSYS 361
In this system is important to determine the optimum values for critical param-
eters in order minimize the auxiliary heater energy for the winter period. The
collecting area, the storage tank volume, the maximum heater power, the controller
strategy and the area segmentation are the parameters that are examined in this
study.
Table 28.4 gives the values of the system parameters. In the case that one
parameter is analyzed for different values, these are also given:
Results
In this paragraph the results of the simulation of the system are presented. The
diagrams show the system performance for different values of important parame-
ters. By evaluating these data is able to determine the optimum system which leads
to a feasible situation. The goal of the optimization is to minimize the auxiliary
heater energy by using a realistic collecting area. It is important to state that the
storage tank volume influences on the results, so in every case the suitable table is
used in order to have an optimal system.
Area Segmentation and Heater Control Strategy
First of all, is important to determine the way that the underfloor system should be
separated in parts in order to heat the building efficiently. So, the floor area is either
separated in four segments, in two segments and in one segment and the three cases
are compared. Simultaneously, the control of the thermostat temperature is ana-
lyzed; because of this is a crucial parameter for the heater energy. By reducing this
temperature, the heater energy is dramatically diminished. It is important to state
that the heater power is selected to be at 6 kW, which is close to maximum heating
load of the building (Figs. 28.4, 28.5, and 28.6).
From the above diagrams, it is obvious that the thermostat temperature of heater
is very important parameter. By using 21 �C as the critical temperature, the energy is low and the thermal comfort conditions are in preferable limits (Fig. 28.7). If the
Table 28.4 System parameters
Collector Parameters Value Other Parameters Value
FR(τα) 0.8 Heating system water flow rate 1500 kg/h FRUL 3.61 Maximum system temperature 98
�C Slope angle 45� Tank losses coefficient 0.7 W/m2 K Azimuth 0� Tank volume 1.5–6 m3
Operation hours 9:00–17:00 Heater thermostat temperature 20–22 �C Collector water mass flow rate 2000 kg/h Heater power 0–12 kW
362 E. Bellos et al.
thermostat was set at 22 �C, which is also the set temperature for the underfloor heating system, then the energy is about four times greater which leads to a high
energy consumption and is not sustainable.
It is obvious that the temperature is over 22 �C for the greater part of the winter and only a few times is lower than this limit. The next diagram (Fig. 28.8) compares
the three heating systems.
It is obvious that the segmentation of four parts gives the better results because
the heat transfer from the piping to the indoor air becomes easily. In the following
analysis, this case is selected as the optimum, but also the case of the two segments
gives similar results. Finally it is important to stat that with only one loop the
auxiliary energy is about five times greater which to an unaffordable solution.
The optimum collecting area is 30 m2 according the Fig. 28.7. More specifically,
a greater collecting area means lower heater energy, but after the 30 m2, the
0 0
1000
2000
3000
4000
5000
6000
7000
8000
9000
20 40 60 Ac(m2)
E au
x( kW
h )
80 100
Tq=20
Tq=20,5
Tq=21
Tq=21,5
Tq=22
Fig. 28.4 Heater energy for one underfloor loop (area segmentation¼ 1 part)
0
500
1000
1500
2000
2500
3000
3500
4000
4500
E au
x( kW
h )
0 20 40 60
Ac(m2)
80 100
Tq=20
Tq=20,5
Tq=21
Tq=21,5
Tq=22
Fig. 28.5 Heater energy for two underfloor loops (area segmentation¼ 2 parts)
28 Modelling of a Solar Assisted Floor Heating System with TRNSYS 363
reduction in the heating energy is very low. Table 28.5 gives the optimum tank
volume for every collecting area and the heater energy consumption for every case.
Heater Power Analyses
In this section a parametric analysis is presented in order to predict the value of the
auxiliary heater power. Figure 28.9 shows how the mean value and the minimum
value of the indoor temperature changes with different values of heater power.
Tq=20
Tq=20,5
Tq=21
Tq=21,5
Tq=22
0
500
1000
1500
2000
2500
3000
3500
4000
4500 E
au x(
kW h
)
0 20 40 60
Ac(m2)
80 100
Fig. 28.6 Heater energy for four underfloor loops (area segmentation¼ 4 parts)
30.00
27.00
24.00
T em
p er
at u
re s
[d eg
C ]
21.00
18.00
15.00
30.00
27.60
25.20
22.80
20.40
Simulation Time-11640.00[hr]
18.00
7. 30
+ 03∋
8. 02
+ 03∋
8. 38
+ 03∋
8. 74
+ 03∋
9. 11
+ 03∋
9. 47
+ 03∋
9. 83
+ 03∋
1. 01
+ 04∋
1. 05
+ 04∋
1. 09
+ 04∋
1. 12
+ 04∋
1. 16
+ 04∋
7. 66
+ 03∋
Fig. 28.7 Distribution of the indoor temperature for all over the winter period, from November to April. The thermostat set temperature of the heater is 21 �C and the floor heating system is consisted of four segments
364 E. Bellos et al.
1seg
2seg
4seg
0
1000
2000
3000
4000
5000
6000
E au
x( kW
h )
0 20 40 60
Ac(m2)
80 100
Fig. 28.8 Comparison of the three heating system with 1 (blue), 2 (red) and 4 (green) area segmentation (Color figure online)
Table 28.5 Results of the 4 segmentation heating
system
Ac (m 2) V (m3) 1seg 2seg 4seg f (%) for 4seg
10 1.50 5706 2569 1940 61.35
20 2.00 4159 1171 871 82.65
30 2.50 3190 689 533 89.38
40 2.50 2347 557 404 91.95
50 2.75 1886 410 314 93.75
60 4.00 1879 261 204 95.94
70 5.00 1882 217 182 96.37
80 6.00 1906 193 164 96.73
Tm Tmin
0 2 4 86 Qaux (kW)
10 12
T (°
C )
23
22
21
20
19
18
Fig. 28.9 Mean (blue line) and minimum (red line) indoor temperature for different values of heater power
28 Modelling of a Solar Assisted Floor Heating System with TRNSYS 365
From this diagram it is obvious that the mean temperature is not changes a lot for
different heating power, but the minimum temperature is influenced a lot. More
specifically, a heater of 6 or 9 kW is suitable by giving the desired indoor
conditions.
Figure 28.10 presents the operation time of the heating system and of the heater.
These times are different, because the auxiliary heater operates when there is great
need for heating.
The Solar Stand-Alone Underfloor Heating System
In this section the case that the solar collectors give all the energy to the heating
system is analyzed. It is very important to determine if this case is feasible because
the energy consumption from electricity or fuel is zero (Fig. 28.11).
heating
auxilliary
0 2 4 86
Qaux (kW)
10 12
H o
u rs
1200
1000
800
600
400
200
0
Fig. 28.10 Operation time of the heating system (blue line) and of the auxiliary heater (red line) (Color figure online)
Tm
Tmin
T (°
C )
25
23
21
19
17
15
13 0 20 40 8060
Ac(m2)
100
Fig. 28.11 Mean (blue line) and minimum (red line) indoor temperature for different values of collecting area in the case without heater (Color figure online)
366 E. Bellos et al.
In order to have an acceptable minimum temperature, 50 m2 of flat plate
collectors should be used. In this case the minimum temperature of the winter
period is about 18.70 �C. The mean temperature is not influenced a lot after the 20 m2 fact that shows a low collecting area is able to cover a great part of the
heating load.
Conclusions
The main conclusions of this study are the following:
• It is able to heat a building efficiently with an underfloor heating system. By
using 30 m2 flat plate selective collectors is able to cover the 90% of the heating
load. The optimum volume of the storage tank in this case is about 2.5 m3.
• A for segmentation of the building area gives better results than the other cases.
Especially, in the case of one underfloor loop, the energy consumption is five
times greater than the four loops case.
• By using two thermostats, one for heating system and one for auxiliary heater, is
able the reduction of the energy consumption. More specifically the heating
system thermostat is set to 22 �C and the heater to 21 �C which lead to a great indoor temperature profile and to a 75% auxiliary heating energy reduction.
Simultaneously, the operations hours of the heater are about the 10% of the total
operation hours of the underfloor heating system. This shows that the heater
operates in moments with high heating need.
• The optimum value for the auxiliary heater power is 6 kW, which is close to the
maximum heating load of the building. This means that the heater should be able
to cover the total building loads in the moments which solar energy is
unsufficient.
• An underfloor heating system is able to operate without auxiliary energy by
using more collecting area. More specifically, 50 m2 are able to keep the thermal
comfort condition in high levels inside the house. This leads to zero consumption
which is a feasible solution for new buildings.
• The ratio of collecting are to building area is about 1–3 for the case with heater
and 1–2 for the case with only solar collectors. For the heater case, other studies
(Zhai et al. 2009) give similar results which validate this analysis.
Nomenclature
Ac Collecting area, m 2
Cp Specific heat capacity, J/kg K
E Energy, kWh
f Solar cover
FR Heat removal factor
28 Modelling of a Solar Assisted Floor Heating System with TRNSYS 367
GT Solar titled radiation, W/m 2
h Heat transfer coefficient, W/m2 K
k Thermal conduction, W/m K
L Layer length, m
m Mass flow rate, kg/s
Q Heat flux, W
R Thermal resistance, mK/W
T Temperature, �C U Thermal transmittance, W/m2 K
UL Collector losses coefficient, W/m 2 K
V Storage tank volume, m3
Greek Letters
η Collector efficiency ρ Density, kg/m3
(τα) Transmittance–absorptance product
Subscripts
A.H. Auxiliary heater
amb Ambient
aux Auxiliary
c Collector
f,i Fluid inlet
f,o Fluid outlet
in Indoor
l Load
min Minimum
max Maximum
out Outdoor
q Heater thermostat
s Heating system
u Useful
Superscripts
B Building
References
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Asimakopoulos, D. A., Santamouris, M., Farrou, I., Laskari, M., Saliari, M., Zanis, G.,
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Giannakopoulos, C. (2012). Modelling the energy demand projection of the building sector
in Greece in the 21st century. Energy and Buildings, 49(June), 488–498. Athienitis, A. K. (1994). Numerical model of floor heating system. ASHRAE Transactions, 100,
1024–1030.
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collectors or solar ponds. Applied Energy, 77, 107–117. David, J. (1984). Under floor air conditioning. Journal of the Charted Institution of Building
Services, 6, 29–34. European Environment Agency. (2010). Consumption and the environment—state and outlook.
Fantidis, J. G., Bandekas, D. V., Potolias, C., & Vordos, N. (2013). Cost of PV electricity—Case
study of Greece. Solar Energy, 91, 120–130. Gao, R., Li, A., Zhang, O., & Zhang, H. (2011). Comparison of indoor air temperatures of different
under-floor heating pipe layouts. Energy Conversion and Management, 52, 1295–1304. Ghali, K. (2007). Economic viability of underfloor heating system: A case study in Beirut climate.
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system consisting of radiators and floor heating. Energy and Buildings, 41, 470–479. Inard, C., Meslem, A., & Depecker, P. (1998). Energy consumption and thermal comfort in
dwelling-cells: A zonal-model approach. Building and Environment, 33(5), 279–291. Kilkis, B. I., Sager, S. S., & Uludag, M. (1994). A simplified model for radiant heating and cooling
panels. Simulation Practice and Theory, 2, 61–76. Kouremenos, D. A., Antonopoulos, K. A., & Domazakis, E. S. (1985). Solar radiation correlations
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28 Modelling of a Solar Assisted Floor Heating System with TRNSYS 369
Part VII
Energy Technologies and Their Effect on Global Warming
Bioenergy–Biofuel Technologies
Novel biofuels
Chapter 29
Biogas Production from Napier Grass at Various Cutting Intervals
Nusara Sinbuathong, Yuwadee Sangsil, and Suriya Sawanon
Introduction
Anaerobic digestion can be applied to convert biodegradable wastes such as plant
biomass, energy crops and grass to produce biogas (Seppala et al. 2009). Napier
grass (Pennisetum purpureum) is known as elephant grass and is a perennial grass with high biomass. Normally it is used for cattle feeds and is cultivated as forage.
The grass has the advantage of being familiar to farmers and suitable for harvesting
and storing with existing methods and machinery. It grows fast and is highly
adaptive, hence is suitable to be grown on marginal lands. Climate, soil fertility,
cutting interval, variety and management practices may affect on chemical com-
position and digestibility of Napier grass. It is interesting to digest the grass in order
to produce biogas. However, grass is not a mature feedstock for anaerobic digestion
facilities due to its complex structure; lignin and cellulose are resistant to hydrolysis
reaction and microbial actions (Nizami et al. 2009). Previous studies about biolog-
ical pretreatment were mainly focused on use of pure cultures, such as anaerobic
bacteria, fungi, and actinomycetes, which were able to degrade lignocellulose
(Desvaux et al. 2000; Xu and Goodell 2001). However, pure cultures of
N. Sinbuathong (*) Scientific Equipment and Research Division, Kasetsart University Research and Development
Institute (KURDI), Kasetsart University, Bangkok 10900, Thailand
e-mail: [email protected]
Y. Sangsil
Department of Environmental Engineering, Faculty of Engineering, Kasetsart University,
Bangkok 10900, Thailand
e-mail: [email protected]
S. Sawanon
Department of Animal Science, Faculty of Agriculture at Kamphaeng Saen, Kasetsart
University, Kamphaeng Saen Campus, Nakhon Pathom 73140, Thailand
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_29
375
microorganisms are difficult to maintain in an open system, and often require long
pretreatment time. In fact, it has been approved that the complete decomposition of
lignocellulose requires the combined actions of various microorganisms (Slater and
Lovatt 1984). Several studies have demonstrated the efficiency of constructed
microbial consortia for the rapid degradation of lignocellulose (Haruta
et al. 2002; Wongwilaiwalin et al. 2010)
Cows rely on rumen microorganisms to convert feed components into useable
source of energy and protein. Rumen microorganisms ferment carbohydrates to
make volatiles fatty acids and grasses. The rate of digestion of feeds depends on the
quality and composition of feed. It is affected by the number and type of microor-
ganism, pH in the rumen and nutrients. These factors limit the growth of the
microorganisms.
Hence, two phase anaerobic digestion with mixed microorganisms may enhance
the efficiency of digestion. In this study, a lab scale, two-stage anaerobic digestion
system was used for digesting Napier grass for biogas production. In the first stage,
the acidogenic condition provides acidic surroundings to digest the recalcitrant
structure and enhances digestibility. The aim of the current study is to digest Napier
grass of different cutting intervals by using mixed ruminal microorganisms from
cow rumen in semi-continuous two-stage reactor in order to minimize inhibition of
the hydrolysis phase by low pH and accumulation of inhibitors. The test was
performed under optimum hydraulic retention time (HRT). Annual CH4 yield per
hectare obtained from Napier grass at various cutting interval was investigated.
Materials and Method
Two-Stage Anaerobic Operation
Two separate bioreactors were designed specifically for the acidogenic and
methanogenic anaerobic digestion. Four set of bioreactors was constructed with a
PET plastic reactors with a working volume of 4 L and 5 L for acidogenic and
methanogenic stage respectively (Fig. 29.1). The reactor was connected to a gas
collection system, which was based on water displacement by the exiting gases
(Fig. 29.1).
Fresh Napier grass (Pakchong 1) of approximately 30 kg. was cut at various
cutting intervals (30, 45, 60 and 90 days) and then bagged and stored in a cold room.
The grass was chopped to a size of 1 cm and ground to a size of approximately
2 mm. The stems and leaves were blended thoroughly into a harmonious whole.
The ground Napier grass was stored in a refrigerator at 4 �C before use. Without pretreatment and supplement with nutrient addition, the grass was prepared with tap
376 N. Sinbuathong et al.
water at a ratio of 1:5 by weight to create a slurry. Napier grass was used as a sole
carbon source. Four systems were developed by varying the cutting intervals of the
Napier grass in the acidogenic and methanogenic reactors. A slurry of grass at
various cutting intervals at a 1:5 grass-water ratio was added to the acidogenic
reactor at a rate of 0.5 L/day for 8 days. This acidogenic reactor was operated for
2 days in batch mode before feeding once daily with the slurry semicontinuously in
an upflow mode at a feed rate of 200 mL/day in each set of reactors, giving rise to
HRT of 20 days for acidogenic and 25 days for methanogenic reactor stage. Mixed
ruminal microorganisms of approximately 10 g mixed liquor volatile suspended
solid/L were used as inoculum. The reactors were operated at ambient temperature
of 30þ 1 �C. pH was adjusted to be 7.5 for all methanogenic reactors at the start-up period. The reactors functioned without pH control during an operation period. In
this study, two-stage anaerobic digestion of Napier grass was investigated by
controlling the HRT of the two digesters. The start-up and operating period were
approximately 55 days. The study was carried out using steady-state conditions.
Slurry in
Water out
Water in
Slurry out
Gas in 3
2
Gas sampling point
Fig. 29.1 Two-stage anaerobic reactor with gas collection system
29 Biogas Production from Napier Grass at Various Cutting Intervals 377
Analysis of Materials
Napier grass (Pakchong 1) used in the test was cultivated in well fertilized field at
Khamphaeng Saen, Nakorn Pathom Province, Thailand. The grass at various
cutting intervals was measured for height and analysed for major (N, P, K) and
minor elements (K, Ca, Mg, Cu, Fe). These elements are nutrients in the digestion.
Nitrogen (N) was determined by the Kjeldahl methods by digesting samples to
convert organic N to NH4 þ-N and determining NH4
þ-N in the digest. Total phos- phorous (P) was determined by digesting samples with sulphuric acid and analysed
by the Vanadomolybdophosphoric Acid Colourimetric method. Methane (CH4)
was determined by employing a gas chromatograph (Model GC 14B, Shimadzu,
Japan) equipped with a thermal conductivity detector (TCD) and a molecular sieve
13X column. The temperatures of the injector, column and TCD detector were
60, 40 and 70 �C, respectively. Argon was used as the carrier gas. The slurry fed to reactors and the digested slurry from the methanogenic reactor were analysed for
Chemical Oxygen Demand (COD), Total Volatile Solids (TVS), Total Solids
(TS) and pH according to the procedures of the Standard Methods (APHA and
AWWA 2005). Organic degradation efficiency (in terms of COD and TVS) and
CH4 production from the system obtained from the Napier grass at various cutting
intervals were used as indicators of reactor performance. All experiments were
conducted in duplicate and the results are calculated using the mean of the exper-
imental values.
Results
The grass yield from the field is as shown in Fig. 29.2. A slurry of Napier grass at a
1:5 grass-water ratio was analysed for COD, TS, TVS also for the major and minor
biological nutrients (Table 29.1). The composition and quantity of Napier grass
varied on the cutting intervals (Table 29.1), thus impacts on the biogas production.
During sample preparation, it was noticeable that the higher age grass (higher
cutting interval) had more stems and had fewer leaves than the lower age. Thus, the
proportion of leaf to stem of the higher age grass was less comparing with that of the
lower age grass. Crowder and Chheda (1995) had also reported this. Napier grass is
easy in propagation and management, thus it has high yield. The data from field
found that when the cutting interval increased, the grass yield increased (Fig. 29.2).
The grass yield obtained from the Napier grass at the cutting interval of 45, 60 and
90 days was double, quadruple and penta times of that from 30 days (Fig. 29.2).
On the other hand, at higher cutting intervals, the major and minor elements by dry
weight decreased (Table 29.1). This is in accordance with the data reported by
Crowder and Chheda 1995. Nutrients are crucial that limit microbial growth in
anaerobic digestion. If the nutrients are in short supply, microbial growth is
retarded, and so is the digestibility of feed (Moran 2005).
378 N. Sinbuathong et al.
The grass was fairly high in organic substrate (Table 29.2) and therefore had
good potential for biogas generation. The COD content in the slurry of Napier grass
(Napier grass:water¼ 1:5) at the cutting intervals of 30, 45, 60 and 90 days was 19.32, 24.00, 27.32 and 30.87 g/L and TKN of the grass was 661, 343, 300, 251 mg/
L as N respectively; thus, the C:N ratio was 100:3.42, 100:1.43, 100:1.10 and
100:0.81 respectively. Microorganisms that decompose organic matter use carbon
as a source of energy and nitrogen for building cell structure. The recommended
COD:N of organic substrate is 100:2.5 in order to assimilate the microorganisms in
Fig. 29.2 Annual Napier grass yield at various
cutting intervals
Table 29.1 Characteristics of the slurry of Napier grass (Napier grass:water¼ 1:5) fed to reactors at various cutting intervals
Parameters Napier grass at various cutting interval (days)
30 45 60 90
Chemical oxygen
demand (COD, g/L)
19.32 24.00 27.32 30.87
Total solids (TS, g/L) 17.73 24.00 26.94 32.30
Total volatile solids
(TVS, g/L)
14.43 18.42 20.88 29.18
pH 5.86 7.22 6.92 6.17
Nitrogen (TKN, mg/L as
N)
661 343 300 251
Phosphorus (PO4 3�,
mg/L as P)
2.74 1.84 2.14 3.11
Calcium (Ca, mg/L) 50.19 32.45 24.11 35.87
Copper (Cu, mg/L) 0.15 0.07 0.07 0.02
Iron (Fe, mg/L) 14.47 2.55 2.99 4.51
Potassium (K, mg/L) 1334 864 972 1017
Magnesium (Mg, mg/L) 34.79 19.79 39.50 35.47
COD:N 100:3.42 100:1.43 100:1.10 100:0.81
COD:N:P 100:3.42:0.014 100:1.43:0.008 100:1.10:0.008 100:0.81:0.010
29 Biogas Production from Napier Grass at Various Cutting Intervals 379
anaerobic digestion (Anderson et al. 2003). If the COD:N ratio is too high,
decomposition slows because the nitrogen is used up and some microorganisms
die. On the other hand, if the COD:N ratio is too low, microorganisms make full use
of the available carbon and get rid of the excess nitrogen as ammonia. Ammonia
caused toxic to microorganisms in the system (Hartmann and Ahring 2006). In this
study, the ratio of COD:N:P was 100:3.42:0.014, 100:1.43:0.008, 100:1.10:0.008,
100:0.810:010. These caused differences in the amount of carbon source and
nutrients fed to reactors.
Table 29.2 Summary of two-stage anaerobic digestion of the Napier grass as a sole carbon source at various cutting intervals
Parameters
Napier grass at various cutting
intervals (days)
30 45 60 90
Reactor volume for each acidogenic, methanogenic reactor
(L)
4, 5 4, 5 4, 5 4, 5
Daily feed (mL/day) 200 200 200 200
HRT for each acidogenic, methanogenic reactor (day) 20,
25
20,
25
20,
25
20,
25
Initial MLVSS (g/L) 10.0 10.0 10.0 10.0
Initial pH of substrate solution 5.86 7.22 6.92 6.17
Initial COD (g/L) 19.32 24.00 27.32 30.87
Initial TS (g/L) 17.73 24.00 26.94 32.30
Initial TVS (g/L) 14.43 18.42 20.88 29.18
OLR (kgCOD/m3.day) 0.97 1.20 1.37 1.54
OLR (kgTVS/m3.day) 0.72 0.92 1.04 1.46
CH4 produced at steady state
(mL at STP/day)
568 610 561 480
Average CH4 (%) 41.34 43.51 42.99 39.43
COD at steady state (g/L) 5.32 6.04 6.60 7.69
COD degradation efficiency (%) 72.46 74.82 75.84 75.88
TVS at steady state (g/L) 5.21 6.09 6.62 7.50
TVS degradation efficiency (%) 63.88 66.94 68.30 74.30
CH4 yield (L at STP/kgCOD added) 147 127 103 78
CH4 yield (L at STP/kgTS added) 160 127 104 74
CH4 yield (L at STP/kgTVS added) 197 166 134 82
Napier grass (DW) for pure CH4 1 m 3 (kg) 6.25 7.87 9.62 13.51
CH4 yield per area (m 3/ha/year) 2700 4763 6500 6013
Average pH of acidogenic reactor at steady state 5.20 5.24 5.35 5.35
Average pH of methanogenic reactor at steady state 7.25 7.20 7.18 7.10
380 N. Sinbuathong et al.
Biogas Production
At steady-state conditions, total biogas production and the performance of digestion
were reported. In this study, the results are reported for 25–55 days of digestion
period. The amount of CH4 production from the reactors are shown in Fig. 29.3 and
the average CH4 content are shown in Table 29.2.
Differences in the amount of CH4 production (Fig. 29.3) by the Napier grass of
each cutting interval were observed. At steady-state condition, the average daily
CH4 produced from the Napier grass at the cutting interval of 45 days was 605 mL
at STP/day and that from the cutting interval of 30 and 60 days was comparable and
was recorded at 570 mL at STP/day while that from the cutting interval of 90 days
was 480 mL at STP/day (Fig. 29.3). However, the key parameter that makes more
sense to use to consider the appropriate cutting interval is the annual CH4 yield per
area of cultivation, which is calculated by using the CH4 gas produced and the
Napier grass added to reactors including the mass of the grass yield obtained from
field.
Organic Substrate Degradation
The initial COD, TS, TVS and other parameters of the slurry of Napier grass
(Napier grass: water¼ 1:5) are summarised in Table 29.2. The COD and TVS of the slurry of Napier grass at the higher cutting interval was higher than that of the
lower (Table 29.2). Ansah et al. (2010) also reported that the higher age grass had
higher stem and higher organic matter (OM), resulted in higher COD and TVS than
0 10
800
700
600
500
400
300
200
100
0
20 30
30 day 45 day 60 day 90 day
Time (days)
C H
, ( m
L a
t S
T P
/d ay
)
40 50 60
Fig. 29.3 Time course of CH4 production of Napier grass slurry at various cutting intervals
29 Biogas Production from Napier Grass at Various Cutting Intervals 381
that of the lower age grass. The steady-state COD and TVS obtained from the
various cutting intervals are as shown in Table 29.2. The COD and TVS removal
efficiency were over 70% and 60%, respectively for all reactors that contained a
slurry of Napier grass of all cutting intervals (Table 29.2).
CH4 Yield
CH4 yield is the amount of CH4 produced per kilogram of organic substrate added
to reactor. For CH4 production and based on the COD, TVS and TS added to
reactors at the steady-state conditions, CH4 yield obtained at various cutting
intervals are shown in Table 29.2, respectively. Differences in the CH4 yield by
the Napier grass of each cutting interval were obviously observed (Table 29.2). The
composition and quantity of Napier grass varied on the cutting intervals (Table 29.1)
impacts on the biogas production (Fig. 29.3). Hence, the CH4 yield was influenced
by the cutting interval of the grass and the grass yield. Napier grass at the cutting
interval of 30 days showed a maximum value of CH4 yield at 147 L at STP/kg of
COD added (197 L at STP/kg of TVS added or 160 L at STP/kg DW of Napier grass
added). CH4 yield obviously dropped when the cutting intervals increased
(Table 29.2). For Napier grass of higher cutting interval (Napier grass of
90 days), grass is composed of more stems and it is not a mature feedstock for
anaerobic digestion facilities due to its complex structure; lignin and cellulose are
resistant to hydrolysis and microbial actions.
The highest CH4 yield was observed from the Napier grass at the cutting interval
of 30 days. For the Napier grass of 30 days, the CH4 yield was 160 L at STP/kg of
dry Napier grass added to the reactor (Table 29.2), which indicated that 6.25 kg of
dry Napier grass is needed to produce 1 m3 of pure CH4. COD and TVS degradation
efficiency was 72% and 64%, respectively (Table 29.2). The average pH in the
acidogenic and methanogenic reactors was 5.20 and 7.25, respectively (Table 29.2).
For the Napier grass at the cutting intervals of 45, 60 and 90 days, the highest CH4 yield was observed at 127, 104 and 74 L at STP/kg of dry Napier grass added to the
reactor, respectively (Table 29.2). The higher the cutting interval, the lower the CH4 yield obtained. Although the higher age grass had more stems, however, the higher
age grass had the more fibre and lignin (lignocelluloses) which are nonbiode-
gradable organics. Hence, the higher age grass gave less CH4 yield during digestion
than the lower age grass.
382 N. Sinbuathong et al.
Annual CH4 Gas Produced per the Napier Grass Added to Reactors
For the digestion of Napier grass at the cutting intervals of 30, 45, 60, 90 day, the
CH4 yield was 160, 127, 104, 74 L at STP/kg of dry Napier grass added to the
reactor (Table 29.2), which indicated that 6.25, 7.87, 9.62, 13.51 kg of dry Napier
grass is needed to produce 1 m3 of pure CH4 (Fig. 29.4).
However, when considering the Napier grass yield from cultivation in the field
(the grass yield at the cutting intervals of 30, 45, 60 and 90 days was 16.88, 37.50,
62.50 and 81.25 tons dry weight/hectare/year as mentioned earlier), it was found
from calculation that the CH4 yield per area of cultivation which was obtained from
the Napier grass at the cutting interval of 30, 45, 60 and 90 was 2700, 4763, 6500
and 6013 m3/hectare/year (Fig. 29.5). The annually highest CH4 yield per area of
cultivation was obtained from the Napier grass at the cutting interval of 60 days
(Fig. 29.5).
The result of this study is in accordance with that reported by Ansah et al. (2010).
Ansah et al. (2010) reported that the lower age grass gives the higher CH4 yield than
the higher age grass due to its higher crude protein and fibre. From this study, even
though the Napier grass of the cutting interval of 30 days gave the highest CH4 yield
but it gave the lowest annual grass yield per area, resulting in least annual CH4 yield
per area.
Fig. 29.4 Napier grass at various cutting intervals to
produce 1 m3 of pure CH4
29 Biogas Production from Napier Grass at Various Cutting Intervals 383
Conclusions
Napier grass (Pakchong 1) at the cutting interval of 60 days gave the highest annual
CH4 yield per area of all various cutting intervals. By two-stage anaerobic digestion
using the Napier grass as the sole carbon source and mixed ruminal microorganisms
from cow as seed source, the CH4 yield obtained was 104 L at STP/kg of dry Napier
grass added to the reactor, which indicated that 9.62 kg of dry Napier grass is
needed to produce 1 m3 of pure CH4. The grass yield obtained from the field was
62.50 tons dry weight/hectare/year, resulting in the annual CH4 yield per area
obtained was 6500 m3/hectare/year.
Acknowledgement This research was supported by the Kasetsart University Research and Development Institute (KURDI), Kasetsart University, Bangkok, Thailand.
References
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Ansah, T., Osafo, E. L. K., & Hansen, H. H. (2010). Herbage yield and chemical composition of
four varieties of Napier (Pennisetum purpureum) grass harvested at three different days after planting. Agriculture and Biology Journal of North America, 1, 923–929.
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Crowder, L. V., & Chheda, H. R. (1995). Tropical grassland husbandry (1st ed.). NJ: Wiley. Desvaux, M., Guedon, E., & Petitdemange, H. (2000). Cellulose catabolism by Clostridium
cellulolyticum growing in batch culture on defined medium. Applied and Environmental Microbiology, 66, 2461–2470.
Fig. 29.5 Annual CH4 produced per hectare from
Napier grass at various
cutting intervals
384 N. Sinbuathong et al.
Hartmann, H., & Ahring, B. K. (2006). Strategies for the anaerobic digestion of the organic
fraction of municipal solid waste: An overview. Water Science and Technology, 53, 7–22. Haruta, S., Cui, Z., Huang, Z., Li, M., Ishii, M., & Igarashi, Y. (2002). Construction of a stable
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Moran, J. (2005). How the rumen work? Tropical dairy farming: Feeding Management for small dairy farmers in the humid tropics (pp. 41–49). Collingwood: Land Links Press.
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production of grass biomethane. Environmental Science and Technology, 43, 8496–8508. Seppala, M., Paavolla, T., Lehtomaki, A., & Rintala, J. (2009). Biogas production from boreal
herbaceous grass-specific methane yield and methane yield per hectare. Bioresource Technol- ogy, 100, 2952–2958.
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29 Biogas Production from Napier Grass at Various Cutting Intervals 385
Chapter 30
Sustainability Assessment of Fuels Production via Hydrotreating Waste Lipids and Co-processing Waste Lipids with Petroleum Fractions
Stella Bezergianni and Loukia P. Chrysikou
Introduction
Considering the depletion of fossil energy resources and the increased greenhouse
gas (GHG) emissions of the transportation sector, biofuels are being extensively
explored as renewable and sustainable energy sources (Demirbas 2009). The
transportation sector contributes around 15% to the global GHG emissions, while
according to the EU targets by 2020, 10% of fuels in the transportation sector
should be biofuels (Directive 2009/28/EC). In particular, biofuels are being pro-
moted as one of the most substantial substitutes of fossil fuels, accounting their
favorable environmental performance, especially if utilizing residual biomass as
feedstock (Gnansounou et al. 2009). FAME (Fatty Acid Methyl Esters) biodiesel
constitutes the most common biofuel mainly derived from energy crops, whereas
residual biomass can be utilized in minor percentages. For instance, waste cooking
oil (WCO) generated from frying and cooking with edible oils has been investigated
as feedstock for FAME biodiesel production through transesterification and ester-
ification processes. FAME biodiesel is used as a low-blend component in transport
fuels (up to 7% v/v) in Europe. However, FAME biodiesel cultivation processes
raised significant issues, such as food-versus fuel debate, land-use alteration ren-
dering the use of bio-based feedstocks imperative, aiming to address global
warming concerns, as well (Gnansounou et al. 2009). Catalytic hydroprocessing
is an alternative conversion process of lipid feedstocks (e.g. vegetable oils, animal
wastes/fats etc.) into bio-based diesel fuels and has been applied in industrial scale
for the production of hydrotreated vegetable oils (HVOs). More specifically, HVOs
S. Bezergianni (*) • L.P. Chrysikou Chemical Process & Energy Resources Institute (CPERI), Centre for Research & Technology
Hellas (CERTH), Thermi Thessaloniki, Greece
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_30
387
are produced from vegetable oils and/or grease by Universal Oil Products (UOP)
(product’s trade name green diesel) (Kalnes et al. 2009) and from vegetable oils and/or animal fats by NesteOil Corporation (product’s trade name NExBTL- acronym for “Next Generation Bio-to-Liquid) (Arvidsson et al. 2011).
WCO has been extensively explored as potential feedstock for renewable diesel
production via catalytic hydrotreatment in CPERI/CERTH (Bezergianni
et al. 2010a, b, 2011). The renewable diesel is a high quality fuel based on its
remarkable properties (Bezergianni and Dimitriadis 2013a). Nevertheless, the high
capital cost investment of hydroprocessing units of vegetable oils and/or animal fats
supports the exploration of co-hydroprocessing petroleum fractions with oils uti-
lizing existing refining facilities, since catalytic hydroprocessing units are available
in all petroleum refineries. Recently, co-hydroprocessing of petroleum fractions
with WCO was also examined in CPERI/CERTH, resulting in the production of a
new hybrid diesel. In particular, catalytic hydroprocessing of a heavy petroleum
fraction (heavy atmospheric gas oil, HAGO) with WCO (at a ratio 95/5% v/v) was
investigated towards the production of a hybrid diesel of increased sustainability
(Bezergianni and Dimitriadis 2013b; Bezergianni et al. 2014a, b). This new hybrid
diesel was evaluated as a blending component of fossil diesel (Bezergianni
et al. 2014b). In this field Garraı́n et al. (2014) studied the production of a renewable
diesel fuel from co-processing soybean vegetable oil (at variant ratios from 9 up to
13.8% v/v/) with conventional fossil fuel.
However, the environmental performance of the production processes involving
the exploitation of existing petroleum refining processes to convert vegetable oils to
renewable bio-based diesel fuels, receives also noticeable attention, accounting the
global necessity to mitigate the climate change and to promote sustainable tech-
nologies (Garraı́n et al. 2014). Life Cycle Assessment (LCA) is a commonly
applied powerful method for the global warming impact assessment of conven-
tional fuels and biofuels. LCA quantifies the environmental impacts of conven-
tional fuels and biofuels throughout their life-cycle stages, proposing concurrently
possible ways to reduce them. A noticeable amount of LCA studies related to fuels
is available in the literature, in order to identify potential sustainable fuels that
could contribute to the transportation sectors’ GHG emissions reduction (Pleanjai et al. 2009; Arvidsson et al. 2011; Kochaphum et al. 2012; Bezergianni et al. 2014c;
Garraı́n et al. 2014). Based on the large number of publications analyzing the life-
cycle of fuels and biofuels significant controversies arise, even for the same biofuel
type and conversion technology, mainly due to variant methodological assump-
tions, inventory data etc. An accurate assessment of a new biofuel technology
requires a comprehensive fuel-cycle analysis, commonly called Well-To-Wheel
(WTW) analysis, involving both the Well-To-Tank analysis (WTT), as well as the
Tank-To-Wheel analysis (TTW). The WTT approach covers the fuel’s production
chain while the TTW the vehicle’s operation. The majority of the LCA studies
separate the analysis in the WTT and TTW counterparts, whilst the WTT is
particularly appropriate if the purpose of the study is concerned with the fuel’s
production process (Malça and Freire 2011).
388 S. Bezergianni and L.P. Chrysikou
The goal of this study is to assess the environmental profile of the renewable
diesel and the hybrid diesel produced via WCO hydrotreatment and
co-hydroprocessing of petroleum fractions with WCO, respectively. In addition,
the environmental impacts of the renewable diesel’s blend (up to 7% v/v) with
fossil diesel were also investigated. A secondary goal of this study is to compare the
environmental performance of all aforementioned fuels with fossil diesel
(containing 7% v/v FAME biodiesel) in order to address the most sustainable
process and to verify the advantages of utilizing WCO as feedstock and its
prospective integration in the refinery. Aiming to establish a reliable comparison
basis of the aforementioned fuels production processes, WTT analysis was
conducted addressing their GHG intensity.
Methodology
The scope of the LCA study is to investigate the environmental impacts of
bio-based fuels produced via hydrotreating WCO and co-processing WCO with
petroleum fractions, and to compare their production processes GHG emissions
with fossil diesel, as well. The experimental procedure followed for the WCO
catalytic hydrotreatment has been previously described in detail (Bezergianni and
Dimitriadis 2013a), utilizing a large pilot plant scale hydroprocessing unit of
CPERI/CERTH. Likewise, the production process of the new hybrid diesel has
been described in authors’ previous work (Bezergianni et al. 2014b), exploiting data collected from the Hellenic Petroleum refinery in Thessaloniki as reported in
authors’ previous work (Bezergianni et al. 2014b). The experiments were carried out in a small-scale hydroprocessing plant of CPERI/CERTH, while the unit is
described extensively by Bezergianni and Dimitriadis (2013a). Apart from the real
experimental data collected for the LCA study, results reported by JRC (2014) were
also employed for comparison purposes referring to the fossil diesel’s and FAME
biodiesel’s production processes GHG intensity.
The fuels production processes examined in the study are shown in Figs. 30.1,
30.2, 30.3 and 30.4 depicting the system boundaries encompassed for each of the
examined fuels. Particularly, Fig. 30.1 presents the production process of the
renewable diesel via WCO catalytic hydrotreatment, including WCO collection
and transportation to the hydrotreating unit and the hydrotreatment process as well.
The production of the new hybrid diesel from co-hydroprocessing HAGO and
WCO in the refinery under consideration is shown in Fig. 30.2, involving the crude
oil extraction and transportation to the refinery, the refining of the crude oil for the
production of petroleum fractions (HAGO and light atmospheric gas oil-LAGO),
the co-processing HAGO with WCO (95/5% v/v), the hydrotreatment of LAGO
and finally the blending with FAME for the production of the new hybrid diesel (the
precise blending ratios are reported below). Figure 30.3 presents the production
chain of fossil diesel, encompassing the stages of crude oil extraction and trans-
portation to the refinery and the refining process based on previous studies (JRC
30 Sustainability Assessment of Fuels Production via Hydrotreating Waste Lipids. . . 389
2014). The final stage of the production process involves its blending with FAME
biodiesel (~7% v/v) as previously mentioned in the introduction. The FAME
biodiesel production chain considered is shown in Fig. 30.4 containing the energy
crops cultivation and the oil extraction from them and finally the transesterification
process, taking into consideration the transport processes as well. More details for
FAME biodiesel production process can be found on a previous thorough study
(JRC 2014).
WCO collection & transportation Hydrotreatment
WCO pretreatment Renewable diesel
Fig. 30.1 Production chain of the renewable diesel via WCO catalytic hydrotreatment
Crude oil extraction & transportation
Refining
WCO collection & transportation
HAGO
LAGO
HAGO/WCO hydrotreatment
LAGO hydrotreatment
FAME production & transportation
New hybrid diesel
Fig. 30.2 Production chain of the new hybrid diesel via co-hydroprocessing HAGO with WCO
Crude oil extraction & transportation Refining
FAME production & transportation
Fossil diesel
Fig. 30.3 Production chain of the fossil diesel
Energy crops cultivation &
transportation
Oil extraction & transportation
Transes- terification
FAME biodiesel
Fig. 30.4 Production chain of the FAME biodiesel
390 S. Bezergianni and L.P. Chrysikou
The functional unit was 1 MJ of the renewable diesel and the hybrid diesel. The
inventory data sources employed for each of the investigated fuels were reproduced
based on this functional unit. The impact category assessed in this study is the
global warming potential (GWP) expressed in CO2 equivalents (CO2 eq-), since
GHG emissions and energy use are of high interest in bio-based fuels LCA studies.
The CO2 eq-outlines the total effect of GHG emissions including related emissions
of CO2, CH4 and N2O. Emissions contributing to acidification and eutrophication
are also often considered as impact categories, yet in the present study were not
accounted, since WCO does not impose these emissions.
Inventory Data
This section includes the inventory data of the fuels production processes previ-
ously described.
Renewable Diesel
Real experimental data were collected from the production of the renewable diesel
via WCO catalytic hydrotreatment while data were derived from current literature
as well. The assumptions and considerations for the environmental evaluation of the
renewable diesel’s production process are listed below:
• the impacts associated to the collection and transportation stages of WCO are
negligible in comparison to the impacts of the hydrotreatment process, account-
ing also the short distances within the city limits.
• main energy supply systems considered were the electric power consumption
from the grid and steam generation. The inventory data referring to the energy
requirements of the hydrotreatment process (electricity and steam) and the
associated GHG emissions were adapted from literature data, considering the
production of a HVO using vegetable oils and/or animal fats (Nikander 2008).
• the GHG emissions of the H2 consumption in the hydrotreatment process have
been estimated based on data retrieved from the literature (Nikander 2008),
produced via natural gas steam reforming.
• construction and demolition phases were eliminated from this study, due to
deficiency of related GHG emissions data.
Table 30.1 gathers the main inventory data (inputs and outputs) for the produc-
tion of renewable diesel from WCO catalytic hydrotreatment, based on experimen-
tal data computed by previously evaluations (Nikander 2008).
At this point it should be underlined that the renewable diesel could be possibly
employed as a blending component to fossil diesel up to ~7% v/v, as HVOs.
Therefore the environmental profile of this blend was also addressed in order to
30 Sustainability Assessment of Fuels Production via Hydrotreating Waste Lipids. . . 391
determine the most sustainable fuel in terms of GHG intensity and the results are
presented below. Data for the GHG emissions of fossil diesel production process
were obtained from literature sources in view of a European context (JRC 2014).
Hybrid Diesel
The key inventory data for the new hybrid fuel production process for the quanti-
fication of the GHG emissions (e.g information on crude oil origin, typical catalytic
hydrotreatment operation conditions, electric power consumption, fuels used for
heat production, main input and output flows used during the production etc.) were
collected from the refinery of the Hellenic Petroleum in Thessaloniki. Secondary
data were taken from assessments previously undertaken (Nikander 2008;
Cetinkaya et al. 2012). For assessing the GHG emissions of the new hybrid diesel
profile GEMIS (Global Emission Model for Integrated Systems, Version 4.9) was
used. GEMIS is a life-cycle analysis program and database for energy, material, and
transport systems providing information for fuels, processes for electricity and
heat etc.
The primary considerations and assumptions of the LCA study are the following:
• the impacts associated with the collection and transportation of WCO to the
refinery were considered negligible, accounting short distances (within city
limits).
• the petroleum refineries are extremely complicated plants with combined and
sequenced processes and as a result the refinery process of the crude oil is often
handled as a “black box” and not partitioned into sub-processes. In this study, the
refining stage is also depicted as a “black box” and the energy consumption and
GHG emissions were allocated according to the final products distribution.
Figure 30.5 illustrates a generic flow diagram of the refinery studied. Briefly,
after crude’s oil refining process the treated petroleum fractions, HAGO and LAGO are further treated to hydrotreating units. In the HAGO hydrotreating
unit, HAGO with WCO (95/5% v/v ratio) are co-hydroprocessed for the pro-
duction of a new hydrotreated hybrid fuel. Then this fuel is mixed with
hydrotreated LAGO and with FAME biodiesel for the production of the new
Table 30.1 Inventory data for the production of
renewable diesel via WCO
catalytic hydrotreatment
Unit Input Output
WCO g/MJ 23 –
H2 g/MJ 1.268
Renewable diesel g/MJ – 20.41
Gas producta g/MJ – 1.587
Total liquid product g/MJ – 3.648
Energy MJ/MJ 0.002 –
Steam MJ/MJ 0.014 – aIncluding excess H2
392 S. Bezergianni and L.P. Chrysikou
hybrid diesel, based on the blending strategy of the refinery of the Hellenic
Petroleum in Thessaloniki. A detailed analysis of the blending followed is
presented in Fig. 30.6.
• data regarding the GHG emissions of the fossil diesel’s and FAME biodiesel’s
production processes were retrieved form scientific papers (JRC 2014) consid-
ering typical refining in the EU. Specifically, the GHG balances of FAME
biodiesel refer to farming emissions not taking account of any land use change
emissions.
• electricity used in the refinery is assumed to be taken from the local grid, while a
small quantity is produced internally by fuels combustion (fuel gas, fuel oil,
natural gas etc.). The GHG emissions from the electricity consumption were
calculated based on the Greek electricity grid mix. The combustion of carbon
containing fuels internally results in the formation of CO2 (very small amounts
of N2O and CH4 are also formed). The contribution of these emissions has been
taken into account in the refinery’s GHG emissions. The electricity power
consumption in the hydrotreatment unit of HAGO did not alter due to the
addition of WCO.
Refinery
Energy
Emissions Cultivation &
transesterification of vegetable oils
Fertilizers Pesticides
New hybrid diesel
Refinery
Emissions
Crude oil
Natural Gas
Energy
Water
Hydrotreatment Unit
HAGO
LAGO
Hydrotreated hybrid fuel
Hydrotreated light gasoilHydrotreatment
Unit
FAMEH2 Fuel gas
Emissions
Emissions
Energy
Fuel gas
H2
Water WCO
Energy
Fig. 30.5 Generic flow diagram of the refinery describing the production process of the new hybrid diesel via co-processing HAGO and WCO
New hybrid diesel
FAME biodiesel (2% v/v)
Hydrotreated mixture HAGO-WCO (49% v/v)
Hydrotreated LAGO(49% v/v)
Fig. 30.6 Blending ratios of the components for the production of the new hybrid diesel
30 Sustainability Assessment of Fuels Production via Hydrotreating Waste Lipids. . . 393
• in the examined production process of the hybrid diesel the H2 consumption of
the HAGO hydrotreating unit is increased by about 6.25%, as compared with
conventional HAGO hydrotreating, due to the addition of 5% v/v WCO. This
increase is expected, due to the more demanding WCO hydroconversion reac-
tions. The additional H2 required can be supplied without operating cost
increase, since in the examined refinery there is a surplus of H2 from the natural
gas steam reforming unit (Bezergianni et al. 2014b).
• the GHG emissions of H2 production process from natural gas steam reforming
were based on literature data (Cetinkaya et al. 2012).
• the GHG emissions of construction and decommissioning of all process steps as
well as the maintenance operations are not accounted, due to lack of detailed
related GHG emissions data.
The inventory data of the new hybrid diesel’s production process are detailed in
Tables 30.2 and 30.3.
Results and Discussion
Environmental Evaluation of the Renewable Diesel and the Hybrid Diesel
The inventory data previously presented were the basis for the calculation of the
GWP associated with the investigated fuels production processes. The results are
Table 30.2 Inventory data of the HAGO/WCO (95/5% v/v) hydrotreating unit for the production of the new hybrid diesel
Unit Inputs Outputs
HAGO m3/m3 hydrotreated hybrid fuel 0.986 –
WCO m3/m3 hydrotreated hybrid fuel 0.052 –
H2 m 3/m3 hydrotreated hybrid fuel 70.924 –
Electricity kWh/m3 hydrotreated hybrid fuel 15 –
Steam kg/m3 hydrotreated hybrid fuel 24 –
Fuel gas mmBtu/m3 hydrotreated hybrid fuel 0.238 –
Hydrotreated hybrid fuel m3/m3 hydrotreated hybrid fuel – 1
Table 30.3 Inventory data of the LAGO hydrotreating unit for the production of the new hybrid diesel
Unit Inputs Outputs
LAGO m3/m3 hydrotreated LAGO 1.04 –
H2 m 3/m3 hydrotreated LAGO 55 –
Electricity kWh/m3 hydrotreated LAGO 15 –
Steam kg/m3 hydrotreated LAGO 24 –
Fuel gas mmBtu/m3 hydrotreated LAGO 0.238 –
Hydrotreated LAGO m3/m3 hydrotreated LAGO – 1
394 S. Bezergianni and L.P. Chrysikou
given in Tables 30.4 and 30.5 for the renewable diesel and the hybrid diesel,
respectively. As it can be observed, the hybrid diesel emits lower GHG emissions
than the renewable diesel, indicative of its optimal environmental characteristics.
Since this study aims to compare the environmental impacts of the aforementioned
fuels among themselves and also relative blend of the renewable diesel with fossil
diesel and fossil diesel, further comparisons results are exhibited in the following
subsection.
The contribution of the process stages encompassed in each production chain
was accounted so as to identify the major parameters affecting the GHG emis-
sions and is depicted in Fig. 30.7. In the case of the renewable diesel, the H2 demands of the hydrotreating process arose as the main source of GHG emissions
(91.41%). This high contribution to the GWP was attributed to the increased H2
Table 30.4 GWP emissions of the renewable diesel
production process Process stage
Renewable diesel
g CO2 eq/MJ
% Contribution to
production process
WCO collection &
transportation
~0 ~0
Pretreatment
Energy 0.957 7.873
Hydrotreatment
Energy 0.088 0.724
H2 11.11 91.403
Total 12.15 100
Table 30.5 GWP emissions of the renewable diesel
production process Process stage
Hybrid diesel
g CO2 eq/MJ
% Contribution to
production process
Refinery
HAGO 3.640 39.052
LAGO 2.463 26.454
Hydrotreatment
HAGO/WCO
Energy 0.410 4.398
H2 0.736 7.896
Fuel gas 0.185 1.985
Hydrotreatment
LAGO
Energy 0.410 4.399
H2 0.572 6.137
Fuel gas 0.175 1.985
FAME 0.720 7.724
Total 9.321 100
30 Sustainability Assessment of Fuels Production via Hydrotreating Waste Lipids. . . 395
consumption required for the conversion of WCO to renewable diesel. Likewise,
the contribution of H2 production has also been identified as the core source of
GHG emissions in the production chain of HVOs from vegetable oils (Arvidsson
et al. 2011). As expected, the hybrid diesel from co-processing HAGO/WCO
mixtures showed a different contribution profile, since the emissions from the
refinery were found to be dominating (~65.4%, encompassing the stage of crude
oil extraction and transportation to the refinery), linked to crude oil refining for
the production of the petroleum fractions HAGO and LAGO. It should be noted
that the H2 requirements in the co-processing of HAGO/WCO mixtures were also
substantial (~7.896%), while FAME biodiesel was also a noticeable GHG emis-
sions source (~7.724%).
The GHG emissions of the hybrid diesel examined could be potentially further
reduced by energy efficiency improvements steps in the refinery, focusing more on
optimizing energy utilization. Improvement actions to minimize the H2 require-
ments in the co-processing of HAGO and WCO are also encouraged via incorpo-
rating H2 from renewable energy sources for instance solar energy. Based on
literature data the dominant contributor to the GWP of the fossil diesel’s production
process is the refining process (JRC 2014). Emissions from the cultivation stage
represent the highest GHG emissions source in the carbon footprint of a renewable
diesel fuel obtained from co-processing soybean vegetable oil with fossil diesel
(mainly emissions connected with nitrogen fertilizers) (Garraı́n et al. 2014). Like-
wise, cultivation processes were identified as key contributors to the GHG emis-
sions of HVOs production processes (Uusitalo et al. 2014).
0%
10%
20%
30%
40%
50%
60%
70%
80%
90%
100%
Renewable diesel Hybrid diesel
Energy H2 Refinery Hydrotreatment LAGO FAME Hydrotreatment HAGO/WCO
Fig. 30.7 Percentage contributions to the GWP of the renewable diesel and hybrid diesel
396 S. Bezergianni and L.P. Chrysikou
Comparison with Other Fuels
This section compares the GHG emissions of the bio-based renewable fuels pro-
duced via hydrotreating WCO and co-processing HAGO with WCO among them-
selves and to relative blends and also to conventional fossil diesel. The comparison
includes only the fuels production processes and in the case of fossil diesel and
FAME biodiesel literature data were retrieved (JRC 2014).
Table 30.6 contrasts the GHG emissions of the targeted fuels production pro-
cesses. As it is shown, the GWP of the new hybrid diesel was estimated as 9.321 g
CO2 eq/MJ, presenting a better environmental profile compared to the renewable
diesel and to the other fuels. This observation validates that the integration of a
bio-based feedstock in the refinery and its co-processing with petroleum fractions,
constitutes a favorable environmental production process over stand-alone biomass
conversion technologies from GHG intensity viewpoint. Furthermore, the environ-
mental superiority of the renewable diesel is also evident, while its blend (7% v/v)
with fossil diesel showed also a better environmental profile than fossil diesel
(containing 7% v/v FAME biodiesel). As a result, the blend of the renewable
diesel with fossil diesel constitutes an alternative to fossil diesel and conventional
bio-based counterparts. As regards to the fossil diesel (containing 7% v/v FAME
biodiesel) it entailed the highest GWP.
Furthermore, when comparing the renewable fuels with HVOs originating from
rapeseed, palm oil and jatropha (GHG emissions range from 20.97 to 57.57 g CO2 eq/MJ, Uusitalo et al. 2014) their sustainable environmental profile is further
validated. Although, it should be underlined that the comparison of life-cycle
studies is frequently ambiguous since a large number of publications present
sometimes contradictory results, due to variant methodological approaches and
assumptions, inventory data for key input parameters etc. The high variability of
the life-cycle results from the various assessments demonstrates the necessity to
appoint key issues used in all the studies (Malça and Freire 2011). Nevertheless, the
variability in the results presented in this study could be high and subject to various
details of all stages included in the investigated production chains.
Overall, the renewable fuels investigated in this study are environmental advan-
tageous than conventional fossil diesel in terms of GHG emissions, identifying the
utilization of WCO as a potential favorable bio-based feedstock. The integration of
WCO in the refinery for the production of fuels with high bio-content via
co-processing technology could be conducive to the global warming mitigation
contrasting to stand-alone biomass conversion technologies. These observations
Table 30.6 GWP emissions of the examined fuels production processes
Fuel type gCO2 eq/MJ
Renewable diesel (via WCO hydrotreating) 12.15
Renewable diesel’s blend (7% v/v) with fossil diesel 14.15
Hybrid diesel (via co-processing WCO with HAGO) 9.321
Fossil diesel (containing 7% v/v FAME biodiesel) 16.974
30 Sustainability Assessment of Fuels Production via Hydrotreating Waste Lipids. . . 397
could be guiding future actions towards the decarbonization of the transportation
sector and guarantee the environmental sustainability of the EU policy at this level.
According to the European legislation the Directive 2009/28/EC establishes
sustainability criteria for biofuels, setting minimum GHG saving limits. In detail,
the GHG emissions savings should be at least 35% for any biofuel. This specific
minimum limit shall be at least 50% by the year 2017 and 60% by 2018 for biofuels
and bioliquids. Therefore, the GHG emissions savings of the renewable fuels
examined were quantified and compared to those of fossil diesel. GHG emission
savings of 89.48, 86.28 and 84.03% were calculated for the hybrid diesel, the
renewable diesel and its blend with fossil diesel, respectively. In all cases the GHG
emission savings meet the sustainability criteria of the regulation for the 2017 and
2018 limits. The new hybrid diesel could be assigned as an alternative to fossil
diesel and be conducive to significant GHG emissions reductions. These results
further validate the environmental performance of renewable fuels derived from
residual biomass via the co-processing approach and the catalytic hydrotreatment
conversion technology.
Conclusions
LCA is a valuable method applied to evaluate the environmental burdens of
processes accounting the inputs and outputs on a life-cycle basis. Renewable diesel
via WCO catalytic hydrotreatment has been produced, while the co-processing of
petroleum fractions/WCO mixtures has been explored as an alternative approach to
integrate residual biomass in the refinery. This new hybrid diesel constitutes a
blending component of fossil diesel. The present study aims to provide the envi-
ronmental characterization of bio-based fuels production systems via hydrotreating
WCO and co-processing petroleum fractions with WCO utilizing existing refinery
infrastructure. A comparison of these fuels with fossil diesel (containing 7% v/v
FAME biodiesel) and the renewable diesel’s blend (7% v/v) with fossil diesel was
also conducted through a WTT analysis. In this respect, the LCA study was
performed by utilizing real experimental data and inventory data sources from
previous environmental studies in the field as well as GEMIS software. The new
hybrid diesel produced via co-processing HAGO/WCO (95/5% v/v) exhibited the
most favorable environmental performance, in terms of GHG emissions. The
renewable diesels’ production chain GHG emissions are also relatively low, whereas its blend with fossil diesel presents also environmental benefits compared
with fossil diesel, enforcing its usage as a blending component. The results also
showed that in the case of the renewable diesel the emissions for the hydrotreatment
process (H2 consumption) were the dominant contributors to the GWP of the
process. Furthermore, in the case of the hybrid diesel the emissions from the
refining processes contributed notably to its GWP, while the emissions of the
hydrotreatment unit of HAGO/WCO mixtures were also prominent. Improvements
actions targeted primarily to energy efficiency techniques in the refinery and to the
398 S. Bezergianni and L.P. Chrysikou
incorporation of H2 originating from RES could probably lead to further GHG
emissions from the hybrid diesel production chain. The GHG emission savings
calculated for the new hybrid diesel further promotes its optimal environmental
characteristics, validating that WCO constitutes a suitable feedstock for bio-based
fuels production from GHG emissions perspective. Based on these findings, it could
be inferred that the co-processing approach of petroleum fractions with WCO could
contribute to the production of sustainable and environmentally efficient fuels.
Supplementary to this observation, it may also be underlined that the integration
of residual biomass in the refinery via co-processing technology for the production
of bio-based fuels compatible with their fossil counterparts is preferable in terms of
GHG balance compared to stand-alone biomass conversion technologies. However,
future studies should also address thoroughly the issue of WCO availability in
Greece in the case the above conversion technologies become commercially viable.
Acknowledgements This work was supported by the EU-Program LIFEþ LIFE08 ENV/GR/ 000569 and by the project SustainDiesel-09SYN-32-328 which is funded 50% by the European
Commission and the Greek Government.
Nomenclature
FAME Fatty acid methyl esters
GHG Greenhouse gas
GWP Global warming potential
HAGO Heavy atmospheric gas oil
HVOs Hydrotreated vegetable oils
LAGO Light atmospheric gas oil
LCA Life cycle assessment
WCO Waste cooking oil
WTT Well-to-tank
TTW Tank-to-wheel
WTW Well-to-wheel
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Part VIII
Energy Technologies and Their Effect on Global Warming
Hydrogen Energy and Technologies
Chapter 31
Spark-Ignition Engine Fueled with Methane-Hydrogen Blends
G.M. Kosmadakis, F. Moreno, J. Arroyo, M. Mu~noz, and C.D. Rakopoulos
Introduction
Apart from engine-related techniques to meet stringent imposed emissions regula-
tions and higher efficiency over a large range of operating conditions and loads,
engine researchers have focused their interest on the domain of fuel-related tech-
niques (Rakopoulos and Giakoumis 2009). It is true that considerable attention has
been paid in the development of alternative fuel sources, with emphasis on liquid
bio-fuels that possess the added advantage of being renewable, such as vegetable
oil, bio-diesel, ethanol, butanol, and diethyl ether (Agathou and Kyritsis 2014;
Rakopoulos 2012, 2013; Wang et al. 2010). Moreover, many internal combustion
engines, usually converted from commercial compression- or spark-ignition
engines, have been fueled with various alternative gaseous fuels, such as the most
common methane (or natural gas) and liquefied petroleum gas to the most rarely
syngas and biogas, for use in power generation and transportation, showing inher-
ently clean nature of combustion with reduced emitted pollutants (Papagiannakis
and Zannis 2013; Rakopoulos and Kyritsis 2006; Rakopoulos and Michos 2009).
Finally, fuel blends show some interesting features, especially when hydrogen is
added to a conventional fuel for combustion enhancement, due to its very high
combustion speed (Kosmadakis et al. 2012).
G.M. Kosmadakis (*) • C.D. Rakopoulos Internal Combustion Engines Laboratory, Thermal Engineering Department, School of
Mechanical Engineering, National Technical University of Athens, 9 Heroon Polytechniou St.,
Zografou Campus, Athens 15780, Greece
e-mail: [email protected]; [email protected]
F. Moreno • J. Arroyo • M. Mu~noz Laboratory of Engines, Department of Mechanical Engineering, University of Zaragoza,
C/Marı́a de Luna s/n, Zaragoza 50018, Spain
e-mail: [email protected]; [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_31
405
One promising fuel blend is the methane/hydrogen one. The addition of even a
small hydrogen quantity in methane increases the combustion speed, improving
engine efficiency, while the fuel flammability limit is extended, allowing the use of
leaner mixtures. Moreover, CO2 and HC emissions are decreased, since the initial
amount of carbon in the fuel blend is decreased (Ma et al. 2008). On the other hand,
nitrogen oxides (NOx) emissions are increased, because of the higher combustion
velocity and burned gas temperature, while the event of knock is likely to occur for
high hydrogen percentage (Moreno et al. 2012).
Various experimental facilities have been developed for the investigation of the
combustion processes of methane/hydrogen blends, and the performance of SI
engines under different operating conditions and strategies (Demuynck
et al. 2009; Moreno et al. 2012), as well as for the in-cylinder processes and their
exhaust emissions (Akansu et al. 2007). Apart from these experimental studies,
there exist many simulation works focusing mainly on the engine performance
parameters (Aliramezani, et al. 2013) and to some extent to the nitric oxide
(NO) emissions, using the thermal NO production path (Dimopoulos et al. 2007),
widely known as the “three-equation Zeldovich mechanism”.
The present study concerns the extension of the combustion model of an
in-house CFD code developed by the NTUA team. This model has been initially
developed for the simulation of the power cycle of hydrogen-fueled SI engines, and
validated over many different conditions, including variable ignition timing, com-
pression ratio, large range of equivalence ratios, and EGR (Kosmadakis et al. 2012;
Kosmadakis and Rakopoulos 2014a, b; Rakopoulos et al. 2010a, 2011). The
extension of this combustion model and of the CFD code mainly concerns the
introduction of the carbon chemistry. Three more species have been added (carbon
dioxide, carbon monoxide and methane), together with an appropriate laminar
flame speed correlation for methane fuel, making the code capable of simulating
such combustion processes.
In order to validate the CFD code, appropriate measured data are used from a
two-cylinder engine. It has been decided here to focus on the variable hydrogen
content, keeping all other parameters constant, whereas it is planned to conduct
further investigation at other conditions as well in the future. For the validation of
this model, the calculated results regarding engine performance and nitric oxide
emissions are compared with the corresponding measured ones. From the analysis it
is concluded that the presented combustion model manages to predict adequately
the engine performance within the range of examined hydrogen content. As far as
the nitric oxide exhaust emissions is concerned, the model manages to capture
qualitatively correct the trend as hydrogen is increased, while in absolute values a
small difference exists from the measured ones. Then, a detailed investigation of
flame propagation and in-cylinder combustion is implemented, revealing the capa-
bilities of the CFD code for detailed combustion analysis and engine research.
406 G.M. Kosmadakis et al.
Experimental Facilities
The experimental facilities are briefly presented next, while further details can be
found in (Moreno et al. 2012).
Engine Modifications
The experimental tests were carried out on a Lombardini LGW 523 MPI spark
ignition engine, with two cylinders and total swept volume of 505 cm3. The engine
was properly modified to work with gaseous fuels containing hydrogen. These
modifications are briefly mentioned next. First, an additional gaseous fuel supply
circuit was mounted in parallel with the original gasoline circuit. Gas injectors are
designed and manufactured by Quantum, and prevent from premature failure in dry
gas applications. To favour the homogeneity of the air-fuel mixture inside the
cylinder, a new gas injection port was designed and installed after the inlet
manifold, where the gas injectors are fitted. Both gas injectors are fed by a gas
ramp connected to the gaseous fuel supply circuit of the test rig, which is explained
next. The ignition system was also modified, adding two BERU coils to ignite two
NGK spark plugs with low enough thermal grade to prevent problems like
pre-ignition. The original engine management system has been replaced by an
AEM 30-1900U Universal Programmable Engine Management System, which
controls all working parameters of the engine. The crankshaft angle at which the
gaseous fuels are injected has a big influence on performance, and therefore the
engine was converted to sequential injection. To this end, the installation of a cam
sensor was necessary, which allowed the synchronization between the strokes of the
cylinders. Moreover, the original narrow band oxygen sensor was replaced by a
wide band universal exhaust gas oxygen sensor (BOSCH LSU 4.2) with better
control of the fuel-air equivalence ratio, especially at lean equivalence ratios.
Finally, in order to perform an analysis of the combustion behavior, a piezoelectric
pressure sensor (Kistler 6053CC60) was mounted in the combustion chamber, in
order to acquire and analyze the pressure inside the cylinder.
Experimental Procedures
The engine was coupled to a Tecner E315 dynamometer, which allows testing
engines at constant speed or load. Data acquisition system of the test bench
recorded the load, speed, temperatures, pressures and fuel and air consumptions.
Pollutant emissions were measured using a Signal Instruments exhaust gas analysis
installation. The measurement principles are based on non-dispersive infrared for
CO and CO2, flame detector ionization for HC, chemiluminescence for NOx and
paramagnetism for O2. The pressure inside the cylinder was measured with the
31 Spark-Ignition Engine Fueled with Methane-Hydrogen Blends 407
piezoelectric sensor mentioned above connected to a signal conditioning and data
acquisition system from National Instruments, controlled by a specific proprietary
software programmed in LabVIEW. The volumetric composition of the different
gaseous fuel blends tested is presented in Table 31.1.
The engine was tested at full load and at a wide range of speeds (from 2000 to
4500 rpm), but the results selected in this study to validate the model were those
corresponding to 4500 rpm. The use of hydrogen blends allows the extension of the
lean operation limits of the methane (Moreno et al. 2012), so an equivalence ratio of
0.8 was selected for all cases. The ignition timing was fixed at 33� CA BTDC, in order to focus on the combustion differences due to the different blend composition.
The injection timing was set to 15� CA BTDC during the intake stroke for all the fuel blends. According to engine valve timing, the injection at this moment ensures
that all fuel is injected, while the inlet valve is open for all cases.
All relevant measurements have been conducted at wide-open throttle (WOT), in
order to reduce the pumping losses. The main specifications of this engine are given
in Table 31.2.
Table 31.1 Composition of the gaseous fuel blends tested
H2 composition (% by vol.) CH4 composition (% by vol.)
Methane 0 100
G1 10 90
G2 30 70
G3 50 50
Table 31.2 Lombardini engine main specifications
Engine model and type
Lombardini engine, two-cylinder, naturally aspirated, four
stroke, water-cooled
Bore 72 mm
Stroke 62 mm
Swept volume (per cylinder) 252.5 cm3
Connecting rod length 107 mm
Compression ratio 10.7
Valves (per cylinder) 2
Engine speed 4500 rpm
Ignition timing 33� CA BTDC Equivalence ratio ~0.8
Number of piston rings 3
Valve timing
events
Inlet valve
opening
5� CA BTDC
Inlet valve
closure
59� CA ABDC
Exhaust valve
opening
57� CA BBDC
Exhaust valve
closure
7� CA ATDC
408 G.M. Kosmadakis et al.
CFD Code
The firing version of the CFD code developed by the NTUA team can simulate
three-dimensional curvilinear domains, using the finite volume method in a collo-
cated grid. It has been validated in previous published works (Kosmadakis
et al. 2012; Kosmadakis and Rakopoulos 2014a, b; Rakopoulos et al. 2010a,
2011), where it has been revealed that it can adequately simulate the power cycle
of hydrogen-fueled spark-ignition engines. In the next subsections the extended
combustion model is briefly presented, as applied in the present study and its main
differences with the addition of methane fuel are discussed. A detailed presentation
can be found in previous publications (Kosmadakis et al. 2012, 2013; Kosmadakis
and Rakopoulos 2014a, b; Rakopoulos et al. 2010a, b, 2011).
Combustion Model
The combustion model is briefly described in this section, which has been already
developed and applied in previous studies for hydrogen combustion. The main
difference here is that methane fuel and carbon chemistry are added in the transport
equations. Only its basic features are given, since its detailed presentation is
provided in previous publications (Kosmadakis et al. 2012; Rakopoulos
et al. 2010a).
For the calculation of the species reaction rates, the characteristic conversion
time-scale method has been followed (Abraham et al. 1985). A characteristic time-
scale (τc) is calculated, as the sum of the laminar conversion time (τl) and the turbulent mixing time (τt), which determines to what extent the combustible gas content of each computational cell has reached its chemical equilibrium during a
specific duration (equal to the computational time step). This method is followed
for the calculation of the reaction rates of all chemical species considered here,
namely H2, O2, N2, H2O, H, O, N, OH, CO, CO2, and CH4. The reaction rates for
the nitric oxide (NO) derived from three different paths (thermal NO, NNH and
N2O paths) have already been discussed in (Kosmadakis and Rakopoulos 2014a, b)
and will not be repeated here. Further details concerning the calculation of the
reaction rates with the use of the characteristic conversion time-scale method can be
found in (Rakopoulos et al. 2010a).
The correlation for the hydrogen laminar flame speed is the one proposed by
(Gerke et al. 2010), which includes stretch effects. A similar correlation for
methane is used, which is proposed by (Ouimette and Seers 2009), which is derived
under a wide range of pressure and temperature similar to the gas properties during
spark ignition. Other correlations have been examined as well (applicable over a
smaller range though), with similar results. The fuel blend laminar flame speed is
calculated using a Le Chatelier rule (Rakopoulos and Michos 2009), which is a
rather simple calculation method, but ensures that the most reliable correlations are
31 Spark-Ignition Engine Fueled with Methane-Hydrogen Blends 409
used for the two fuels (hydrogen and methane), taking into consideration stretch
effects. The laminar flame speed is used to track the computational cells, in which
the flame has propagated during the ignition phase through the calculation of the
flame radius, assuming that the flame propagation velocity is approximately equal
to the laminar flame speed during this phase. When the flame reaches a critical
radius, turbulent effects become dominant and then a turbulent burning velocity (ut)
is used to track the flame. The expression used for this velocity is the one proposed
by Zimont/Lipatnikov and Chomiak (Lipatnikov and Chomiak 1997; Zimont
2000), in which one calibration constant exists (constant “A”), which is appropri-
ately tuned for each fuel blend (Rakopoulos et al. 2010a). This correlation is given
in Eq. (31.1).
ut ¼ A u0ð Þ3=4 u1=2l D�1=4T,u L1=4t þ ul ð31:1Þ
where A is the calibration constant that needs to be tuned, u’ the rms turbulent
velocity given by u0 ¼ ffiffiffiffiffiffiffiffiffiffi2k=3p , ul the stretched laminar flame speed, DT,u the thermal diffusivity of the unburned mixture, and Lt the turbulent integral length
scale given by Lt ¼ 0:37 u0ð Þ3=ε.
Computational Details
Some initial and boundary conditions are provided from the experimental data, such
as the pressure at IVC, and the inlet air (humidity in the inlet air is neglected) and
hydrogen/methane flow rates. For the rest of the required conditions, reliable
estimations are used, such as the gas temperature at IVC (from 380 up to 405 K
as the hydrogen content increases), wall temperature at IVC (from 440 up to 450 K
as the hydrogen content increases), residual gas mass fraction (around 6–7%), and
turbulent kinetic energy at IVC (constant and equal to 55 m2/s2 for all cases).
The constructed computational mesh has (40� 40� 30) grid lines along each axis (see Fig. 31.1) and has been tested for grid independence. The addition and
removal of mesh layers according to the piston movement is also used, since during
compression the height of the cells decreases at the dead volume. The engine is
equipped with a small bowl-in-piston, and its geometry has been extrapolated with
the highest possible detail from the engine design provided by the manufacturer.
The computational time step used is equal to 1� CA, which is further decreased from the beginning of the combustion period and afterwards becoming equal to 0.4�
CA. Such time step is sufficient small, since the engine speed is high and equal to
4500 rpm. Finally, the only calibration constant used in the in-house CFD code,
which exists in the expression of the turbulent flame speed (no calibration factors
exist in the heat transfer and crevice models), has a different value for each fuel
blend, which is however in the range of 0.7 (similar with hydrogen combustion).
410 G.M. Kosmadakis et al.
Results and Discussion
Test Cases Considered
The main engine conditions and settings of the test cases examined in the current
study have been shown previously in Table 31.2. Focus is given on the effect of
hydrogen content in the fuel (four test cases considered).
CFD Code Validation
The validation of the CFD code is presented here, which includes the comparison of
the predicted performance and NO emissions with the available measured data for
the methane/hydrogen-fueled SI engine.
Fig. 31.1 Computational grid at IVC with
40� 40� 30 grid lines along the x, y, z axis. The
bowl-in-piston is depicted
at the bottom
31 Spark-Ignition Engine Fueled with Methane-Hydrogen Blends 411
Engine Performance
The CFD code has been applied for the simulation of the four test cases. In Fig. 31.2
is shown the comparison of the predicted with the measured cylinder pressure for
variable hydrogen content.
The pressure traces are predicted with high accuracy, since for every case
considered the peak pressure and its timing are very well captured, with only
some minor discrepancies. These can be partly attributed to the correlation of the
laminar flame speeds used in the CFD code, being near to their application range,
50-50%: methane-H2
120 140 160 180 200 220 240
0
10
20
30
40
50
70-30%: methane-H2
120 140 160 180 200 220 240
Crank angle degrees (ABDC)
0
10
20
30
40
50
90-10% methane-H2
120 140 160 180 200 220 240
0
10
20
30
40
50
100-0%: methane-H2
120 140 160 180 200 220 240
Crank angle degrees (ABDC)
0
10
20
30
40
50 Measured
Calculated
C yl
in d
er p
re ss
u re
( b
ar )
C yl
in d
er p
re ss
u re
( b
ar )
C yl
in d
er p
re ss
u re
( b
ar )
C yl
in d
er p
re ss
u re
( b
ar )
Fig. 31.2 Comparison of calculated pressure traces with the corresponding measured ones for variable hydrogen content
412 G.M. Kosmadakis et al.
and to the higher heat loss calculated during the end of combustion. Nevertheless,
the cylinder pressure numerical results can be considered reliable, providing a good
proof of the reliability of the CFD code developed and of the presented results in the
next subsections.
This conclusion is also justified with the good comparison of the net heat release
rates, which is shown in Fig. 31.3. The maximum rate is well captured from the
CFD code, together with the combustion timing and profile.
Again, the process during the expansion stroke shows some differences, which
are under further investigation. Some possible causes can be some differences with
the exact bowl geometry, a non-homogeneous gas mixture at IVC, and the uncer-
tainty on the values of the initial gas temperature at IVC and wall temperature.
50-50%: methane-H2
120 140 160 180 200 220 240
-4
0
4
8
12
16
20
70-30%: methane-H2
120 140 160 180 200 220 240
-4
0
4
8
12
16
20
90-10% methane-H2
120 140 160 180 200 220 240
-4
0
4
8
12
16
20
100-0%: methane-H2
120 140 160 180 200 220 240
Crank angle degrees (ABDC)
Crank angle degrees (ABDC)
-4
0
4
8
12
16
20 Measured
Calculated
N et
h ea
t re
le as
e ra
te (
J/ o C
A )
N et
h ea
t re
le as
e ra
te (
J/ o C
A )
N et
h ea
t re
le as
e ra
te (
J/ o C
A )
N et
h ea
t re
le as
e ra
te (
J/ o C
A )
Fig. 31.3 Comparison of calculated net heat release rates with the corresponding measured ones for variable hydrogen content
31 Spark-Ignition Engine Fueled with Methane-Hydrogen Blends 413
The local increase of the heat release rates during the expansion stroke at around
200� CA ABDC is due to the rapid combustion of the end gas near the cylinder liner. This is advanced as the hydrogen content is increased, due to the more rapid
combustion. According to the measured values, a different trend exists, since this
end gas slowly burns during a larger period at the expansion stroke.
Similar comparisons have been made concerning the indicated mean effective
pressure (IMEP) and indicated efficiency. These parameters provide a more general
insight on the accuracy of the numerical results using the CFD code. It has been
shown that both IMEP and indicated efficiency are adequately predicted, since for
all cases considered a good match exists with few differences. These exist due to the
discrepancies of cylinder pressure during the exhaust stroke.
The main conclusion of this validation process is that the CFD code can predict
adequately the performance of such engine with methane/hydrogen fuel blends and
its application can be extended for the investigation of various conditions and
engine designs.
NO Emissions
After the validation of the performance, the study focuses on the NO exhaust
emissions, which are investigated for the test cases of Table 31.1. The calculated
NO values are obtained using the CFD code and are compared with the measured
values (see Fig. 31.4).
It can be observed that the trend of the NO emissions is adequately captured, as
the hydrogen content increases. Concerning the absolute emission values there is
some discrepancy, which is almost equal for all cases (around 800 ppm). For high
hydrogen content, the relevant variation is maintained lower than around 30–40%,
which can be considered acceptable, since no calibration factor is included in the
0 10 20 30 40 50
Hydrogen content (by vol. %)
0
1000
2000
3000
Measured Calculated
N O
e xh
au st
e m
is si
o n
s (p
p m
)
Fig. 31.4 Comparison of calculated NO emissions
with the corresponding
measured ones for variable
hydrogen content
414 G.M. Kosmadakis et al.
emissions model. Nevertheless, such prediction level is adequate, having in mind
all uncertainty factors in the calculation of NO emissions (Kosmadakis et al. 2012;
Kosmadakis and Rakopoulos 2014a).
Combustion Analysis
The validation of the extended combustion model revealed that the power cycle of a
SI engine with variable hydrogen content can be simulated with detail, while both
performance and NO emissions are adequately calculated. Therefore, the CFD code
can be then applied for further combustion analysis, by providing some insight on
the in-cylinder processes.
As the hydrogen content increases, the combustion speed is higher, increasing
the gas temperatures during combustion. This is the main reason that NO emissions
are higher, which is one of the main concerns for the use of hydrogen in blends
(Moreno et al. 2012). Such indication is provided in Fig. 31.5, where the calculated
mean gas temperature is observed. In the same figure are also shown the mean NO
reaction rates, which depend a lot on the local gas temperature and the local species
concentration.
It is observed that the maximum temperature (around 2400 K) is reached for the
50–50% blend, which is observed some CA degrees before the 100–0% blend.
Also, as the hydrogen content increases, the NO reaction rates rapidly increase,
since there is an exponential dependence from the temperature (Kosmadakis and
Rakopoulos 2014a). Moreover, even some small addition of hydrogen in the fuel
160 180 200 220 240
0
1
2
3
4
5
6 Case 1 (100-0%)
Case 2 (90-10%)
Case 3 (70-30%)
Case 4 (50-50%)
160 180 200 220 240
600
1000
1400
1800
2200
2600
Case 1 (100-0%)
Case 2 (90-10%)
Case 3 (70-30%)
Case 4 (50-50%)
M ea
n g
as t
em p
er at
u re
( K
)
Crank angle degrees (ABDC) Crank angle degrees (ABDC)
M ea
n N
O r
ea ct
io n
r at
e (k
g N
O /k
g m
ix /s
)
Fig. 31.5 Mean gas temperature and mean NO reaction rates during combustion and early expansion for variable hydrogen content
31 Spark-Ignition Engine Fueled with Methane-Hydrogen Blends 415
blend, as is the case of 90–10%, increases the maximum mean gas temperature by
more than 100 K and almost doubles the mean NO reaction rate.
Some more detailed aspects of flame propagation are presented next. The
differences observed are mainly due to the variable hydrogen content, since all
other important parameters and conditions are exactly the same for all cases. The
initial temperature and pressure at IVC show some small differences, which are
however negligible and do not introduce any important changes. In Fig. 31.6 is
shown the flame radius, calculated from the computational cells, which are located
at an axial direction crossing the spark-plug, and until the flame reaches the piston.
In the same figure is also shown the mean laminar flame speed during the early
stages of combustion and the turbulent flame speed. It should be stressed that these
speeds are mean values averaged over the cells that are inside the flame front and
therefore should be only treated as indicative ones.
The spark-timing is constant and equal to 147� CA ABDC. Therefore, for all cases the combustion starts at the same time and it is possible to identify the effect
of hydrogen addition on the flame speeds and flame propagation inside the cylinder.
It is observed that the flame radius increases more quickly for higher hydrogen
content, which is directly related with the mixture laminar flame speed (the
hydrogen laminar flame speed is many times higher than the methane one) and
turbulent flame speed. The latter mainly depends on the local turbulent properties
and the laminar flame speed. These properties are more or less the same for all
cases, since a constant value of turbulence has been considered for all cases (engine
speed is 4500 rpm). Therefore, the turbulent flame speed depends almost exclu-
sively on the laminar flame speed. For the 50–50% blend, its maximum value is
around twice the maximum value for the pure methane case. In other words, flame
propagation is around two times higher, in case hydrogen is added in methane by
50% by vol. This is verified by the combustion duration angles (0–5 and 5–95%),
but it can be better visualized by the flame images, shown in Fig. 31.7. These
images depict how the flame propagates inside the cylinder after the ignition timing,
140 150 160 170 180 190
100-0% 90-10% 70-30% 50-50%
0
10
20
30
40
140 150 160 170 180 190
0
2
4
6
8 100-0% 90-10% 70-30% 50-50%
140 150 160 170 180 190
0
2
4
6
8
10
12 100-0% 90-10% 70-30% 50-50%
F la
m e
ra d
iu s
(m m
)
L am
in ar
f la
m e
sp ee
d (
m /s
)
T u
rb u
le n
t fl
am e
sp ee
d (
m /s
)
Crank angle degrees (ABDC) Crank angle degrees (ABDC) Crank angle degrees (ABDC)
Fig. 31.6 Flame radius, laminar flame speed and turbulent flame speed for variable hydrogen content
416 G.M. Kosmadakis et al.
noticing the differences for the various hydrogen contents. The spark-plug is offset
from the cylinder axis, as one can guess from the location of the ignition kernel.
Owing to the high burning velocity of hydrogen, the flame has significantly
expanded at TDC for the 50–50% blend. Moreover, the flame has covered the
whole combustion chamber at around 200� CA ABDC for the 50–50% blend, and at 220� CA ABDC for the pure methane case. The main differences can be identified during early combustion, where the flame propagates with its laminar
flame speed, which is much lower for the pure methane case, as mentioned
previously.
Fig. 31.7 In-cylinder flame images for 50–50% hydrogen/methane blend and pure methane
31 Spark-Ignition Engine Fueled with Methane-Hydrogen Blends 417
Summary and Conclusions
In the present work, the combustion model of a 3D-CFD code has been extended.
This was originally developed for pure hydrogen combustion, while this extension
allowed it to simulate the power cycle of hydrogen/methane blends. The first step
was to validate the code. Therefore, detailed measurements on a SI engine have
been used for that purpose. The experimental data are for constant equivalence ratio
and load, while only the hydrogen content is varied within the range 0–50% by vol.
The validation has been conducted for both performance and NO emissions. This
procedure showed that the CFD code is capable of predicting the performance
parameters of such engine for variable hydrogen content, while the NO emissions
are adequately predicted and closely following the same trend as the measured
ones. Such conclusions are encouraging, in order to apply the CFD code for further
combustion analysis. Some first relevant tasks have been presented in the second
part of this work, where focus has been given on the flame propagation for variable
hydrogen content. It has been shown that the addition of even a small amount of
hydrogen can substantially increase the flame speed, especially during the early
combustion period.
In conclusion, the results obtained so far are encouraging, by showing that the
simulation of SI engines fueled with hydrogen/methane blends using a detailed
numerical tool, such as the one presented here, can yield reliable results, with the
use of just one calibration constant per blend. However, a more extended study
should be conducted in the future, covering a wider range of operating conditions
(such as variable equivalence ratio and speed), to justify the validity of the model
and its ability to capture combustion phenomena without adjusting the value of the
calibration constant.
Acknowledgement Dr. G.M. Kosmadakis (NTUA) wishes to thank the Greek State Scholarships Foundation for granting him an “IKY Fellowship of excellence for postgraduate studies in
Greece—Siemens Program, years 2013–2015.”
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Chapter 32
Hydrogen Fueled Airplanes, Test Case: Aviation in Libya
Satya P. Bindra, Ali Alwafi, Ashour Saasi, Elbahlul Musa Abogrean,
Mohsen Masaud A. Maatugh, and Khaled Khalifa
Introduction
World over CO2 emission from aviation is on the rise. See Fig. 32.1 Hydrogen
fueled airplane offers the most promising zero-emission alternative to conventional
aircraft since they have a similar flying range and refueling time. While Hydrogen
fueled airplanes require massive investment and government subsidies for fuelling
stations, it is noted that hydrogen—the most abundant element in the universe—
could be extracted from many different sources and had the advantage of being
portable and more easily stored than electricity. The example is the southern
Japanese city of Fukuoka that recently completed a fuelling station that uses
hydrogen made from sewage. Of course, there are technological hurdles that need
to be cleared to make this commercially viable.
Low carbon environmental friendly science and technology for sustainable civil
aviation in new Libya is being planned in line with UNCSD Rio+20 Focal Point
Libya (Bindra 2012; Bindra et al. 2012) objectives (a) To Make the airport
environment friendly and achieve higher level of customer satisfaction; (b) To
lay special emphasis on the development of infrastructure for remote and inacces-
sible areas; (c) To provide airport capacity ahead of demand; (d) To encourage
greater efficiency in Airport Operations on ground and in the air; (e) To provide
multi-modal linkages for flexibility. The focus regarding the internal infrastructure
lies on the vehicles moving at, in, on and around the airport as well as an innovative
taxiway and runway constellation using: (1) CAV: Clean Air Vehicles; (2) ITC:
Innovative Taxiway Constellation; (3) ERS: Efficient Runway system. The purpose
S.P. Bindra (*) UNCSD Rio+20 Focal Point, Sbia, Libya
e-mail: [email protected]
A. Alwafi • A. Saasi • E.M. Abogrean • M.M.A. Maatugh • K. Khalifa
Civil Aviation and Meteorology Technical College, Sbia, Libya
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_32
421
is to meet and exceed ICAO guidelines issued to its Member States. The idea is to
commit the country to help develop solutions for the sustainable future of interna-
tional civil aviation, in cooperation with industry, sister United Nations agencies
and Non-governmental Organizations. It would serve as a catalyst for economic and
social development. Therefore, air transport work force needs to be equipped with
tools, techniques and technologies that focus on help reduce environmental foot-
print, in line with the guidance and leadership of Environmental General Authority
and ICAO. Its goal is to strike a balance among the three pillars of sustainability—
social, economic and environmental so that air transport grows in an environmen-
tally sustainable manner, while continuing to ensure freedom to travel by air.
Policy of Libya is helping establish democratization of air travel by access to
sustainable air transport in a guaranteed manner for its future generations. Libyan
national UNCSD Rio+20 Focal Point has set clear objectives and provides frame-
work to address the new energy challenges as we transition to a green economy
(Bindra 2014; Robertson 2008). This includes use of sustainable alternative fuels as
one of the most promising win-win-win solutions for aviation’s future. Our Green Airport Concept [4.5] is based on a Clean Air Vehicle Policy. The fleet operating at
or near the airport consists of:- Compressed Natural Gas Vehicles (CNG);- Electric
Vehicles;- Hybrid-Electric Vehicles;- Green Airport TRAIN powered by hydro
electricity.
Furthermore it supports Diesel Vehicles Filters for all transporter and charter bus
operators and shuttles. Libya is committed to make available of these fuels through
policies that incentivize their development and their deployment. This paper after
review of the situation is designed to show that how the civil aviation industry in the
country is committed to meet its environmental commitments through its own
15
10
5
0 1950
M ill
io n
B ar
re ls
p er
D ay
1960
Transportation sector leads in petroleum use Carbon emissions from global aviation exceed the total output of many countries
Aviation Contribution to CO2
Electric Power1
1970 1980 1990
Industrial
Transportation
Residential and Commercial
2000
Fig. 32.1 Aviation contribution to CO2
422 S.P. Bindra et al.
resources. For this the country policy is devised based on better co-ordination of
Libyan national Civil aviation activities at the international level by elimination of
duplication in all areas, and to build upon the work of specialized agencies and
existing sustainable development frameworks.
An Overview of Civil Aviation and Airports in Libya
Civil aviation in Libya in 1987 was the responsibility of the Secretariat of Com-
munications, which operated all airports, and the Civil Aviation Institute, which
trained all personnel. The three international airports in 1985 were located at Tripoli
(Al Aziziyah), Benghazi (Benina), and Sabha. Smaller airfields were located at
Marsa al Burayqah, Tobruk Ghat, Ghadamis, Al Kufrah, and several other loca-
tions. Most civil air personnel went abroad for training. Britain suspended its air
traffic control training program for Libyans in 1985, but Pakistan subsequently
agreed to train about 78 Libyan air traffic controllers (Bindra 2014).
The national air carrier, Libyan Arab Airlines (LAA), was nationalized in 1973.
Possessing only a dozen aircraft in 1977, it grew rapidly, expanding its fleet to
25 aircraft in 1985. The main aircraft in service were manufactured by Boeing,
Hawker Siddeley, Caravelle, and Fokker. In 1980, LAA carried 1.17 million
passengers. A new carrier called United African Airlines (UAA) was created in
1985 in association with LAA.
Airports in New Libya
Currently air transportation is one of the most pressing issues for the new Libya.
The country’s infrastructure has suffered from decades of neglect and the transport network is essential to rebuilding the economy. The ports and the airports, in
particular, have been neglected and underdeveloped. In a country which imports
some 80% of its food, the freight sector requires urgent attention. Despite some
damage to facilities and aircraft, Libya’s airports steadily reopened after the revolution. Most recently Sirte airport reopened at the end of October, following
extensive repair and maintenance work to address damage sustained during the
fighting. Even before the airports were fully-functional, airlines resumed flights to
Libya, with the very first being Turkish Airlines, which restarted daily Istanbul to
Benghazi flights from 13 September 2011.
Concerns have been raised about safety, not least by the European Union. In
accordance with the International Civil Aviation Organisation (ICAO), in March
the EU banned Libya’s two state-owned carriers, Afriqiyah Airways and Libyan Airlines from flying to Europe, on the grounds of flight safety and airport security.
Both carriers were obliged to wet-lease aircraft to maintain services to some
European destinations. The EU said when it imposed the ban last April that it
32 Hydrogen Fueled Airplanes, Test Case: Aviation in Libya 423
would review it this month. The ban is expected to remain in force for some further
while. Aviation freight at Libya’s 18 main airports faces similar to the ports, in particular limited and obsolete equipment. For smaller-scale cargo, air freight is
often more straightforward and cheaper, as well as faster, than sea freight, because
the airports do not have the congestion problems of the ports. Urgent cargo, such as
medicine, hospital equipment and essential equipment for the oil industry usually
comes via air freight. A state monopoly operates at all airports, where only one
company, the state-run Shorooq Handling and Ground Services company, can deal
with freight deliveries. “The country’s airports need to be rebuilt to accommodate big planes,” said Mohamed Douas, CEO of Libya Shipping Line “and the services
need to be liberalised, because the current state-run services are inadequate, inef-
ficient and totally under-equipped.” Recently Civil Aviation Authority of Libya
(LCAA) has launched a pioneering program to perform a fundamental country-
wide upgrade of the existing Aeronautical Fixed Telecommunication Network
(AFTN) and Automatic Identification System (AIS) infrastructure in order to
enhance flight safety. LCAA have been effectively operating COMSOFT’s highly dependable AIDA-NG and CADAS products since 2004, and have again put their
full confidence in the German expert to address Libya’s high technical and opera- tional expectations. With the upgrade Libya will join the still exclusive club of Air
navigation service provider (ANSPs) processing the aeronautical information data
in line with the ICAO Roadmap AIS to AIM. In addition, LCAA will benefit from
the fast and highly reliable Aeronautical Message Handling System (AMHS) that
already connects many countries in the Arab peninsula and North African Region.
Home to the world’s hottest desert, The Sahara, Libya’s expansive sandy land- scape makes air travel essential in order to facilitate Libya’s transportation infra- structure; meanwhile a number of national airports are of growing importance.
COMSOFT’s innovative AMHS and AIM solutions will be provided to the central site in capital city Tripoli and countrywide messaging and information
management services will also be delivered via remote installations at Metiga,
Mistrata, Sahba, Benina.
During the course of the ambitious project LCAA will upgrade their NOTAM,
OPMET, Briefing and Flight Plan Management facilities and simultaneously inte-
grate the components in a state-of-the-art AIXM 5.1-based AIM concept (Bindra
2012; Bindra et al. 2012). This includes the central handling of static data and the
fully integrated ability to generate electronic AIP and aeronautical charts directly
from the central AIXM 5.1 database contents.
Tripoli International Airport is a public airport serving international and domes-
tic passengers from most European and Arab airlines, and handling over three
million travelers per year. With the installation of two new terminals they hope to
increase this capacity to 20 million passengers annually, therefore, increasing the
need for advanced and reliable message handling. Installation of an end around
taxiway, which is based on the newest developments regarding safety and effi-
ciency: ITC—Innovative Taxiway Constellation is planned to ensure that:
424 S.P. Bindra et al.
• Aircraft will be allowed to taxi around the end of the runway instead of waiting
to cross them.
• Even if aircraft have to expect a longer taxi, it can be another way of avoiding a
lengthy queue at the holding point.
• New taxiway constellation significantly decreases runway crossings thereby
increasing safety and efficiency, thereby reducing the probability of an runway
incursion.
• Airlines, passengers and the environment are the ultimate benefactors of the new
taxiway, because it will safe time, fuel and fumes.
Hydrogen Powered Airplanes
Hydrogen powered aircraft are usually designed with the liquid hydrogen fuel
carried inside the fuselage, in order to minimize surface-area and reduce boil-off.
The future of low carbon science & technology airplanes are assessed, evaluated &
its findings are being implemented & monitored after a fact finding mission. The
information was gathered to help assess and create three new concentration curric-
ulums. One of the current green sky initiative related curriculum objectives being
developed is the specialty in Aviation Management as the first of its kind in Libya
(Bindra et al. 2012). It is based on the meetings with industry & academia leaders
representing a vast cross-section of the Libyan aviation industry. This includes the
Civil Aviation Authority, Libyan Airlines, Air Libya, ICAO—International Civil
Aviation Organization, Airport Company of Libya, local airport managers, and
local and regional government agencies. The overall impression is that there is a
great need for greener aviation in the higher education system of Libya. This paper
examines the needs assessment for aviation fuel curriculum in the higher educa-
tional system and also explores the content of this curriculum.
Rationale for Change and Development
Aviation management encompasses a multitude of aviation interest since the
industry has delineated itself into various categories such as airline, airport, civil
aviation, air traffic control, and piloting (as evident by the number of professional
associations). All these represent the planning and managing of a business that
brings people together with a specific mission and need to accomplish a specific
organizational goal. Aviation helps contribute to growth in many other areas:
tourism hinges on airports and the airlines to deliver passengers to resort locations,
corporate enterprises depend on civil aviation businesses to maintain and fuel their
aircraft and to take care of their flying customers. All these aviation services require
a strong regulatory body like the Libyan Civil Aviation Authority (CAA) and a
strong airport management system.
32 Hydrogen Fueled Airplanes, Test Case: Aviation in Libya 425
The current state of the Libyan Aviation Industry is in turmoil and requires a
growing and prospering environment for great strides to modernize and expand. A
move by the country to become a North African hub requires participation at the
highest forum with regards to aviation matters. There is a need for better trained
individuals to work in this dynamic industry. In the Libyan Civil Aviation
Authority’s Strategic Plan in line with Ministry of planning 2013–2030 3rd gener- ation planning requires, strategic mapping process (Bindra 2012, 2014). This out-
lines the new strategic objective to attract, develop, and retain human capital. The
critical issues outlined in this process include: establishing competitive remunera-
tion structures, favorable working environments, and commitment by management
to training development, creation of a management development program, and staff
Morale. It is hoped that these issues will assist in accomplishing one of its main
priorities that is aviation safety, security, transformation and growth.
UNCSD RIO+ 20 Libya Focal Point for Sustainable Development
Rio + 20, like the past Rio Earth Summit & Johannesburg Conferences, did provide
an opportunity for the international community to assess achievements and progress
since 1992 together (Bindra et al. 2012). It also gave a forum to highlight the unmet
objectives and gaps that have hindered implementation of the decisions and rec-
ommendations of the two previous summits, with a view to making the improve-
ments needed for the post-2012 global agenda. This agenda acknowledges the
legitimate expectations by incorporating economic, social and environmental con-
cerns, in order to better respond to the necessity for growth and progress that can
ensure a decent standard of living for citizens in a context of multidimensional
international crisis. New Libya’s input to the United Nations Conference on Sustainable Development held in Rio de Janeiro in June 20–22, 2012 is part of
the both national New Libya rebuilding efforts in line with international
community’s global effort to promote support and enhance development that is respectful of the environment. It is the outcome of a non-exhaustive analysis of
New Libya’s socio-economic and environmental achievements as a result of the commitments made at the 1992 Rio Summit, Johannesburg Summit and numerous
subsequent events & conferences. It also reflects the concerns that free Libyan
society emerging out of the recent crisis and faced with formidable task of rebuild-
ing the nation shares with its neighbour regional and international partners in the
Mediterranean & Euro Med region, Maghreb Union, African Union, the League of
Arab States and the Group of 77 and BRICS, which it shared once again in 2012.
Libya has initiated a revitalized national environment strategy (NES) and a
national plan of action for environment and sustainable development (NPAE-SD)
in the context of a participatory approach involving all stakeholders as national
actors. The national environmental strategy aims to achieve sustainable economic
426 S.P. Bindra et al.
growth both during and after rebuilding by putting in place public policies to
improve health and quality of life, conserve and increase the productivity of natural
resources especially its Oil & Gas reserves, reduce economic losses and increase
competitiveness and, lastly, protect the environment. It is committed to put into
practice through the rebuilding New Libya laws on sustainable development.
A number of initiatives (Bindra et al. 2012; Bindra 2014) have also been created,
including the First Libyan Environmental Engineering & Sciences Center (EESC),
Libyan Business Council for Sustainable Development (LBCSD), Libyan 350 org,
Libyan National Platform for Risk Reduction, Care Libya Brand Foundation
(CLBF), Green Sky Initiative, Desert Prosperity Initiative, Sustainable Solid
Waste Management Initiative. The national, regional rebuilding schemes, and
initiatives provide a policy framework for a wide range of environmental protection
and regional rebuilding development after the Arab Spring aimed at sustainable
development.
The country is committed to implement many initiatives to foster education and
training on sustainable development. Authors as focal point in Libya have set up a
network of technical institutions committed to education and training on
Eco-Efficiency and sustainable development in the country (Bindra 2014).
Greener Skies Initiative in Libya
The green skies initiative by a team of leading former and serving professors and
experts in Libya is based on principles that govern both ecological systems and
control economic systems. Airspace design for the Environment considerations are
shown below:
It considers that “If you violate ecological principles you might be able to make a
fast buck on the short term,” “but long-term, you’ll have an economic disaster” It is
based on UNCSD Rio +20 Future we want that advocates and requires the need to
use citizen power backed by intelligent management of the ecosystems and nature-
based infrastructure (Bindra et al. 2012). It provides a way forward to think about
pragmatic and realistic approaches to the challenges of climate change and envi-
ronmental sustainability, and the critical role of innovation and greening of indus-
try. Equity, the right to development and the principle of common but differentiated
responsibilities are the basis of Libyan approach.”
In addition even for external infrastructure there is plan to introduce Inherently
Low Emission Vehicle Program (ILEAV). The purpose of the Program is to
evaluate airport use of alternative fuel vehicles (AFV) and infrastructure to deter-
mine their reliability, performance, and cost-effectiveness in the airport environ-
ment (Robertson 2008; Maniaci 2006). The Requirements are:
• Public-use airports in areas that do not meet federal air quality standards
designed to protect public health.
32 Hydrogen Fueled Airplanes, Test Case: Aviation in Libya 427
• Vehicles operating exclusively on six alternative fuels: Compressed Natural Gas
(CNG); Liquefied Natural Gas (LNG); Liquefied Petroleum Gas (LPG); elec-
tricity, hydrogen, or methanol-85. See Fig. 32.2 below with H2 Tanks of liquid
hydrogen study plane.
Being an alternative to traditional jet fuel, hydrogen has a higher energy density
per unit mass but a lower energy density per unit volume, and containing the hydrogen at high pressure requires a heavy container. In aircraft heavy containers
are not an option, and therefore regular carbon fibre tanks are often used, which can
only sustain a pressure of about 350 bar. This is significantly lower compared to
steel hydrogen containers (used in cars and ships) which can sustain 500–700 bar.
This limitation decreases the amount of energy that can be spent on the propulsion
by about half. Alternatively, as with some rockets, cryogenic liquid hydrogen could
be employed. Libya being a country blessed with highest solar radiation intensity
supports the recent Si2 as the first sun-powered aircraft able to stay aloft for several
days and nights. That is powered by more than 17,000 solar cells built into wings
that, at 72 m (236 feet), are almost as long as those of an Airbus A380 superjumbo.
This is an innovative design, the light-weight carbon fibre aircraft weighs only 2.3-
tonnes, about the same as a family 4� 4 and less than one percent of the weight of the A380. The propellor craft has four 17.5 horsepower electric motors with
rechargeable lithium batteries. It is planned to land 12 times on the trip lasting
about 25 days spread over five months.
The longest single leg allows a lone pilot fly non-stop for 5 days across the
Pacific Ocean between Nanjing, China and Hawaii, a distance of 8500 km (5270
miles) (Fig. 32.3).
From the Gulf Si2 it did cross the Arabian Sea to India before heading on to
Myanmar, China, Hawaii and New York. Landings are also earmarked for the
Mid-Western United States and either southern Europe or North Africa, depending
on weather conditions.
Fig. 32.2 H2 tanks of liquid hydrogen study plane
428 S.P. Bindra et al.
Si2 is the successor to Solar Impulse, a smaller craft that notched up a 26-h flight
in 2010, proving its ability to store enough power in the batteries during the day to
keep flying at night. It travels at 50–100 km per hour, with the slower speeds at
night to prevent the batteries from draining too quickly.
Libyan Strategy
The Libyan strategy includes a project to use information and communications
technologies to reform the technical education and scientific research system,
which has the potential to become a model for the proper integration of ICTs in
cleaner and greener skies using fuels like Hydrogen in the country.
Libya has also helped the country in developing system level improvement,
institutional level improvement and individual level improvement based on key
principles for GEF-UNDP supported national capacity self assessment (NCSA).
These principles are (1) Ensuring national ownership, leadership and policy com-
mitment, (2) Using existing mechanisms and structures whenever possible, (3) Pro-
moting multi-stakeholder participation, (4) Adopting a holistic approach to capacity
building, (5) Adopting a long-term approach to capacity building, (6) Considering
obligations of the three Rio Conventions; (7) Balance Between Process and Product
so that (a) The process should increase stakeholders buy-in and (b) The Product
should be of high quality so that government take recommendations/actions as
priorities into national budgeting and donor can support it.
The current proposal under the form of civil aviation cleaner and greener
airplanes fuels aims at ensuring at relatively short notice, access to and progressive
Wingspan: 72.3 m
Planned world tour to promote alternative energy Solar Impusle 2
Distance: 35,000 km 500 hours flight time A 5-month missionLength: 22.4 m
Weight: 2,300 kg Ave. speed: 70 kph Max. altitude : 8,500 m Carbon fibre: 80%
17,000 solar cells spread across
Propulsion: 4 electric engines
Propellers 4 m in diameter
Cockpit: 3.8 m3 - Non-pressurised cabin - No heating or air conditioning - Insulating foam
Thickness of cells: 35 microns
Source: solarimpulse.com
270 m2 of wings and fuselage
Fig. 32.3 Factfile on the new solar-powered aircraft solar impulse 2
32 Hydrogen Fueled Airplanes, Test Case: Aviation in Libya 429
ownership by the Libyans, of the required technical and instrumental capacities.
This would also provide opportunities for implementation of practical steps like
rapid diffusion of economic data, information on best practices through networking.
At the international level, Libya intends to help in not only in transfer, adapt,
adopt, absorb and embrace advanced technology and governance practices but also
access to most up to date and unbiased scientific data and information to confront
challenges of future. This would help country to play an effective and leading role
in promoting international cooperation with organizations of the UN System,
among others ICAO, UNEP, UNESCO, FAO, as well as, regional counterparts
(Mediterranean, Euro-Med, Maghreb Union, Arab, Sahel and other African) and
also other multi- and bilateral funding or assistance providing sources.
Discussion of Case Study Survey Results from Respondents
Based on pilot scale surveys, interviews and meetings with stakeholders it is found
that every civil aviation entity has offered advice and input to the potential new
airplanes fuels & alternative Fuels See Figs. 32.2 and 32.4 and expressed immediate
support of the new program in Libya. All organizations express that they are
struggling to find relevant personal with appropriate aviation qualifications to hire
for entry level positions. Presently they are spending much time and money to
introduce the basic knowledge of aviation to new hires. They both agree there is a
1
0.9
0.8
0.7
0.6
0.5
0.4
0.3 0.6 0.7 0.8 0.9
Relative Fuel Carried
Advanced Technology
Design J Min Fuel
Design K Min NOx
Design C Min NOx
R el
at iv
e LT
O N
O x
Design B Min Fuel
1.1 1.2 1.31
Aerospace Design for the Environment • 60% laminar wing • 20% composite weight reduction • 10% vortex drag saving
Fig. 32.4 Airspace design for the environment
430 S.P. Bindra et al.
need for greener aviation management curriculum in higher education (Figs. 32.5
and 32.6).
Many respondents suggest that new Libya needs airport and airline managers
who are able to communicate with the public, understand their needs and deliver a
product to meet these needs within budget. They all feel that professional aviation
management skills must be help to coordinate elements of marketing, media,
sponsorship, budgets, financial management, public speaking, planning, and
Fig. 32.5 Jet fuel alternatives
Fig. 32.6 Alternative fuels for aviation
32 Hydrogen Fueled Airplanes, Test Case: Aviation in Libya 431
complying with regulatory bodies. Most stakeholders say that new Libya needs
more of sophisticated IT systems. These systems are required along with skill sets
needed for financial management, logistics, reservations, and certification.
Concluding Remarks
Hydrogen-fueled airplanes use hydrogen as a power source. Hydrogen is either
burned in jet engine, or internal combustion engine, or used to power a fuel cell to
generate electricity to power a propeller. The science & technology of hydrogen
fuelled airplanes for aviation industry impacted by low carbon requirement in new
Libya is in the process of change. The appraisal of existing situation and needs
assessment surveys of industry and government officials in Libya clearly indicate
the need for improved hydrogen fuelled airplanes. Survey results indicate that new
aviation fuel is feasible alternative similar to Toyota Mirai sedan—powered by
hydrogen and emitting nothing but water vapour from its tailpipe. The hydrogen
fuelled airplane like Mirai car can travel without refuelling, some three times
further than an electric car, and its tank can be filled in a few minutes like gasoline
engine vehicles. However, aircrafts need to be configured in such a fashion that the
current low energy output from hydrogen propulsion (a result of the low-pressure
hydrogen tanks) do not pose a problem due to its volume and high volatility. Finally
the paper demonstrates that in order to achieve aviation sustainability it is possible
to meet the challenges of 4� larger fuel tanks, higher drag, higher empty weight, H2 production issues, new infrastructure, affordable cost, high technical risk, passenger
acceptance and environmental effects.
References
Bindra, S. P. (2012). Rio+20 Libyan National Report. UNCSD. Brazil: Rio. Retrieved June 2012.
Bindra, S. P. (2014). Civil aviation technical college on low carbon sky related science &
technology education in Libya, Istanbul Turkey.
Bindra, S. P., et al. (2012). Change and development in civil aviation. ICERI 5th International Conference of Education, Research an Innovation 19th–21st of November, 2012. Madrid, Spain: IATED.
Maniaci, D. C. (2006). Operational performance prediction of a hydrogen-fueled commercial
transport. 2006 Symposium.
Robertson, D. (2008). Boeing tests first hydrogen powered plane. London: The Times.
432 S.P. Bindra et al.
Chapter 33
Perspectives of Hydrogen Automotive Applications in Croatia
Ankica Đukić, Ivan Güttler, and Robert Pašičko
Introduction
Global Warming
The warming signal in the global near-surface air and ocean temperature began to
emerge from the middle of the 20th century. Up to then, it was masked by the
internal variability of the Earths climate system and influences of the events such as
changes in the solar energy output and volcanic activities. Globally averaged
surface temperature change was estimated to equal 0.85 �C over the period from the 1880 to the 2012. However, the rate of this warming is increasing in recent
decades and regionally warming can acquire even higher levels. The changes in the
climate system are not limited only to temperature changes. Other changes in the
climate system include the melting of the Arctic sea ice, melting of the most of
the worlds glaciers, reduction of the land ice over Greenland and Antarctica.
Furthermore, the increasing rates of the sea level rise as well as the ocean heat
content, various changes in the hydrological system (this can regionally and locally
A. Đukić (*) Faculty of Mechanical Engineering and Naval Architecture, University of Zagreb, Ivana
Lučića 5, Zagreb 10000, Croatia
e-mail: [email protected]
I. Güttler
Meteorological and Hydrological Service of Croatia, Grič 3, Zagreb 10000, Croatia
e-mail: [email protected]
R. Pašičko
United Nations Development Programme, Radnička cesta 41, Zagreb 10000, Croatia
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_33
433
emerge either as a positive or negative change in the precipitation, runoff and soil-
moisture signal) and other changes that put pressure to the biosphere and society
(IPCC 2014).
Observed and projected temperature and precipitation changes over Croatia
were assessed in (Branković et al. 2013) and (MZOIP 2014). Various human
activities related to economic activities and population growth are intrinsically
related to the energy production and emission of various combustion products.
Although there are human related impacts such as changes in the land types and
land use practices (this can locally and regionally change the energy, momentum
and mass flows), most important impact is related to the changing the chemical
composition of the atmosphere, primarily through the emission of the GHG such as
CO2, CH4, N2O etc., and secondly through emission of different aerosols. Current
GHG emissions are approximately 50 Gt CO2 eq. per year, and rising.
Therewithal, oceans and biosphere are still net sinks of the additional CO2, but
the amount of CO2 is accumulating in atmosphere and currently equals approxi-
mately 400 ppmv in standard conditions. In nutshell, although different human
activities can induce warming and cooling effects, the current net impact on the
state of the climate system is substantial warming related to the GHG emissions.
IPCC AR5 presented estimates indicating that in order to constrain anthropogenic
warming to less than 2 �C (relative to 1861–1880) would require cumulative CO2 emissions since 1870 to amount below approximately 3000 GtCO2. At the same
time, by the year 2011, about 2000 GtCO2 was already emitted, strongly controlling
the available time period and the scale of the changes that are needed to be
implemented in order to keep the global mean temperature increase below 2 �C (IPCC 2014). Of course, the most of these estimations are also constrained by the
various uncertainties. However, independent studies indicate the need for rapid and
large-scale upgrade of the existing energy, transport, housing and food production
systems.
Transition to Low-Carbon Society and Hydrogen Economy
Concepts of green economy, low emission development, Hydrogen Economy or
achieving a 100% renewable energy systems became increasingly important after
2008 both in the number of published studies, analyses or papers as well as in the
attention it gained on an international level (Pašičko 2014). It also became clear that
the existing model of economic development needs to change and transition
towards different foundations is needed. There are several reasons that can be
found and understood or that were mentioned in the literature: (1) Economic crisis
that started in 2008 was heavily influenced by the energy crisis (record high prices
of oil and gas) and combined and / or alone resulted in other crises such as food
crisis, political crisis etc; (2) Increased warnings that society is in danger of
transgressing a number of planetary boundaries or ecological limits (Raworth
2012); contrary to economic philosophy that resources come from the market, it
434 A. Đukić et al.
is more and more clear they come from nature. Every incident including a deep oil
drilling is a reminder that harm to society and environment are increasing as fewer
fossil fuels are available; (3) Global warming is becoming more evident while on
the other side there is a clear lack of political decision on the global level to tackle
this issue; (4) Avoid the trap of ‘growing first, cleaning up later’ (Atkisson 2012); (5) Growing pressure from people excluded from economic growth (1.3 billion still
do not have access to the electricity, 2.6 billion do not have access to the sanitation
and 900 million lack access to the clean drinking water); (6) Given the fact that
fossil fuels are still heavily subsidized by governments (Kovacevic 2011), in a
much higher share than renewable energy or energy efficiency, the present eco-
nomic model represents a sort of lock-in against low emission development;
(7) Energy security issues—with higher and higher energy import dependences,
renewable energy and energy efficiency are becoming more and more important.
The term of Green Economy was first coined in 1989 in a pioneering report for
the Government of the United Kingdom by a group of leading environmental
economists, entitled Blueprint for a Green Economy (Pearce et al. 1989). In 2008
the term was revived in the context of discussions on the policy response to
the multiple global crises. The United Nations Environment Programme (UNEP)
introduced Green Economy, which it defines as one that ‘results in improved human well-being and social equity, while significantly reducing environmental risks and
ecological scarcities’ (UNEP 2011). During the financial crisis it inspired several governments to implement signif-
icant ‘green stimulus’ packages as part of their economy recovery efforts. The concept of Green Growth has its origins at the Fifth Ministerial Conference on
Environment and Development (MCED) held in March 2005 in Seoul. 52 Govern-
ments and other stakeholders from Asia and Pacific agreed to move beyond the
sustainable development rhetoric and pursue a path of Green Growth. As with
Green Economy, Green Growth attracted significant attention as a way out of
economic problems in the aftermath of the 2008 financial crisis. Green Growth is
principally a ‘top-down’ approach, driven by government initiatives. It can also be criticized for being ‘green’ in relatively limited ways, but it emerged as a serious and very mainstream alternative to Growth as Usual with both environmental and
social dimensions.
To define Sustainable Development, an international exercise was performed that catalogued, analyzed, and synthesized: written submissions and expert testi-
mony from ‘senior government representatives, scientists and experts, research institutes, industrialists, representatives of non-governmental organizations, and
the general public’ held at public hearings throughout the world, in 1987, the United Nations released the Brundtland Report, that included what is now one of
the most widely recognized definitions: ‘Sustainable development is development that meets the needs of the present without compromising the ability of the future
generations to meet their own needs’ (UNWCED). The concept of Low Carbon Development has its roots in the United Nations Framework Convention on Climate
Change (UNFCCC) adopted in Rio in 1992. In the context of this convention, Low
Carbon Development is now generally expressed using the term Low‐Emission
33 Perspectives of Hydrogen Automotive Applications in Croatia 435
Development Strategies (LEDS). Though no formally agreed definition exists,
LEDS are generally used to describe forward‐looking national economic develop- ment plans or strategies that encompass low‐emission and / or climate‐resilient economic growth.
Whilst the concepts of Green Economy, Green Growth, Sustainable Develop-
ment and Low Carbon Development emerged from different sources, through the
work of different organizations and with different target audiences, the distinctions
among them became blurred and they are now being used almost interchangeably.
A main driver behind the development of these concepts was the move towards a
more integrated and holistic approach to incorporating environment in policies,
economic decision making and planning.
Croatia has recently joined the growing number of countries in the world that
have already started to develop a long-term strategy for low-carbon development
and thereby firmly embarked on the road to sustainable development. The approach
that determines impacts of Hydrogen Economy in the context of low emission
development was the core for the methodology used in this work. The design of the
low-carbon society requires innovative energy systems considering a trans-
disciplinary approach that integrates multi-dimensional elements, related to
the social, economic, and environmental aspects (Nakata et al. 2011). Development
of energy and transportation sector is complex and increasingly often evaluated as a
part of society-biosphere-climate-economy-energy system (Akhtar et al. 2013).
Description of Croatian Power System and Renewable Energy
Croatia is currently importing around 50% of its energy of which 80% is oil.
Almost all electricity generation capacity is in ownership of Croatian Electrical
Utility, HEP Group. From 3993 MW installed, 2056 MW is in hydro, 1589 MW in
thermal power plants and 348 in Croatian part of nuclear power plant Krsko.
Specificity of Croatian power system is large percentage of installed power in
hydro (52%) that requires reserve capacity during summer period when water
level is low. Ever growing electricity consumption is not offset with new generation
capacities and electricity import is rapidly rising. That emphasizes need for new
generation capacities. Currently, LEDS is in progress—with focus up to 2030 and
outlook to 2050.
Hydrogen in Transport
Based on today’s global climate changes, the main goal of this work was to research how new technologies application can help in mitigation of GHG. Due to
the increasing of the GHG concentrations, this work focuses on climate change
analysis, transition of energy, and transportation sector towards low carbon
436 A. Đukić et al.
paradigm. As one of the most critical barriers to achieve 100% renewable energy
system is intermittent nature of renewable energy such as solar and wind, demand
for energy storage becomes important (Moriarty and Honnery 2009; Najjar 2013).
And that’s the point where hydrogen as the great energy carrier can be implemented. This is where the focus of this work was positioned, related to the
transport sector as the highest energy consumer and polluter (Shafiei et al. 2014).
Given the intermittent nature of renewables, energy peaks from wind and solar
energy can be transferred to the hydrogen for later use and / or utilize in transport
sector (Đukić 2015). This also provides more flexibility in the power system network to offset production peaks to energy for use when needed (Cipriani
et al. 2014).
A global trend of population growth leads to the increasing of energy demands,
resulting in decreasing of fossil fuels reserves, increasing of CO2 emission and
increasing of the temperature, respectively. Here is where the transfer to the Hydro-
gen Economy has to be applied. The drivers of Hydrogen Economy in the countries
worldwide are energy safety, climate changes, air pollution, and competitiveness in
the world market (Andrews and Shabani 2012). Hydrogen technologies and their
applications are investigated worldwide, from the aspect of sustainable develop-
ment, cleaner technologies, energy efficiency and energy savings. A transport
sector is the leader of energy consumption and air pollution, the most evident in
urban cities. Due to that hydrogen fuel cells powered vehicles present one of the
rare technologies capable to switch over internal combustion engines vehicles
(Biswas and Thompson 2013). As it is written above importance of involving of
hydrogen fuel cells powered vehicles is recognized not just in Europe but all over
the world. US Department of Energy predicts demands for hydrogen of 150 Mt until
2040 (Hamad et al. 2014). Thus, countries of Asia such as Japan, China, Korea,
India, Malaysia, and Taiwan invest millions dollars to make green transport sector
(Lu et al. 2013). For instance, Japan set the goal to have each new vehicle as
hydrogen fuel cells powered until 2020. In India the goal is to have 1 million
hydrogen fuel cells powered vehicles. A rapid implementation of hydrogen fuel
cells powered vehicles in Asia also started because 13 of 20 the most polluted cities
are located in China (Pudukudy et al. 2014).
The goal of EU is set to be the first Hydrogen based Economy in the world. In
order to realize this plan the list of legislatives has to be set. In other words, EU
country states need to reform their statutes to ensure successful transition to the
hydrogen technologies (Apak et al. 2012). Nowadays EU Commission applied
directive in order to approve hydrogen fuel cells powered vehicles. Furthermore,
EU established platform for hydrogen and fuel cells to encourage the development,
making strategy, and introduction of standards and legislatives. Aside of legisla-
tives, public-private partnership should be highlighted as a step forward in
the financing major projects. These partnerships is going to be applied within
several years. During that time period both parties should invest 470 millions
euros each. As the result, future EU investment in hydrogen technologies will be
around one billions euros.
33 Perspectives of Hydrogen Automotive Applications in Croatia 437
Croatia as a full member of EU should aim to shift to the new technologies as
soon as it can. Meeting this demand the increased investment in hydrogen technol-
ogies is required. Croatia is a touristic country with large amount of motorized
vehicles during the year with trend of double / triple increasing in summer months.
It is important to highlight that hydrogen as a fuel is clean as much as is clean
energy and processes used for its production. To satisfy this claim hydrogen
production via water electrolysis using renewable energy sources is unquestionable
(Đukić and Firak 2011). In Croatia there are around 1.9 millions vehicles. From this number, approximately 1.5 millions belong to the passenger cars. To accomplish
hypothesis of clean and environmentally friendly hydrogen, there were performed
calculations for the systems that include use of solar and / or wind energy,
i.e. photovoltaic cells and / or wind turbines (Nowotny and Veziroglu 2011).
Given results represent directions in the system development based on installed
power of solar and wind energy, taking into account demands for hydrogen
amounts. Conclusions and recommendations are based on analyzing three different
scenarios with hydrogen as the energy storage in Croatia; in what extent can
hydrogen be used as the energy carrier to store excessive energy from intermittent
renewable energy sources. In order to estimate potential savings in CO2 emissions,
in this study some methodological approaches from (Pascala and Socolow 2004)
were applied. These options are related to the improved fuel economy, reduced
reliance on the vehicles and the use of the renewable hydrogen in the transportation
sector.
Methodology
Following potential changes in the transportation system were analyzed in this
study: (1) A fraction of the hydrogen powered vehicles was assumed to be equal
10%, 50 %, and 75% by the year of 2030. Starting fraction of the hydrogen fuel
cells powered vehicles in Croatia was assumed as 0%; (2) The kilometers values
were assumed to be equal 600, 700 or 800 km / 5 kg of H2 by the year of 2030 with
starting kilometers value assumed to be equal 500 km / 5 kg of H2 as an average
value of 500 km that can be traveled by the current generation hydrogen fuel cells
powered vehicles. Total number of scenarios in this set was 9, where all combina-
tions of the fraction of the hydrogen fuel cells powered cars and the average
efficiency were evaluated. It was also applied following 3 constants in this set of
scenarios: the number of the passenger cars was assumed to be equal 1448229 (DZS
2014) and constant by the year of 2030. Also, average number of kilometers
traveled per year was assumed to be equal 11000 km / year and constant in this
set of scenarios, while the average gasoline consumption used to estimate potential
savings was assumed to be equal 10 km / L.
Although various assumptions in this set of scenarios were subject to the various
uncertainties and limitations, they provided simple and realistic framework to
evaluate possible hydrogen production and storage needs in Croatia. In order to
compare hydrogen scenarios in this work to potential savings in the gasoline
438 A. Đukić et al.
consuming cars, next set of scenarios was also evaluated. There were additionally
constructed 9 scenarios based on the following options: (1) The average distance
was assumed to decrease up to the year of 2030. Starting from 11000 km / year,
potential reductions in the gasoline consumptions and reductions in the CO2 emissions, when distance was reduced to the 9000 km, 7000 km or 5000 km per
year, were evaluated; (2) The average distance was assumed to reach 11 km, 15 km
or 20 km per liter by the year 2030. In this set of scenarios the same number of
passenger cars as in the hydrogen scenarios and the same starting average distance
and gasoline consumption were assumed. All changes in the projections
were assumed to vary as a linear function of time, and were estimated on the yearly
time scale. Scenarios were compared in term of the CO2 emission saved by the year
of 2030 and in the year of 2030. Some other details related to the various conversion
factors and comparisons were introduced in the results and discussion sections
where needed.
Results and Discussion
Due to the described methodology, two cases were evaluated. First one was related
to the hydrogen demands till the end of 2030 and second one was related to the
saved gasoline till the end of 2030. Case of hydrogen was consisted of the fraction
of the hydrogen fuel cells powered vehicles (included scenarios 1A: 10%, 1B: 50%
and 1C: 75%), and average efficiency of the fuel cells, i.e. kilometers per 5 kg of
hydrogen (included scenarios 2A: 600, 2B: 700 and 2C: 800). Further discussion of
these scenarios was given in the Table 33.1 with conversion factors included.
In the Fig. 33.1 there is given a projected increase of the hydrogen fuel cells
powered vehicles in Croatia by the end of 2030 (a) and average kilometers range
with 5 kg of hydrogen by the end of 2030.
Due to the average kilometers per 5 kg of hydrogen, Fig. 33.1b presents
projected ranges of 600 km, 700 km, and 800 km. However these approximations
are related to the expected improving of hydrogen storage that allows to have these
ranges. From the Fig. 33.2a it is seen how much hydrogen is needed per year from
the 2015 to the 2030. Related to the hydrogen automotive application, Fig. 33.2b
brings amounts of saved gasoline. Given results promise CO2 emissions reducing.
All Scenarios were compared in term of the CO2 emission saved by the year of
2030. The results are given in the Table 33.2
In the Table 33.3 are given results of calculations for saved gasoline within
Scenarios 1A, 1B, and 1C. Accumulated gasoline not spent / L for Scenario 1A is
1.27� 109 L, for Scenario 1B is 6.37� 109 L, and for Scenario 1C is 9.56Eþ 09 L. Table 33.4 presents data within 6 Scenarios for gasoline of average kilometers
per year and average kilometers per litre started from the 2015 to the end of
the 2030.
To compare savings in CO2 emissions and gasoline, further calculations based
on current needs of gasoline were performed. Figures 33.3a and 33.3b give view
on average kilometers per year and average kilometers per liter of gasoline.
33 Perspectives of Hydrogen Automotive Applications in Croatia 439
Both calculations results were presented in term of accumulated CO2 not released
and accumulated C not spent including 25% overheads.
In the Fig. 33.4 the combined Scenarios included in the Fig. 33.3
were presented that gives overall data of amount of gasoline needed per year.
Results were grouped into 3 additional Scenarios with group of 3 discussed
above. Calculated values of each grouped Scenarios were given in the Table 33.5.
Table 33.1 Hydrogen by the end of the 2030
Starting number of the hydrogen powered cars 0
Starting efficiency of fuel cells (km / 5 kg H2) 500
Number of passenger cars (assumed constant) 1448299
Average kilometers per year (assumed constant) 11000
Average kilometers per litre of gasoline (km / L) (assumed constant) 10
Fraction of hydrogen fuel cells powered vehicles by the end of 2030
Scenario 1A 10%
Scenario 1B 50%
Scenario 1C 75%
Average kilometers (km / 5 kg H2) by the end of 2030
Scenario 2A 600
Scenario 2B 700
Scenario 2C 800
Conversion factors
1 gal of gasoline>X kg of C 2.40
1 L of gasoline>X kg of C 0.63
1 kg of C corresponds to X kg of CO2 3.67
kWh needed in the electrolyzer to get 1 kg of H2 52.5
Peak power output produced by a windturbine (MWp) 3
Peak power output produced by a photovoltaic array (MWp) 0.01
Capacity factor for the windturbine 30%
Capacity factor for the photovoltaic cells 15%
1,200,000 900 800 700 600 500 400 300 200 100
0
1,000,000
800,000
600,000
400,000
200,000
0
20 10
20 15
20 20
20 25
Year
a b
N u
m b
er o
f h
yd ro
g en
f u
el c
el ls
p o
w er
ed v
eh ic
le s
A ve
ra g
e ki
lo m
et er
s p
er 5
k g
o f
h yd
ro g
en
20 30
20 35
20 10
20 15
20 20
20 25
Year
20 30
20 35
Scenario 1A
Scenario 1B
Scenario 1C
Scenario 2A
Scenario 2B
Scenario 2C
Fig. 33.1 Hydrogen fuel cells powered vehicles: 10 %, 50 %, and 75% (a); Average kilometers per 5 kg of hydrogen (b)
440 A. Đukić et al.
The main Scenarios studied within this work were based on the hydrogen and
gasoline calculations. Results give good directions to the shift to the hydrogen fuel
cells powered vehicles. A stronghold is basically in high CO2 saving as well as
savings in fuel cell consumption. Hence, as a very rich with renewables such as
solar and wind energy, Croatia has a good potential to follow trends of Hydrogen
based Economy what gives tailwind to its transport sector.
a b 1.20E+08
1.00E+08
8.00E+07
6.00E+07
4.00E+07
2.00E+07
0.00E+00
20 10
20 15
20 20
20 25
Year
A m
o u
n t
o f
h yd
ro g
en n
ee d
ed p
er ye
ar \
kg
20 30
20 35
Scenario: 1A+2A
Scenario: 1A+2B
Scenario: 1A+2C
Scenario: 1B+2A
Scenario: 1B+2B
Scenario: 1B+2C
Scenario: 1C+2A
Scenario: 1C+2B
Scenario: 1C+2C
1.40E+09
1.20E+09
8.00E+08
1.00E+09
6.00E+08
4.00E+08
2.00E+08
0.00E+00
A m
o u
n t
o f
sa ve
d g
as o
lin e
/L
20 10
20 15
20 20
20 25
Year
20 30
20 35
Scenario 1A
Scenario 1B
Scenario 1C
Fig. 33.2 Amount of hydrogen needed per year (a); Amount of saved gasoline (b)
Table 33.2 Amount of H2 needed per year (kg)
Scenario 1Aþ 2A 1Aþ 2B 1Aþ 2C Accumulated H2 (1000 t) 112.23 100.53 91.22
2030 - demand for H2 (1000 t) 13.28 11.38 9.96
Electricity needed in 2030 for H2 production (MWh) 696.994 597.423 522.745
Installed power of the windturbines needed in 2030
(MW)
265.2 227.3 198.9
Installed power in the photovoltaic array needed in
2030 (MW)
530.4 454.6 397.8
Scenario 1Bþ 2A 1Bþ 2B 1Bþ 2C Accumulated H2 (1000 t) 561.13 502.64 456.08
2030 - demand for H2 (1000 t) 66.38 56.90 49.79
Electricity needed in 2030 for H2 production (MWh) 3484969.47 2987116.69 2613727.10
Installed power of the windturbines needed in 2030
(MW)
1,326.1 1,136.6 920.9
Installed power in the photovoltaic array needed in
2030 (MW)
2,652.2 2,273.2 1,841.8
Scenario 1Cþ 2A 1Cþ 2B 1Cþ 2C Accumulated H2 (1000 t) 841.70 753.97 684.13
2030 - demand for H2 (1000 t) 99.57 85.35 74.68
Electricity needed in 2030 for H2 production (MWh) 5227454.20 4480675.03 3920590.65
Installed power of the windturbines needed in 2030
(MW)
1989.1 1705 1491.8
Installed power in the photovoltaic array needed in
2030 (MW)
3978.2 3410 2983.7
33 Perspectives of Hydrogen Automotive Applications in Croatia 441
Table 33.3 Amount of gasoline saved in Scenarios 1A, 1B, and 1C
Scenario 1A 1B 1C
Accumulated gasoline not spent (L) 1.27Eþ 09 6.37Eþ 09 9.56Eþ 09 Accumulated C not spent (kg) 8.08Eþ 08 4.01Eþ 09 6.02Eþ 09 Accumulated C not spent (kg)þ 25% overheads 1.01Eþ 09 5.02Eþ 09 7.53Eþ 09 Accumulated C not spent (1000 t)þ 25% overheads 1010.06 5018.36 7527.53 Accumulated CO2 not released (1000 t)þ 25% overheads
3706.94 18417.37 27626.05
2030 - not released CO2 (1000 t)þ 25% overheads 463.37 2316.84 3475.25
Table 33.4 Gasoline by the end of 2030 (Mt CO2¼ 3.71Eþ 00 for the 2015) Number of passenger cars (assumed constant) 1448299
Starting average kilometers per year 11000
Starting average kilometer per liter of gasoline (km / L) 10
Average kilometers per year by the end of the 2030
Scenario G1A 9000
Scenario G1B 7000
Scenario G1C 5000
Average kilometers per liter of gasoline (km /L) by the end of the 2030
Scenario G2A 11
Scenario G2B 15
Scenario G2C 20
Conversion factors
1 gal of gasoline>X kg of C 2.40
1 L of gasoline>X kg of C 0.63
1 kg of C corresponds to X kg of CO2 3.67
12,000
10,000
8,000
6,000
4,000
2,000
0A ve
ra g
e ki
lo m
et er
s p
er y
ea r
A ve
ra g
e ki
lo m
et er
s p
er li
tr e
o f
g as
o lin
e
Scenario G1A
Scenario G1B
Scenario G1C
Scenario G2A
Scenario G2B
Scenario G2C
20 10
20 15
20 20
20 25
Year 20
30 20
35 20
10 20
15 20
20 20
25
Year 20
30 20
35
25.00
20.00
15.00
10.00
5.00
0.00
a b
Fig. 33.3 Average kilometers per year: 9000, 7000, and 5000 km (a); Average kilometers per liter of gasoline: 11 km, 15 km, and 20 km (b)
442 A. Đukić et al.
Conclusions and Future Work
Croatia as a touristic country has a great potential for hydrogen automotive appli-
cation. The number of motorized tourists is rapidly increasing during summer
months. This fact opens enough room to the hydrogen fuel cell powered vehicles
shift starting with 10%, 50%, and 75% up to the end of the 2030. Due to the EU
directives flows of hydrogen powered vehicles should be set for every 300 km.With
G as
o lin
e n
ee d
ed p
er y
ea r/
L
1.20E+09 1.40E+09 1.60E+09 1.80E+09
1.00E+09 8.00E+08 6.00E+08 4.00E+08 2.00E+08 0.00E+00
20 10
20 15
20 20
20 25
Year 20
30 20
35
Scenario: G1A+G2A
Scenario: G1A+G2B
Scenario: G1A+G2C
Scenario: G1B+G2A
Scenario: G1B+G2B
Scenario: G1B+G2C
Scenario: G1C+G2A
Scenario: G1C+G2B
Scenario: G1C+G2C
Fig. 33.4 Amount of gasoline needed per year
Table 33.5 Gasoline needed per year (L)
Scenario G1AþG2A G1AþG2B G1AþG2C Accumulated gasoline not spent (L) 3.36Eþ 09 6.52Eþ 09 9.13Eþ 09 Accumulated C not spent (kg) 2.13Eþ 09 4.13Eþ 09 5.79Eþ 09 Accumulated C not spent (kg)þ 25% overheads 2.66Eþ 09 5.17Eþ 09 7.23Eþ 09 Accumulated C not spent (1000 t)þ 25% overheads
2664.48 5167.12 7234.84
Accumulated CO2 not released (1000 t)þ 25% overheads
9778.63 18963.33 26551.85
Scenario G1BþG2A G1BþG2B G1BþG2C Accumulated gasoline not spent (L) 5.53Eþ 09 8.26Eþ 09 1.05Eþ 10 Accumulated C not spent (kg) 3.51Eþ 09 5.24Eþ 09 6.68Eþ 09 Accumulated C not spent (kg)þ 25% overheads 4.38Eþ 09 6.55Eþ 09 8.35Eþ 09 Accumulated C not spent (1000 t)þ 25% overheads
4383.50 6545.02 8347.89
Accumulated CO2 not released (1000 t)þ 25% overheads
16087.43 24020.21 30636.75
Scenario G1CþG2A G1CþG2B G1CþG2C Accumulated gasoline not spent (L) 7.70Eþ 09 1.00Eþ 10 1.19Eþ 10 Accumulated C not spent (kg) 4.88Eþ 09 6.34Eþ 09 7.57Eþ 09 Accumulated C not spent (kg)þ 25% overheads 6.10Eþ 09 7.92Eþ 09 9.46Eþ 09 Accumulated C not spent (1000 t)þ 25% overheads
6102.51 7922.92 9460.94
Accumulated CO2 not released (1000 t)þ 25% overheads
22396.23 29077.10 34721.65
33 Perspectives of Hydrogen Automotive Applications in Croatia 443
area of 56594 km2 (89810 km2 with associated coastal see) starting point
was suggested to be installation of hydrogen refueling stations along the seaside.
With seaside of 1777 km (over 6000 km including islands) number of demanded
hydrogen refueling stations was calculated to be 6. Hydrogen production technol-
ogy is water electrolysis using solar energy installed on-site during transition period
of infrastructure construction. Obtained results are talking of 27626.05 accumulated
CO2 not released (1000 tones) plus 25% overheads. Energy needed for fuel cells
was calculated as it comes from renewable energy—wind power plants (3 MW each
unit, with 30% capacity factor) and PV systems installed on the roof (10 kW each,
15% capacity factor). However, methodology used in this work can be easily
applied in every country for calculations of demands, taking into account total
number of internal combustion engines vehicles. Future work of the authors will be
adjusted by changing the time horizon from the year of 2030 to the year of 2050. It
will produce two additional sets of Scenarios each including nine of them.
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33 Perspectives of Hydrogen Automotive Applications in Croatia 445
Part IX
Energy Technologies and Their Effect on Global Warming
Fossil Fuels and Climate Change
Chapter 34
Contribution to Multi-Criteria Evaluation of the Impacts of Air Pollution: Case of Cement Plant (Ain Touta- ALGERIA)
Lylia Bahmed, Samia Daas, Mourad Chebila, and Loubna Khadoudja Aggabou
Introduction
The implementation of a strategy or an Environmental Management Plan (EMP), to
minimize air pollution that results from the manufacture of a product, fall within the
scope of the EMS policy of most of the cement companies in Algeria, and in
accordance with the requirements of the ISO14001 standard (Hariz and Bahmed
2013; Bahmed et al. 2009), in terms of improving their EMS, and depending on the
environmental context and legal restrictions that subject the companies regarding
the dust releases’ limits and their technical capacity to address the problems of air pollution (Hariz 2009).
In this article and after presenting the proposed methodology for the quantitative
assessment of the impacts of air pollution of cement by means of a multi-criteria
approach, a state of play on the life cycle of the cement product modeled by the
SADT method of the process of the cement plant of Ain-Touta, and its environ-
mental impacts will be quantified by the AHP method before concluding on the
prospects and expectations from this study.
L. Bahmed (*) • S. Daas • M. Chebila • L.K. Aggabou Laboratory of Research in Industrial Prevention- Industrial Health and Safety Institute,
University of Batna 2, Batna, Algeria
e-mail: [email protected]; [email protected]; [email protected]; loubna.
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_34
451
Method and Material
This study allows the proposition of a first perspective of the different actions
required to implement an effective management of the EMS. These objectives
constitute the indices that permit the assessment and evaluation of the impacts of
air pollution related to the manufacturing of a product.
Proposed Methodology
LCA is a global approach standardized according to the ISO 14040 standard, which
quantifies the impacts of a product. LCA encrypts the impacts of each component of
the product from the extraction of raw materials to the end of the cycle. The final
result is presented according to the specific impacts on climate change, human
health, ecosystems and non-renewable resources (ISO 14044 2006).
The phase of the LCA and its standardized methodology and high precision, is
an internationally recognized tool for decision support, it allows the reduction of the
impacts of the new products on the environment, the identification of what can be
improved in the already existing products, avoiding the improvement of an aspect
that creates more serious problems to another stage of the product’s life and the comparison of the environmental performances of products with the same utility
(Fig. 34.1).
In order to evaluate the environmental impacts associated with the manufacture
of cement, we have chosen the multi-criteria approach to decision support AHP,
taking into account the product life cycle and at the same time the two steps of the
LCA method (Bouhidel 2009): evacuation of the environmental impacts and
interpretation of the results.
The articulation of these tools in a methodological approach is of great impor-
tance especially for the quantitative evaluation of the environmental impacts.
Interpretation
Definition of the objectives and the
field of study
Inventory analysis
Impacts evaluation
Direct applications:
- Development and improvement of products - Strategic planning - Public policies - Marketing
Fig. 34.1 Framework of a LCA according to ISO 14040 (2006)
452 L. Bahmed et al.
Hence, the major stages of the proposed methodology are based on the multi-
criteria approach to decision support (Fig. 34.2).
The Analytic Hierarchy Process (AHP) method of T.L. Saaty (1994) was
developed in the 70 to facilitate the decision making in the complex situations
using a structured approach (Rousval and Bouyssou 2009). The AHP method takes
into consideration qualitative and quantitative criteria. This method is simple to use,
very flexible, as it is a computerized method by software called Expert Choice.
The AHP method consists of representing a decision problem for evaluating the
impacts of air pollution by a hierarchical structure reflecting the interactions
between the various phases of the life cycle of cement, then to make paired
comparisons of the criteria of the evaluations of the hierarchy, and finally to
determine the priorities of the environmental impacts.
Presentation of the AHP Method
The multi-criteria hierarchy method (MHM) or Analytic Hierarchy Process (AHP)
of T.L. Saaty (1994) was developed in the 70s to facilitate the decision making in
the complex situations using a structured approach (Aull-Hyde et al. 2006). The
AHP method allows taking into account qualitative and quantitative criteria. This
method is simple to use, very flexible, as it is a computerized method by software
called Expert Choice. Actually, several steps compose the AHP method. These
steps are sequentially detailed hereinafter.
• Step 1: Hierarchical decomposition of the complex problem into simple elements.
This essential step aims to pose the problem to be solved, to position it in its
environment in order to accurately identify its various aspects and features and
Fig. 34.2 The proposed methodology
34 Contribution to Multi-Criteria Evaluation of the Impacts of Air Pollution. . . 453
also to identify the stakeholders or experts of the decision-making process
(Fig. 34.3).
• Step 2: Comparison of criteria by means of binary comparison matrix.
The preferences of experts reflecting the relative importance between the criteria
are expressed by the weights ajj resulting from pair-wise comparison matrices between the criteria of the same hierarchical level according to a scale of
linguistic ratio. The aggregation and evaluation of weights is done from the
roots to the leaves according to a principle that akin to a weighted sum.
Configure a reciprocal square matrix formed by the evaluations of the weight
ratios N∗Nð Þ where, N represents the number of the compared elements. In this way, we obtain:
a ¼ aijWithajj ¼ 1
Let A ¼ aij to be a pair-wise comparison matrix:
A ¼ a11 a12 a1n a21 a22 a2n an1 an2 ann
0 @
1 Aaij ¼ 1
aji ,8i, j ¼ 1, 2, ::::n
The values of aij can be determined through the scale of Saaty (Table 34.1.).
Fig. 34.3 Hierarchical structure of the problem (Aull-Hyde et al. 2006)
454 L. Bahmed et al.
The reciprocal comparison according to (Saaty 1994) can be:
– Favorable and positive, the appreciation will correspond to an integer value.
– Unfavorable and therefore negative, the appreciation will be expressed using
a fraction.
• Step 3: Determine the relative importance of the criteria.
The determination of the elements’ priorities of each matrix is done by solving the eigenvector problem. The relative importance of the different criteria is
expressed by the values of the normalized vector that is equal to 1.
So the priorities are determined by solving a system of equations (Saaty
1994):
A:w ¼ λmax:w ð34:1Þ
Where:
A: is the comparison matrix of dimension N∗Nð Þ. w ¼ w1,w2, :::::::::wnð Þ Is an eigenvector of dimension N∗1 associated with
the eigenvalue.
λmax: The maximum Eigen value of the matrix. Therefore,
A:w ¼ λmax:w ) A:w ¼ Xn j¼
aij:wj
" # ,8i ¼ 1, :::::n ð34:2Þ
Then, we obtain:
λmax ¼ 1 n : Xn i¼1
Xn j¼1
aij: wj wi
ð34:3Þ
This step of the appreciations’ collect is the most controversial. Indeed, a major criticism pronounced towards AHP method concerns the scale of judg-
ment on the lack of consideration of the uncertainty in the opinions and percep-
tions of experts (Vincke 1998).
• Step 4: Consistency of judgments.
Table 34.1 Weighting scale of the AHP method (Saaty and Hu 1998)
Numerical scale Verbal scale
1 Importance equals to the two elements
3 One element is a little more important than the other
5 An element is more important than the other
7 An element is much more important than the other
9 An element is absolutely more important than the other
2, 4, 6, 8 Intermediate values between two judgments used to refine the judgment
34 Contribution to Multi-Criteria Evaluation of the Impacts of Air Pollution. . . 455
The obtained answers often exhibit some degree of inconsistency. The method
does not require that judgments neither be consistent nor transitive, contrariwise
the method to define an index of consistency IC (Saaty and Hu 1998).
IC ¼ λmax � 1 n� 1 ð34:4Þ
Where:
λmax: is the maximal eigenvalue corresponding to the matrix of pair-wise comparisons.
n: number of the compared elements.
The ratio of coherence can be interpreted as the probability that the matrix is
completed randomly. The ratio of coherence is given by the following formula:
RC ¼ IC IA
ð34:5Þ
Where:
RC: is the ratio of coherence. IA: is a random index. IC: is the index of coherence (Table 34.2). The overall coherence of appreciation is evaluated using the ratio of coher-
ence RC. Still according Saaty, the value of this latter must be at most equal to
10%.
In the case where this value exceeds 10%, the appreciations may require some
revisions.
• Step 5: Establish the relative performance of each criterion.
This last step aims to assign a performance rating for each action Pai, which will be multiplied by a weighting coefficient wi. The sum over n actions gives an aggregated performance results expressed in an overall rating (Saaty 1994):
Pci ¼ Xn i¼1
Paji � wi ð34:6Þ
Where:
Pci: Rating of performance for the criterion cj. Paji: Rating of performance for the action ai of the criterion cj. wi: Weighting coefficient for the action ai of the criterion cj.
Table 34.2 Table of the acceptable coherency’s ratios (Saaty 1994)
Size of the matrix (n) Ratio of the acceptable coherence
3 0.05
4 0.08
5 et þ 0.10
456 L. Bahmed et al.
Application of the Methodology
Our case study is applied to the life cycle of cement manufacturing of the cement
plant Ain-Touta Batna.
The application of the SADT method allows us to model the cement life cycle
and determine its major phases and their interactions (Fig. 34.4).
This method facilitates the passage of the environmental impacts’ evaluation during the analysis of the life cycle of the cement product, by the application of
normative LCA methods and AHP method.
This method facilitates the passage of the environmental impact evaluation in
the analysis of the life cycle of the cement product, by the application of normative
LCA methods and the AHP method.
The characterization of environmental impacts in the cement plant of Ain Touta
results in an approach which consists of developing the hierarchical structure of our
multi-criteria system (Fig. 34.5).
Three criteria are determined; the extraction of raw materials, cement
manufacturing and transport of cement. Each criterion is defined by several
sub-criteria, and each sub-criterion is divided into three alternatives (air pollution,
soil pollution and depletion of the natural resources).
The evaluation of the overall environmental impacts in the cement plant of Ain
Touta implies an evaluation of the impacts of the extraction, manufacturing,
transport of cement, and each criterion has sub criteria. Three types of impacts
Citizens
Sa
Robot
Truck
Control room
Clinker crusher
Oven
Crusher at raw
Worker
Borehole’s engines
Hammer crusher
Cement use
Cement transport
Cement manufacturing
Extraction of RM
A1
A2
A3
A4
End of life
Dust
Waste
Dust
CO2 Clinker’s waste
Dust Heat
Noise
Noise
Dust
Cement
Cement
R.M cracked
R.M
Explosive
Weight control
Dater Cement quantityTemperature
Pressure
Standards of manufacturing
1000 t/h (clay)
500 t/h (limestone) Quality
control
Fig. 34.4 Phase of the life cycle by the method SADT
34 Contribution to Multi-Criteria Evaluation of the Impacts of Air Pollution. . . 457
(air pollution, soil pollution and depletion of the natural resources) were selected as
alternatives.
In order to evaluate the environmental impacts of cement in the cement plant of
Ain Touta, a survey was conducted to consolidate the various opinions of the
judgment of the services’ heads of the different specialties of the cement plant of Ain Touta (SCIMAT 2015).
The table below presents the results of the evaluation of the environmental
impacts related to the cement product by means of the decision support multi-
criteria AHP method (INERIS, 2009).
Results and Discussion
The main objective of this study is to evaluate the environmental impacts related to
the manufacture of cement. Several steps compose the AHP method. These steps
will present the results obtained using the Expert Choice software, through the
cement life cycle. Therefore, The obtained results using the AHP method
(Table 34.3) revealed that the highest pollution levels at the manufacturing stage
in which we must take all preventive and corrective measures to reduce this critical
Fig. 34.5 Hierarchical structure for the evaluation of the environmental impacts in the cement plant of Ain touta
458 L. Bahmed et al.
and significant rate (65% atmospheric pollution). Pollution level of other steps
(extraction of raw materials and transport of cement) is not negligible, but remains
less than that of manufacturing.
Sensitivity analysis is a good tool that allows us to validate the robustness of an
environmental decision. To do this, we can change the weight of our criteria to
determine the limits of our best choice. This permits us to check the shift thresholds
of our results regarding the importance of our criteria. The Expert Choice software
skillfully synthesizes the results by graphics of weights of life phases and the
associated impacts.
The Fig. 34.5 illustrates hierarchical structure for the evaluation of the environ-
mental impacts in the cement plant of Ain touta, through analysis of the life cycle.
The Fig. 34.6 illustrates the performance graph in the basis of the final eigen-
vectors of the three impacts per cycle phase, we notice that the alternative of
winning solution is either, the “air pollution” before the resources depletion and
soil pollution at all stages of the life cycle of the cement except the phase
“extraction of RM” where we can see that “transport of cement” has less impact
on the environment in the same criterion performances better than the others.
Conclusion
The main objective of this study is the evaluation of the environmental impacts of
different life cycle’s phases of cement of the cement plant of Ain-Touta Batna. For this, we have applied the LCA method combined with the method of multi-criteria
hierarchy AHP which allows the quantification of the different categories of
environmental impacts of the cement product, particularly when the software
Expert Choice is used (www.expertchoice.com 2015).
The results of the application of LCA and AHP method in this study show that
the environment is seriously threatened by the environmental impacts. It is affected
Table 34.3 The obtained results using the AHP method (SCIMAT 2015)
Phase of the cement life cycle
Criteria of the hierarchy Results
Extraction of raw materials Felling 32% Atmospheric pollution 48% Soil pollution
20% Depletion of natural
resources
Transport of MP
Crushing
Storage of MP
Cement manufacturing Raw grinding 65% Atmospheric pollution 23% Depletion of natural
resources
12% Soil pollution
Baking
Cement grinding
Transport of cement Bagging 38% Soil pollution 55% Atmospheric pollution
7% Depletion of natural resources Expedition
34 Contribution to Multi-Criteria Evaluation of the Impacts of Air Pollution. . . 459
by the impacts of air pollution generated throughout the different stages of the life
cycle of the cement such as the phase of cement manufacturing and this in the
sub-step of raw grinding of semi finished product, extraction in the sub-step of
felling of raw materials and the sub-step of bagging the cement.
Therefore, special attention should be paid to these problems:
From an environmental viewpoint and for the problem of air pollution, the
current remedy is to ensure the capture of dust during the cement manufacturing
phase to reduce dust levels released into the air, in order to avoid environmental
problems.
Despite the fact that many of the dust collection techniques such as the electro-
bag filters are implemented, unfortunately they are ineffective. For this reason, it is
necessary to proceed preventive maintenance plans, to make the best environmental
decision as well as the regulatory compliance.
The regulatory texts play a key role in this area, which will require companies to
take serious decisions about the environment. Therefore, to improve the conserva-
tion of the environment and to respect the principles of the sustainable develop-
ment, the strategic environmental planning must be implemented to meet the needs
of green products and also the needs of the future generations.
The study has allowed us to expand our knowledge on methods and tools for
assessment of environmental impacts related to air pollution from cement plants,
based on a multi-criteria evaluation and analysis of the life cycle by method SADT,
which has allowed us to develop an original analytical approach on the basis of
which we will in future perspective make further quantitative assessments.
Fig. 34.6 The final eigenvectors of the three impacts per cycle phase
460 L. Bahmed et al.
References
Aull-Hyde, R., Erdogan, S., & Duke, J. M. (2006). An experiment on the consistency of aggre-
gated comparison matrices in AHP. European Journal of Operational Research, 171, 290–295. Bahmed, L., Djebabra, M., Boubakeur, L., & Boukhalfa, A. (2009). Implementing the ISO 14001
certification—an empirical study of an Ajgerian company in the process of certification.
Journal of Management of Environmental Quality: An International Journal, 20(2), 155–164. Emerald Group Publishing Limited ISSN 1477-7835.
Bouhidel, M. (2009). Application d’analyse du cycle de vie (ACV) pour un développement durable: cas des cimenteries Algériennes. Mémoire de Magister. Institut d’Hygiène et Sécurité Industrielle, Université Hadj Lakhdar de Batna.
Hariz, S. (2009). Etude critique du système de management environnemental au niveau des
entreprises Algériennes, Mémoire de Magister, Institut d’Hygiène et Sécurité Industrielle, Université Hadj Lakhdar de Batna.
Hariz, S., & Bahmed, L. (2013). Assessment of environmental management system performance
in the Algerian Companies Certified ISO 14001. Management of Environmental Quality: An International Journal, 24(2), 228–243. Emerald Group Publishing Limited ISSN 1477-7835.
INERIS. (2009). Panorama des méthodes d’analyse multicritère comme outils d’aide �a la décision. ISO 14040. (2006). Environmental management: Life-cycle assessment. Principles and frame-
work. International Organization for Standardization.
ISO 14044. (2006). Environmental management: Life-cycle assessment. Requirements and guide-
lines. International Organization for Standardization.
Rousval, B., & Bouyssou, D. (2009). De l’aide multicritère �a la décision �a l’aide multicritère �a l’évaluation Un cadre et une application aux transports et �a l’environnement. Cahier du Lamsade. (p. 293).
Saaty, T. L. (1994).Décider face �a la complexité—Une approche analytique multicritères d’aide �a la décision. Paris: Collection Université-Entreprise, Entreprise Moderne d’Edition. 232p.
Saaty, T. L., & Hu, G. (1998). Ranking by eigenvector versus other method in the analytic
hierarchy process. Applied Mathematics Letters, 11(4), 121–125. SCIMAT. (2015). Technical report. Algeria: Cemet Plant Ain Touta. Vincke, P. (1998). L’aide multicritères �a la décision. Editions de l’université de Bruxelles,
Editions Ellipses, 179 p. www.expertchoice.com. Retrieved February 12, 2015.
34 Contribution to Multi-Criteria Evaluation of the Impacts of Air Pollution. . . 461
Chapter 35
Environmental Impact Assessment of Electricity Production, A Case Study of Turkey
Fatih Yılmaz, M. Tolga Balta, Reşat Selbaş, and Do�gan Demiral
Introduction
Energy has significant effects in the evolution of economy and technology.
Electricity was the major actor during the transition from the industrial to the
technological revolution, almost all the financial and economic activities depend
directly on it and any development coincides with an increasing demand of electric
energy. Recent year’s electricity energy majority is produced from fossil fuels. Fossil fuels have historically been the world’s primary source of energy and will continue to dominate the world in the next few decades. Combustion of fossil fuels
results in carbon dioxide (CO2). The bigger contributor to global warming from
fossil fuel combustion is CO2. In recent years, the problem of air pollution has
reached limits of remarkably dangerousness both for the environment and human
health (Nicoletti 2001; Churchill 1997). Greenhouse gases are causing climate
change and increasing the world’s average temperatures. Electricity production accounts for 32% of total global fossil fuel use and
around 41% of total energy-related CO2 emissions. Improving the efficiency with
which electricity is produced is therefore one of the most important ways of
F. Yılmaz (*) Department of Energy, Vocational School of Technical Sciences, Aksaray University, Aksaray
68100, Turkey
e-mail: [email protected]
M.T. Balta • D. Demiral
Department of Mechanical Engineering, Faculty of Engineering, Aksaray University, Aksaray
68100, Turkey
R. Selbaş
Department of Energy Systems Engineering, Faculty of Technology, Suleyman Demirel
University, Isparta 32100, Turkey
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_35
463
reducing the world’s dependence on fossil fuels, thus helping both to combat climate change and improve energy security (IEA 2007).
Fossil fuel comprises from coal, natural gas, petroleum shale oil and bitumen.
They all contain carbon. Coal usage of for a long time to generate heat and electrical
energy. But natural gas since 19985 year, it has been usage for heat and electrical
energy in Turkey.
Currently, Turkey is turn into utilizing electric power in a clean energy resource
because of the coal-based thermal power with the high occurrence of environmental
pollution. Figure 35.1 shows the electricity generation mix in Turkey from 1970 to
2010.
An increase in the use of hydropower, renewable energy, and natural gas has
been observed over the years in Fig. 35.1.
When examining the literature, several studies are available. Mukhopadhyay and
Forssell 2005, stated that empirical investigation of air pollution from fossil fuel
combustion and its impact on health in India during 1973–1974 to 1996–1997. The
study categorizes the changes in the amount of CO2, SO2 and NOx emissions into
four factors: the pollution intensity or eco-efficiency, technology or input-mix,
composition of final demand, and the level of final demand. The main factors for
these changes were the pollution intensity, technology, and the volume of final
demand. A number of studies concentrate on energy and environment (greenhouse
gas emissions) by applying input–output structural decomposition analysis. Lin and
Chang 1996, used the divisia index approach to examine emissions of CO2, NOx and SO2 from major economic sectors in Taiwan during 1980–1992. They found
that economic growth had the greatest impact on the variation of emission intensi-
ties during this period, while the influence of fuel mix was limited.
1970
70.000
Lignite Other termal Hydraulic + Renewable Natural gas
60.000
50.000
40.000
30.000
20.000
10.000
0 1980 1990
Years
P o
w er
( M
W )
2000 2010
Fig. 35.1 Electricity production in Turkey from 1970 to 2013 (TEİAS 2015)
464 F. Yılmaz et al.
Zhang 2000, analyzed the relationships of fuel mix, energy saving, economic
productivity and population expansion to the increase of China’s CO2 emissions during 1980–1997. Paul and Bhattacharya 2004, clear that, paper selected pollution
coefficient, energy intensity, structural changes and economic activity as primary
input to identify the major factors affecting the energy-related CO2 emissions from
the major economic sectors in India from 1980 to 1996. Their results showed that
economic growth was the most important component of CO2 emissions.
Wier 1998, illustrate that paper explores the anatomy of Danish energy con-
sumption and emissions of carbon dioxide (CO2), sulphur dioxide (SO2) and
nitrogen oxides (NO2). Changes in emissions between 1966 and 1988 were inves-
tigated using input-output structural decomposition analysis. Hayami et al. (1993),
stated that paper estimation of air pollutions and evaluating CO2 emissions from
production activities: using Japan’s 1985. The aim of this research is to extend the input-output tables for environmental analysis in the most detailed classification
possible. It can also be shown that it plays an important role in evaluating accurately
the emissions of CO2, NOx and SOx.
Liaskas et al. (2000), stated that his paper aims at identifying the factors that
have influenced changes in the level of industrial CO2 emissions. By means of an
algebraic decomposition method the observed changes are analyzed into four
different factors: output level, energy intensity, fuel mix and structural change.
The application study refers to the industrial sector of European Union countries.
Proops et al. (1996), illustrate that paper examines the UK economy wide, lifecycle
implications of eight forms of electricity generations for the emission of three air
pollutants, CO2, SO2 and NO, The lifecycle of the generating stations is considered
in three phases: construction, operation and decommissioning.
Felix and Grewal (2012), stated that environmental assessment of electricity
production in Tanzania. They paper presents the environmental assessment of the
centralized grid-connected electricity production in Tanzania using a life cycle
approach for the years 2000, 2015, 2020, 2026 and 2030, according to the Tanzania
Electricity Supply Company Limited, TANESCO’s, plans for power system expan- sion (power system master plan of the year 2009). The results of their study show
that in all the chosen impacts categories, based on the absolute annual electricity
production, environmental impacts increase significantly with time when compar-
ing the years 2000, 2015, 2020, 2026 and 2030.
Kim 2007, illustrated that evaluation of negative environmental impacts of
electricity generation: Neoclassical and institutional approaches. This paper
focuses on three dimensions: theoretical and methodological backgrounds; critical
review of specific studies: methodologies, results, and limitations; and discussing
their results and implications for environmental policy and further research.
In the literature research is understood that in the Turkey almost isn’t on this topic. This study focuses on the environmental impacts associated with the atmo-
spheric emissions and other wastes that are produced from fossil fuels from elec-
tricity generation. And also a case study is presented for Turkey from 1975 to
2011, according to the TUİK (2015) data.
35 Environmental Impact Assessment of Electricity Production, A Case Study. . . 465
Materials and Methods
The world energy demand has increased rapidly during the last decades with the
increase in the industrialization and population (Balta and Eke, 2011). There has
been a continuous increase in the utilization of electricity produced from consump-
tion of fossil fuels, which further causes several problems such as increased CO2 emissions mainly from fossil fuel combustion products and leads to the global
problems. The ongoing growth in fossil fuels consumption suggest that global
carbon dioxide emission are still rising (Yilanci et al. 2008) The combustion of
fossil fuels for generating electricity is the largest source of CO2 emissions.
The environmental impacts associated with the electricity generated and sup-
plied in Turkey from 1975 to 2011 were evaluated and compared for comparison
purposes. This study mainly focused on the assessment of Turkey’s electricity
production. Electricity production from fossil fuels such as coal, liquid fuels and
natural gas are considered, in this study. Table 35.1 illustrates that between 1975
and 2011 year’s electricity production and energy resource in Turkey.
Table 35.1 1975–2011 years electricity production and shares by energy resources in Turkey (TUIK 2015)
Years Coal (TJ)
Liquids Fuel (TJ)
Natural gas (TJ)
Hyro (TJ) Renewable energy (TJ)
1975 36.97964 55.30073 0 22.98182 3.936996
1976 38.99764 55.52474 0 32.58676 2.961846
1977 44.05023 70.68396 0 33.37282 4.07187
1978 50.0567 68.6559 0 36.35603 2.346408
1979 57.97163 58.00001 0 40.0545 2.432376
1980 53.6256 59.93918 0 44.20157 2.5137
1981 55.29219 59.48907 0 49.06492 1.776456
1982 58.06922 61.02287 0 55.17809 0
1983 77.28262 76.31782 0 44.16579 0
1984 91.19911 72.24292 0 52.30134 0.551052
1985 135.1993 72.675 0.447913 46.87466 0
1986 175.055 71.67964 8.833058 46.18864 0.71451
1987 158.8724 56.42766 16.54605 72.49374 0.798354
1988 112.4347 34.01581 21.06956 112.7535 0.864882
1989 182.2025 43.78482 62.33182 69.87304 0.936774
1990 181.7783 40.73699 66.65951 90.0216 1.035774
1991 194.1126 33.99682 82.40829 88.38891 2.168856
1992 221.2185 53.89246 70.95913 103.5169 2.424312
1993 213.8956 53.00891 70.52656 132.1264 2.657088
1994 253.7633 57.05444 90.21792 119.176 2.819592
1995 252.2725 59.28791 108.3781 138.2832 6.209784
1996 274.0563 67.1566 112.3744 157.6334 5.122548
1997 304.9298 73.12737 144.6751 154.7649 7.437312
(continued)
466 F. Yılmaz et al.
The Table 35.2 is given from combustion resulting factor GHG emission values.
It is clear that from the Table 35.2 coal of CO2 emission is much higher than liquid
fuels and natural gas. Therefore, if we want to reduce GHG emissions, we should
decrease the usage of coal.
GHG emission values which are given in Table 35.2, used for calculating the
CO2, CH4 and NOx emissions in Table 35.3. The average values are used [14-16],
while calculating the CO2, CH4 and NOx emissions.
Table 35.3 illustrates that the electricity production emission values from 1975
to 2011 in Turkey. It is obviously seen that CO2 emissions are the highest energy
resource is coal as expectedly.
Total electricity productions 1975–2011 is shown in Table 35.1. Table 35.2
show that between 1975 and 2011 years emission release into atmosphere in
Turkey. Coal emission release CH4 and NOx values could not be found. As the
approached the 2000s years, because of increase in population growth and electric-
ity demand, has increased emissions released into the atmosphere. Table 35.1 and
Table 35.2 data’s for this paper has been collected from the Turkish Statistical Institute (TUİK) database (TUIK 2015).
Figure 35.2 shows that the electricity production percent of distribution from
years 1980 to 2010 in Turkey [13]. In 1980 year, electricity production as percent of
Table 35.1 (continued)
Years Coal (TJ)
Liquids Fuel (TJ)
Natural gas (TJ)
Hyro (TJ) Renewable energy (TJ)
1998 320.7426 80.87509 162.7622 164.1802 5.995188
1999 333.2513 82.43253 237.7679 135.0351 6.28776
2000 344.0352 96.12748 302.5081 120.0782 6.745788
2001 345.7163 105.7693 324.4971 93.60894 6.62715
2002 288.8208 110.1945 343.8402 130.929 6.9876
2003 289.7374 93.75347 415.8737 137.3183 5.060916
2004 310.5886 78.85424 407.3371 179.4556 5.425128
2005 389.1803 56.49673 480.1662 153.7854 5.830416
2006 420.4755 45.22095 528.4625 172.2084 6.3468
2007 481.0021 66.82309 621.8396 139.4024 13.79218
2008 519.6567 77.35921 645.4072 129.7235 21.42914
2009 501.4487 49.96953 628.581 140.2548 42.07961
2010 596.6564 23.53593 698.1251 218.7148 78.45309
2011 612.1543 9.828957 711.6268 212.502 112.0846
Table 35.2 GHG emissions values (IPCC 1996; CIPEC
2002; Hepbasli 2010)
Fuel type CO2 (t/TJ) CH4 (kg/TJ) NOx (kg/TJ)
Natural gas 49.68 0.13–1.27 0.62
Liquid Fuelsa 59.84–74 0.16–121.11 3.11–12.5
Coal 93.8–95 – –
t ton, kg kilogram, TJ terajoule aGasoline, kerosene, jet fuel, LPG, diesel, jet fuel, aircraft
35 Environmental Impact Assessment of Electricity Production, A Case Study. . . 467
T a b le
3 5 .3
E m is si o n re le as e v al u es
b et w ee n th e y ea rs
1 9 7 5 – 2 0 1 1 in
T u rk ey
(T U İK
, 2 0 1 5 )
Y ea rs
C o a l
L iq u id s F u el
N a tu ra l g a s
C O
2
(t /y ea r)
C H
4
(t /y ea r)
N O
x
(t /y ea r)
C O
2
(t /y ea r)
C H
4
(k g /y ea r)
N O
x
(k g /y ea r)
C O
2
(t /y ea r)
C H
4
(k g /y ea r)
N O
x
(k g /y ea r)
1 9 7 5
3 5 0 5 .6 7
– –
3 7 0 0 .7 2 5
3 3 5 1 .2 2 4
4 3 1 .3 4 5 7
0 0
0
1 9 7 6
3 6 9 6 .9 7 6
– –
3 7 1 5 .7 1 6
3 3 6 4 .7 9 9
4 3 3 .0 9 3
0 0
0
1 9 7 7
4 1 7 5 .9 6 2
– –
4 7 3 0 .1 7 1
4 2 8 3 .4 4 8
5 5 1 .3 3 4 9
0 0
0
1 9 7 8
4 7 4 5 .3 7 6
– –
4 5 9 4 .4 5 3
4 1 6 0 .5 4 7
5 3 5 .5 1 6
0 0
0
1 9 7 9
5 4 9 5 .7 1
– –
3 8 8 1 .3 6
3 5 1 4 .8
4 5 2 .4
0 0
0
1 9 8 0
5 0 8 3 .7 0 7
– –
4 0 1 1 .1 3
3 6 3 2 .3 1 4
4 6 7 .5 2 5 6
0 0
0
1 9 8 1
5 2 4 1 .7
– –
3 9 8 1 .0 0 9
3 6 0 5 .0 3 8
4 6 4 .0 1 4 7
0 0
0
1 9 8 2
5 5 0 4 .9 6 2
– –
4 0 8 3 .6 5
3 6 9 7 .9 8 6
4 7 5 .9 7 8 4
0 0
0
1 9 8 3
7 3 2 6 .3 9 3
– –
5 1 0 7 .1 8 9
4 6 2 4 .8 6
5 9 5 .2 7 9
0 0
0
1 9 8 4
8 6 4 5 .6 7 5
– –
4 8 3 4 .4 9 6
4 3 7 7 .9 2 1
5 6 3 .4 9 4 8
0 0
0
1 9 8 5
1 2 ,8 1 6 .8 9
– –
4 8 6 3 .4 1 1
4 4 0 4 .1 0 5
5 6 6 .8 6 5
2 2 .2 5 2 3 2
0 .3 1 3 5 3 9
0 .2 7 7 7 0 6
1 9 8 6
1 6 ,5 9 5 .2 1
– –
4 7 9 6 .8 0 2
4 3 4 3 .7 8 6
5 5 9 .1 0 1 2
4 3 8 .8 2 6 3
6 .1 8 3 1 4 1
5 .4 7 6 4 9 6
1 9 8 7
1 5 ,0 6 1 .1 1
– –
3 7 7 6 .1 3 9
3 4 1 9 .5 1 6
4 4 0 .1 3 5 8
8 2 2 .0 0 7 6
1 1 .5 8 2 2 3
1 0 .2 5 8 5 5
1 9 8 8
1 0 ,6 5 8 .8 1
– –
2 2 7 6 .3 3 8
2 0 6 1 .3 5 8
2 6 5 .3 2 3 3
1 0 4 6 .7 3 6
1 4 .7 4 8 6 9
1 3 .0 6 3 1 3
1 9 8 9
1 7 ,2 7 2 .8
– –
2 9 3 0 .0 8
2 6 5 3 .3 6
3 4 1 .5 2 1 6
3 0 9 6 .6 4 5
4 3 .6 3 2 2 7
3 8 .6 4 5 7 3
1 9 9 0
1 7 ,2 3 2 .5 9
– –
2 7 2 6 .1 1 9
2 4 6 8 .6 6 2
3 1 7 .7 4 8 5
3 3 1 1 .6 4 5
4 6 .6 6 1 6 6
4 1 .3 2 8 9
1 9 9 1
1 8 ,4 0 1 .8 8
– –
2 2 7 5 .0 6 7
2 0 6 0 .2 0 7
2 6 5 .1 7 5 2
4 0 9 4 .0 4 4
5 7 .6 8 5 8
5 1 .0 9 3 1 4
1 9 9 2
2 0 ,9 7 1 .5 1
– –
3 6 0 6 .4 8 3
3 2 6 5 .8 8 3
4 2 0 .3 6 1 2
3 5 2 5 .2 4 9
4 9 .6 7 1 3 9
4 3 .9 9 4 6 6
1 9 9 3
2 0 ,2 7 7 .3
– –
3 5 4 7 .3 5 6
3 2 1 2 .3 4
4 1 3 .4 6 9 5
3 5 0 3 .7 5 9
4 9 .3 6 8 5 9
4 3 .7 2 6 4 6
1 9 9 4
2 4 ,0 5 6 .7 6
– –
3 8 1 8 .0 8 3
3 4 5 7 .4 9 9
4 4 5 .0 2 4 7
4 4 8 2 .0 2 6
6 3 .1 5 2 5 4
5 5 .9 3 5 1 1
1 9 9 5
2 3 ,9 1 5 .4 3
– –
3 9 6 7 .5 4 7
3 5 9 2 .8 4 8
4 6 2 .4 4 5 7
5 3 8 4 .2 2 5
7 5 .8 6 4 6 8
6 7 .1 9 4 4 3
1 9 9 6
2 5 ,9 8 0 .5 4
– –
4 4 9 4 .1 2
4 0 6 9 .6 9
5 2 3 .8 2 1 5
5 5 8 2 .7 5 8
7 8 .6 6 2 0 5
6 9 .6 7 2 1
1 9 9 7
2 8 ,9 0 7 .3 4
– –
4 8 9 3 .6 8 4
4 4 3 1 .5 1 9
5 7 0 .3 9 3 5
7 1 8 7 .4 5 7
1 0 1 .2 7 2 5
8 9 .6 9 8 5 3
1 9 9 8
3 0 ,4 0 6 .3 9
– –
5 4 1 2 .1 6 1
4 9 0 1 .0 3
6 3 0 .8 2 5 7
8 0 8 6 .0 2 4
1 1 3 .9 3 3 5
1 0 0 .9 1 2 5
468 F. Yılmaz et al.
1 9 9 9
3 1 ,5 9 2 .2 2
– –
5 5 1 6 .3 8 5
4 9 9 5 .4 1 2
6 4 2 .9 7 3 8
1 1 ,8 1 2 .3 1
1 6 6 .4 3 7 5
1 4 7 .4 1 6 1
2 0 0 0
3 2 ,6 1 4 .5 4
– –
6 4 3 2 .8 5 1
5 8 2 5 .3 2 5
7 4 9 .7 9 4 3
1 5 ,0 2 8 .6
2 1 1 .7 5 5 7
1 8 7 .5 5 5
2 0 0 1
3 2 ,7 7 3 .9 1
– –
7 0 7 8 .0 8 2
6 4 0 9 .6 2
8 2 5 .0 0 0 6
1 6 ,1 2 1 .0 1
2 2 7 .1 4 8
2 0 1 .1 8 8 2
2 0 0 2
2 7 ,3 8 0 .2 1
– –
7 3 7 4 .2 1 3
6 6 7 7 .7 8 4
8 5 9 .5 1 6 7
1 7 ,0 8 1 .9 8
2 4 0 .6 8 8 2
2 1 3 .1 8 0 9
2 0 0 3
2 7 ,4 6 7 .1 1
– –
6 2 7 3 .9 8 2
5 6 8 1 .4 6
7 3 1 .2 7 7 1
2 0 ,6 6 0 .6
2 9 1 .1 1 1 6
2 5 7 .8 4 1 7
2 0 0 4
2 9 ,4 4 3 .8
– –
5 2 7 6 .9 2 5
4 7 7 8 .5 6 7
6 1 5 .0 6 3
2 0 ,2 3 6 .5
2 8 5 .1 3 5 9
2 5 2 .5 4 9
2 0 0 5
3 6 ,8 9 4 .2 9
– –
3 7 8 0 .7 6 1
3 4 2 3 .7 0 2
4 4 0 .6 7 4 5
2 3 ,8 5 4 .6 6
3 3 6 .1 1 6 4
2 9 7 .7 0 3 1
2 0 0 6
3 9 ,8 6 1 .0 8
– –
3 0 2 6 .1 8 6
2 7 4 0 .3 9
3 5 2 .7 2 3 4
2 6 ,2 5 4 .0 2
3 6 9 .9 2 3 7
3 2 7 .6 4 6 7
2 0 0 7
4 5 ,5 9 9
– –
4 4 7 1 .8 0 1
4 0 4 9 .4 7 9
5 2 1 .2 2 0 1
3 0 ,8 9 2 .9 9
4 3 5 .2 8 7 7
3 8 5 .5 4 0 5
2 0 0 8
4 9 ,2 6 3 .4 6
– –
5 1 7 6 .8 7 8
4 6 8 7 .9 6 8
6 0 3 .4 0 1 8
3 2 ,0 6 3 .8 3
4 5 1 .7 8 5 1
4 0 0 .1 5 2 5
2 0 0 9
4 7 ,5 3 7 .3 3
– –
3 3 4 3 .9 6 1
3 0 2 8 .1 5 4
3 8 9 .7 6 2 4
3 1 ,2 2 7 .9
4 4 0 .0 0 6 7
3 8 9 .7 2 0 2
2 0 1 0
5 6 ,5 6 3 .0 3
– –
1 5 7 5 .0 2 4
1 4 2 6 .2 7 7
1 8 3 .5 8 0 2
3 4 ,6 8 2 .8 6
4 8 8 .6 8 7 6
4 3 2 .8 3 7 6
2 0 1 1
5 8 ,0 3 2 .2 3
– –
6 5 7 .7 5 3 8
5 9 5 .6 3 4 8
7 6 .6 6 5 8 6
3 5 ,3 5 3 .6 2
4 9 8 .1 3 8 8
4 4 1 .2 0 8 6
35 Environmental Impact Assessment of Electricity Production, A Case Study. . . 469
rate respectively coal 25.6%, liquid fuels 25.1%, natural gas 0%, hydro 48.8% and
renewable energy 0.6%. Moreover, in 2000 years, while from coal and natural gas
increase in for electricity production, hydro and liquids fuels usage of decreased
shows that from Fig. 35.1. Approximately, percentage of the electricity production
from coal and natural gas at about 72% in 2010 year. As can be seen in this figure
that electricity production from natural gas increases from 1988 in Turkey.
Results and Discussion
In this paper CO2, CH4 and NOx emissions are calculated from 1975 to 2011 for
Turkey. The Turkish Statistical Institute (TUİK) database is considered (TUIK
2015) while calculating these emission values.
Figure 35.3 shows that CO2 emissions from electricity production in Turkey
between 1975 and 2011. The CO2 emission values from liquid fuels did not change
too much, between 1975 and 2011. But, an increase is seen for coal and natural gas
CO2 emission values in this figure. As expected that CO2 emissions values from
coal are higher than that of others. CO2 emissions values from coal and natural gas
were observed sharply changes in 2002. CO2 emissions values from coal decreased
while the CO2 emissions values of natural gas increased at 2002.
Figure 35.3 illustrates the change of electricity production resource in Turkey
from 1975 to 2011. Especially, the usage of natural gas subsequently increase after
1998. The usage of liquid fuels decrease because of the commonly usage of the
natural gas after 1998. The use of natural gas is better than coal in terms of
emissions. In 2001 year was observed that from natural gas electricity production
is higher than coal (Fig. 35.4).
60
50
40
30
20
10
0 1980 1990 2000
years
E le
ct ri
ci ty
p ro
d u
ct io
n r
es o
u rc
es (
% )
2010
Caol (%)
Liquid Fuels (%)
Natural Gas (%)
Hydro (%)
Renewable Energy (%)
Fig. 35.2 Electricity production resources of Turkey from 1980 to 2010
470 F. Yılmaz et al.
CH4 emission values from 1975 to 2011 for electricity production resource is
given in Fig. 35.5. While resulting from natural gas emissions quite a few, but liquid
fuels are higher. Also as can be seen in this figure that, CH4 emissions from liquid
fuels decreases, while CH4 emissions from natural gas increases after than 2003.
NOx emission values from 1975 to 2011 for electricity production resource is
given in Fig. 35.6. Also as can be seen in this figure that, NOx emissions from liquid
fuels decreases, while NOx emissions from natural gas increases after than 1988.
1979
Coal Liquid Fuels Natural gas
65000 60000 55000 50000 45000 40000 35000 30000 25000 20000 15000 10000 5000
−5000 0
1987 1995
Years
C O
2 em
m is
io n
( t/
ye ar
)
2003 20111971
Fig. 35.3 Between 1975 and 2011 from electricity production release CO2 emission
750 700 650 600 550 500 450 400 350 300 250 200 150 100
50
−50 0
Years
T J
Coal Liquid Fuels Natural gas
1979 1987 1995 2003 20111971
Fig. 35.4 Between 1975 and 2011 electricity production resource (TUİK 2015)
35 Environmental Impact Assessment of Electricity Production, A Case Study. . . 471
Conclusions
In this study, an environmental impact assessment of electricity production was
investigated and compared for CO2, CH4 and NOx emissions in Turkey.
Some concluding remarks from this study can be extracted as follows:
(a) In 2011, the electricity production from coal is 642.15 TJ, and corresponding
CO2 emission is 58032.23 t/year. And 711.62 TJ for natural gas and
corresponding CO2 emission is 498.13 kg/years.
Liquid Fuels
7000
6000
5000
4000
3000
2000
1000
0
Years
C H
4 em
is si
o n
Natural gas
19 75
19 77
19 79
19 81
19 83
19 85
19 87
19 89
19 91
19 93
19 95
19 97
19 99
20 01
20 03
20 05
20 07
20 09
20 11
Fig. 35.5 Between 1975 and 2011 from electricity production release CH4 emission
1971
1000
900
800
700
600
500
400
300
200
100
0 1979 1987 1995
Years
N O
x em
is si
o n
( t/
ye ar
)
2003 2011
Liquid Fuels Natural gas
Fig. 35.6 Between 1975 and 2011 from electricity production release NOx emission
472 F. Yılmaz et al.
(b) It has been observed a continuous increase in electricity production from coal
and natural gas from 1975 to 2011.
(c) It has been observed that most of the CO2 emissions arise from coal and CH4 emissions from liquid fuels higher than natural gas.
(d) Until 2009 year, it has been observed that from liquid fuels NOx emissions
higher than that of natural gas, but after this year this situation is reversed.
As can we concluded that, in Turkey the electricity produced mostly from coal
and natural gas. The usage of liquid fuels decreased while the usage of the natural
gas increased.
Nomenclature
GHG Greenhouse gas
MW Megawatt
TJ Terajoule
t Ton
kg Kilogram
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Chapter 36
Hybridization of Parabolic Trough Power Plants with Natural Gas Through Integration of Industrial Gas Turbines
Tobias Vogel, Gerd Oeljeklaus, and Klaus G€orner
Introduction
The operation of concentrating solar power (CSP) plant concepts without thermal
energy storage is completely dependent on the course of the sun. Because of this
dependency such power plants have only a limited capability of regulating the
electrical grid. The operation temperature is also very closely linked to collector
technology and available solar radiation. The input of fossil fuel, however, can be
controlled and therefore used according to needs. Through the systematic combi-
nation of solar and fossil energy a more flexible power plant is created. Even from
financial standpoint hybrid plants offer in mid-term a cost reduction potential and
thereby lessen economic inhibitions.
The total electricity consumption will grow until 2035 by roughly 65%, as
predicted in (BP 2014) based on the reference year 2012, whereas the absolute
share of natural gas will be approximately constant at 20.5% (BP 2014). This
indicates that natural gas will play in mid-term an important role. In terms of the
combined usage of natural gas and concentrated solar thermal energy in one power
plant the most common solution is the ISCC (Integrated Solar Combined Cycle).
Due to technical reasons the amount of integrable solar energy is strongly limited,
for instance the annual solar share is relatively low at 2–8% (Turchi et al. 2011). An
alternative approach is to integrate smaller gas turbines, like industrial or
aeroderivative gas turbines, into a CSP plant. A fairer performance ratio and a
comparatively lower natural gas usage are achievable, for what reason this idea is
increasingly studied in the last years (e.g. Turchi et al. 2011; Vogel et al. 2013;
Servert et al. 2014).
T. Vogel (*) • G. Oeljeklaus • K. G€orner LUAT, University of Duisburg-Essen, Leimkugelstrasse 10, Essen 45141, Germany
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_36
475
For this case study the configuration of the parabolic trough power plant Shams
One (cf. Goebel 2010), located Madinat Zayed in Abu Dhabi part of the United
Arab Emirates (UAE) has been used. The power plant itself as well as the region
fulfills all requirements to make such an analysis worthwhile.
The UAE have the world’s seventh largest proved reserves of natural gas (BP 2014). For that reason natural gas covers roughly 63% of the UAE’s primary energy consumption and thus represents their main energy source (BP 2014). In
2011 the installed gross electricity capacity has been divided into 18.5 GWel of
combined cycle, 5.4 GWel gas turbine and 2.3 GWel steam turbine (UAE 2012). But
in Abu Dhabi itself are still 0.4 GWel of open cycle gas turbine capacity installed,
which indicates a potential of combining such gas turbines with Shams One. Due to
an expected rising energy consumption and sharper summerly load transients the
local grid operator TRANSCO is forecasting an amount of 1.3 GWel installed gross
capacity of open cycle gas turbines until 2020 (TRANSCO 2014).
In addition it should be noted, that there is one additional power plant located in
Madinat Zayed with the name “Madinat Zayed Power Plant,” owned by the Al
Mirfa Power Company. It consists out of four open cycle gas turbines with an
installed gross capacity of 0.1 GWel (Al Mirfa Power Company 2014). Altogether it
can be assumed that at least for this application example from outer perspective a
market potential for the developed hybridization configuration exists.
The Site
As site for the calculations Madinat Zayed in the United Arab Emirates was chosen,
where also Shams One is located. The weather profile was taken in hourly time
resolution from the meteonorm database (version 7.0). This averaged dataset has a
yearly total direct normal irradiance (DNI) of 1889 kWh/(m2a), which corresponds
well with the number of 1925 kWh/(m2a), published in (Goebel 2010), whose value
is based on ground data collected during the project development of Shams One.
The sorted distribution curve and the interval frequency of the aperture effective
DNI (cosine correction included) are shown in Fig. 36.1, whereas for the interval
frequency only all hours with an aperture effective DNI greater than 1 Wh/(m2h)
are considered.
Within respect of the cosine correction the yearly available aperture effective
DNI is lowered by 8.5% to 1729 kWh/m2. An average aperture effective DNI of
over 700 Wh/(m2h) appears only in 204 h, which underpins the medium insolation
quality for the analyzed site.
The design point was set to be on 21st March at solar noon, because of the
comparatively low aerosol charge of the air in spring compared to the summer
month. Referring to (Goebel 2010) the DNI for the design point is 750 W/m2.
476 T. Vogel et al.
The Base Case Power Plant
The layout of the base case power plant is shown in Fig. 36.2 and the main technical
performance data from the design point are given in the diagram in the lower left
part of Fig. 36.2. The thermodynamic model can be divided into the solar-heat-
transfer-fluid-cycle (solar-HTF-cycle) and the water/steam cycle. The main param-
eters were primarily taken from publications or otherwise estimated based on
typical values and design guidelines.
Solar-HTF-Cycle
The solar-HTF-cycle has the following two main tasks:
• transform the solar irradiation into heat.
• transfer the gained heat to a power generation process.
Therefore the solar-HTF-cycle consists out of the main components solar field,
HTF-pump, HTF-heater and the connecting solar steam generator (SSG).
As heat transfer fluid (HTF) the thermal oil Therminol VP1 has been used,
similar to Shams One. It is thermally stable up to 400 �C, whereas the related vapor pressure is 10.9 bar (SOLUTIA 2013). For security reasons a HTF-evaporation
should be avoided at any time. In order to fulfill this requirement the minimum
pressure (position: suction HTF-pump) in the solar-HTF-cycle has been set to
15 bar. The pressure loss over the complete solar field is assumed to be 5.25 bar
(Balan 2014) for nominal conditions and in the SSG 2.5 bar, so that the HTF-pump
discharge pressure overall amounts to 22.75 bar.
Fig. 36.1 Sorted distribution curve and interval frequency of the aperture effective DNI for the used weather profile from Madinat Zayed
36 Hybridization of Parabolic Trough Power Plants with Natural Gas Through. . . 477
The solar field of Shams One consists out of 768 ASTRØ 150 collectors (Goebel
2010), in a typical 4 collectors per loop arrangement. Due to the fact that the solar
library (Pawellek et al. 2009) of the power plant simulation program Ebsilon®
Professional includes only a model of the EUROTrough ET 150 collector, this
comparable collector type has been used. In order to serve a sufficient thermal heat
input even in case of low solar insolation, e.g. due to cloud passing, the solar-HTF-
cycle is additionally furnished with a HTF-heater, which is fuelled with natural gas.
At nominal conditions 1061.6 kg/s of HTF are circulating, whereby its temper-
ature is elevated from 296.6 �C (HTF-side outlet of SSG) to 393 �C (HTF-side inlet of SSG) while passing the solar field.
Water/Steam Cycle
The main components in the water/steam cycle are the SSG, the booster, the turbo-
generator (steam turbine and generator), the air-cooled condenser, condensate and
feedwater pump as well as the low and the high pressure feed heaters.
The solar heat is transferred to the water steam cycle via the SSG. By that heat
input the feedwater entering the SSG at 219.46 �C and 111 bar is preheated, evaporated and superheated up to 380 �C at 102.5 bar. Subsequently, the steam is further superheated in a natural-gas-fired booster. At live steam parameters of
540 �C and 100 bar (Reuß 2012) the steam enters a 35-staged, single flow steam turbine (MAN 2014). The 35 turbine stages can be arranged for the thermodynamic
solar-HTF-cycle
solar field
natural gas inlet
flue gas outlet
air inlet
solar steam
generator
natural gas inlet
air inlet
flue gas outlet booster steam turbine
G
technical data
main HTF pump
M
M
M
M
LP feed heaters
feed water tank
feed water pump
condensate pump
air cooled condenser air
inlet
air outlet
H P
fe ed
h ea
te rsheat input 303.97 MWth
heat input solar steam generator 249.95 MWth heat input booster 54.02 MWth heat input heater 0.00 MWth gross power output 120.70 MWel auxiliary power demand 6.50 MWel net power output 114.20 MWel water/steam cycle gross efficiency 39.70 % net plant efficiency 21.65 % live steam flow 120.00 kg/s live steam temperature 540.00 °C live steam pressure 100.00 bar condenser pressure 0.13 bar
HTF-heater 1 2
34 5
678
1
2
34 5
6 78
M
Fig. 36.2 Process flow diagram of the base case power plant based on the configuration of Shams One
478 T. Vogel et al.
modelling related to the required extractions for the feedwater preheating into
7 stage groups. Through passing the steam turbine the steam is expanded to the
condenser pressure of 0.13 bar (Reuß 2012), while six partial flows are extracted for
the feedwater preheating. For the last 3 stage groups the wetness correction for the
isentropic efficiency was used because of the present steam wetness. Following, the
discharge steam streams through an air-cooled condenser (ACC). Then the fully
condensed water is delivered by the condensate pump to the feedwater tank, while
passing two low pressure (LP) feed heaters. From the feedwater tank the feedwater
is led through the feedwater pump to the SSG, while passing three high pressure
(HP) feed heaters. The extraction pressure levels have been chosen in order to
enable a temperature step of 28 K in each preheater (regulation cf. Schr€oder 1966). All assumed machinery efficiency data are given in Table 36.1.
At nominal conditions with a heat input of 301 MWth 120 kg/s of water/steam
circulates in the system. The power plant therefore generates 120.7 MWel of gross
electricity, which represents a water/steam cycle gross efficiency of 39.45%. In part
load the live steam pressure level is set in general by the steam generator while the
pressure entering the first stage of the turbine undergoes the Stodola’s law. Because of that coherence for part load operation a modified sliding pressure mode was
assumed for the steam generator.
Technical Boundary Conditions
An important basis for the development of the operating logic of a power plant
represents the knowledge of the elementary technical boundary conditions,
whereby for reasons of presentation a differentiation into the three areas solar
field, water/steam-cycle and natural-gas-firing has been made.
For the solar field off-design operation a minimum circulating HTF mass flow of
200 kg/s has been considered, while the outlet temperature is limited to 393 �C. In case of high solar insolation when the heat-entry oversteps the nominal value, the
troughs are defocussed automatically until the heat-entry achieves the allowed
nominal value.
Table 36.1 Efficiency data (isentropic, mechanical and electrical) for the process machinery
Component ηs (%) ηmech (%) ηel (%) Electric motor – 99.80 97.00
Generator – – 98.55
Pump 80.00 99.80 –
Blower 86.00 99.80 –
HP steam turbine (1. stage group) 84.00 99.80 –
IP steam turbine (2.-6. stage group) 90.00 99.80 –
LP turbine (7. stage group) 86.00 99.80 –
36 Hybridization of Parabolic Trough Power Plants with Natural Gas Through. . . 479
Regarding the water/steam cycle the SSG and the steam turbine are in general
the limiting components, whereby in this work the steam turbine has been used as
benchmark. For that reason an industry-related, steam turbine model has been
developed, whose technical boundary conditions mainly occur during the
off-design operation. The following main technical boundary conditions for the
steam turbine with maximum allowable steam wetness (15%), maximum turbine-
exhaust pressure (0.23 bar), smoothed live steam temperature and permissible
temperature gradients for heating (5 K/min) and cooling (�2 K/min) have been identified in (Vogel et al. 2013), thus this reference is referred for further explana-
tion. It has to be mentioned, that as specific state point for the steam wetness at the
steam turbine outlet the expansion line end point has been used. Furthermore the
maximum turbine-exhaust volume flow factor is limited to the factor 1.5 of the
nominal value for the volume flow at the turbine-exhaust. Besides, the live steam
temperature is smoothed by the booster until 3 O’clock pm, in order to avoid negative temperature gradients during main steam turbine operation time.
According to (Goebel 2010) the amount of natural gas is limited to 600,000
MMBTU/a. From that the booster has an approximated contribution share of 81.8%
and the HTF-heater one of 18.2% (Goebel and Luque 2012). Due to the fact that the
composition of natural gas fluctuates and is not clear defined, in this case study
methane was used as reference fuel with a lower heating value of 50,015 kJ/kg.
Based on these boundary conditions the heater has in total a potential of 2,301.3
tmethane/a and the booster one of 10,355.6 tmethane/a. In addition the booster’s min-load is set to 5% of nominal fuel mass flow.
Operational Logic
The power plant operation can be divided in four main operating states, namely:
night, below min-load, normal day and heater operation. During night no insolation
is available and the power plant is out of operation. In exceptional situations the
grid operator can prescribe power plant operation during night by using the fossil-
only mode (Goebel and Luque 2012), but that exception has been neglected for the
performed case study. The other three operating states are during the day. If the
insolation is too low to provide the minimum amount of circulating HTF-mass flow
the power plant is out of operation as well. If the DNI is high enough the power
plant is in typical normal day operation. Is the power plant in normal operation and
it appears a sudden (or forecasted) short-term insolation drop in the next time step,
for example caused by cloud passing, the power plant should still operate in order to
avoid start-up and shut-down losses by using the HTF-heater.
The following three identification criteria need to be fulfilled for HTF-heater
operation. At first the HTF-heater shall operate only up to 16 o’clock to follow the typical diurnal variation of the insolation. Secondly the insolation drop compared to
the previous DNI must be higher than 250 W/(m2h). As third criteria for HTF-heater
480 T. Vogel et al.
operation the DNI must be lower than 400 Wh/(m2h). When HTF-heater operation is
identified, the HTF-heater can be operated with its load in different ways. For this
case study the HTF-heater operates in order to enable the same load, meaning
entering the SSG with the same HTF-mass flow, as in the time step before.
The booster operates in respect to the given technical boundary conditions.
When the steam generator achieves a load level close to full load in the previous
and the actual hour the booster goes to full load and delivers live steam at 540 �C and 100 bar, as long as none of the named boundary conditions are opposed.
In case of the necessity to reduce the power plant load, e.g. due to the turbine-
exhaust pressure limitation, firstly the fossil-firing is reduced to the technical lowest
limit, e.g. booster min-load or smoothed live steam temperature. Secondly, the load
of the solar field is reduced through defocussing.
The Base Case Power Plant with Front End Gasturbine
Concept Layout
Figure 36.3 shows the process flow diagram of the developed concept with the
additional integration of a gas turbine into the base case power plant.
In general there are different ways for the integration of the gas turbine’s waste heat possible, for instance the integration into the booster’s air flow or directly into the water/steam-cycle. In order to avoid technical changes of the installed booster
arrangement the waste heat has been integrated directly through two heat
LP-FH 2
condensate pump
air-cooled condenser
feedwater pump
feed- water tank
HP-FH 3
fan
LP-FH 1
HP-FH 2
HP-FH 1
economizer
evaporator
superheater
booster
HTF-pump
HTF-heater
steam turbine generator
solar f ield G~
G~
GT-SH
GT-FH stack
gas turbine (GT)
Fig. 36.3 Process flow diagram of the base case power plant added with a front end gas turbine
36 Hybridization of Parabolic Trough Power Plants with Natural Gas Through. . . 481
exchangers into the water/steam cycle. The waste heat at high temperature level is
firstly integrated through the gas turbine waste heat recovery superheater (GT-SH),
located between the SSG-superheater and the booster, in order to lower the
booster’s load. The remaining waste heat with a temperature of up to 390 �C can be used part vise further for preheating the feed water. Replacing HP bled off steam
is thermodynamically favorable. For that reason secondly the gas turbine waste heat
recovery feed heater (GT-FH) is installed in parallel to the HP feed heaters
(HP-FH). Thus, the required amount of bled steam is reduced and consequently a
higher steam turbine power output reveals. In terms of corrosion by the cause of
condensation of exhaust gas components it has to be mentioned, that through the
chosen arrangement the stack temperature stays above 100 �C even in low load due to the minimum pressure in the feedwater tank of 1.15 bar. A displacement of the
HP-FH 3 was not undertaken in order to secure always the required feed water
temperature at the inlet of the economizer.
Gas Turbine Selection
In respect to the developed concept layout the following specification requirements
have been used for the gas turbine selection:
• grid frequency: 50 Hz
• gas turbine performance class: 10–20 MWel • emission reduction technology: dry, resp.no water/steam injection
• exhaust gas temperature: at least 540 �C
Based on the market review, given in (Gas Turbine World 2011), out of the
276 listed gas turbines only four gas turbines fulfill the above mentioned require-
ments. Namely: THM 1304-14 (MAN), L20A (Kawasaki), H-15 (Hitachi) and
SGT-400 (Siemens). In order to cover the complete range of electrical efficiency
the THM 1304-14 (31.0%) and the SGT-400 (34.8%) have been chosen for the
conducted case study. The technical data of these two gas turbines at nominal
conditions (cf. ISO 2314-2009) are summed up in Table 36.2.
The operation of gas turbines has a strong dependence on the ambient condi-
tions. For example, a change in the elevation level (resp. ambient pressure) or the
Table 36.2 Technical data for the two gas turbines
for generation drive at
nominal conditions
(GTW-Performance
Specs 2011)
Parameter Unit GTa) GTb)
Type THM 1304-14 SGT-400
Electric power kWel 12,680 12,900
Heat rate kJ/kWh 11,610 10,355
Electric efficiency % 31.0 34.8
Exhaust temperature �C 545.0 555.0 Exhaust mass flow kg/s 49.0 39.4
Pressure ratio – 11.0 16.9
482 T. Vogel et al.
ambient temperature have a strong influence on the performance of the gas turbine.
For that reason the operating characteristic of the gas turbines need to be taken into
account for the annual yield simulation. Therefore two different approaches have
been used. For the GTa) a full thermodynamic model has been developed based on
the design point data and the instructions given in (Lechner and Seume 2010),
which covers the part load and operating behavior. Contrary for the GTb) charac-
teristic curves provided by the manufacturer have been used. It should be noted, that
GTb) has a customized design referring to the studied site. For both gas turbines the
same site boundary conditions with an ambient pressure at the design-point of
99.9 kPa and pressure losses at gas turbine inlet and gas turbine outlet (due to waste
heat recovery) of 1 and 2.5 kPa have been used.
Figure 36.4 shows for GTa) the distribution of the electrical efficiency for each
operating point as subject to the ambient temperature.
The operating points of GTa) are arranged in Fig. 36.4 as a passel. That means
that even for operating points with an equal ambient temperature different efficien-
cies occur, due to various ambient pressure and ambient humidity. With decreasing
ambient temperature the GT-efficiency is raised. Summarizing, the developed
thermodynamic model for GTa) enables a typical operating behavior.
The Solar Only Bench Mark Model
For the closing assessment of the concepts in terms of power generation efficiency
from natural gas it is necessary to perform the annual yield simulations as well with
a, so called, solar only model. Using the base case power plant and operating it in
solar only mode is not feasible, because for example technical limitations like steam
turbine wetness could not be fulfilled with the given design of the components. For
Fig. 36.4 Annual operating behavior of the gas turbine GTa)
36 Hybridization of Parabolic Trough Power Plants with Natural Gas Through. . . 483
that reason a solar only benchmark model has been developed, whose process flow
diagram and technical data for the design-point are given in Fig. 36.5.
In comparison to the base case power plant, shown in Fig. 36.5, the booster has
been removed. With the objective to fulfill still the steam turbine wetness limitation
the power plant has been additionally equipped with a reheating. Therefore the
superheated steam leaving the first turbine stage group at 225.54 �C and 25.75 bar is reheated up to 380 �C. Following the reheated steam is returned to the steam turbine for the further expansion. Through this arrangement the steam turbine-exhaust
wetness limitation could be fulfilled, e.g. at the design-point the steam wetness is
11.4%. The solar field and the nominal HTF-mass flow are still the same as for the
base case power plant. But the HTF-mass flow is now split up between the solar
steam generator and the reheating. For that reason the transferred heat into the
water/steam cycle through the solar steam generator is lowered to 252.27 MWth,
while heat input in reheating amounts to 39.38 MWth. As consequence the circu-
lating steam mass flow is lowered to 102.02 kg/s. Using the efficiency data given
Table 36.1 altogether a net power output of 88.96 MWel at the design-point could be
generated. Whereas the gross efficiency is 37.5%, which represents a reduction of
2.2%-points related to the base case power plant.
Results and Discussion
For all in the previous chapters mentioned configurations, namely
• solar only bench mark model: abbr.: solar only
• base case power plant: abbr.: BC
solar-HTF-cycle solar field
natural gas inlet
flue gas outlet
air inlet
solar steam
generator
reheating
HTF-heater 1 2
34 5
678
M
M main HTF pump
steam turbine
G
M
M
M
condensate pump
air cooled condenser air
inlet
air outlet
feed water tank
feed water pump LP feed heaters
H P
fe ed
h ea
te rs
technical data
heat input 252.27 MWth heat input solar steam generator 212.89 MWth heat input reheating 39.38 MWth heat input heater 0.00 MWth gross power output 94.60 MWel auxiliary power demand 5.64 MWel net power output 88.96 MWel water/steam cycle gross efficiency 37.50 % net plant efficiency 18.89 % live steam flow 102.02 kg/s live steam temperature 380.00 °C live steam pressure 100.00 bar
condenser pressure 0.13 bar
reheating steam temperature 380.00 °C reheating steam pressure 25.75 bar
Fig. 36.5 Process flow diagram of the solar only benchmark model
484 T. Vogel et al.
• base case power plant plus GTa) (THM1304-14): abbr.: BCþGTa) • base case power plant plus GTb) (SGT-400): abbr.: BCþGTb),
annual yield simulations have been performed in hourly time resolution, based
on the given information regarding the operational logic and the used exemplary
annual weather profile.
In order to enable a fundamental understanding of the power plant model at first
the behavior of the base case power plant is analyzed. Therefore initially the daily
behavior is discussed based on two example daily curves, before subsequently the
attention is given to the annual behavior.
Base Case Power Plant
In Fig. 36.6 the daily variation for process parameters (steam turbine inlet temper-
ature, steam turbine outlet pressure and DNI), shown as curves, and performance
values (heat input through SSG, HTF-heater and booster, generated net electricity),
shown as bars, are displayed exemplary for (a) 25th March (spring) and (b) 17th
July (summer).
Figure 36.6a shows with the 25th March an ideal sunny day in spring. The DNI is
very constant and lies during the day at around 600 W/m2. The power plant starts in
solar only mode, wherefore the steam turbine inlet temperature without booster-
operation is roughly 380 �C. In the next hour the solar heat input raises analog to the DNI and the daily shape of the incidence correction. Following, the steam mass
flow is increasing and so the shape of the process in the T,s-diagram is moving to
the left. Assuming a similar expansion in the steam turbine the steam wetness is
increasing and the steam turbine wetness limitation moves into focus. As a result,
the steam turbine inlet temperature is raised by the booster to 524 �C. Also in the following hour through the SSG a heat input of nearly 250 MWh/h is transferred to
the water steam cycle. Thus, the booster goes into full load and delivers steam at
300
Q_SSG Q_Heater
W_net Q_Booster
200
100
0 1
800
400
600
200
0 3 5 7 9
local time
o u
tp u
t [M
W h
/h ]
(b ar
s)
D N
I [ W
/m 2 ]
; p
S T ,o
u t [
m b
ar ]
T S
T ,in
[ °C
] (c
u rv
es )
11131517192123
T_ST_in p_ST_out DNI
800
400
600
200
0 D N
I [ W
/m 2 ]
; p
S T ,o
u t [
m b
ar ]
T S
T ,in
[ °C
] (c
u rv
es )
o u
tp u
t [M
W h
/h ]
(b ar
s)
local time
1 3 5 7 9 11131517192123
300
200
100
0
Fig. 36.6 Performance values (bars) and process parameters (curves) for the (a) 25th March and (b) 17th July
36 Hybridization of Parabolic Trough Power Plants with Natural Gas Through. . . 485
540 �C. Despite the later on slight reduction of the in the SSG transferred heat into the water steam cycle the steam temperature at steam turbine inlet is constant at
540 �C, due to the approach of smoothed live steam temperature. During night the steam turbine is cooling out. In spring the ambient temperature is on a moderate
level, wherefore the steam turbine outlet pressure is obvious lower than the limi-
tation of 230 mbar.
A summer day with a short-term insolation drop is shown in Fig. 36.6b with the
17th July. In comparison with Fig. 36.6a it is easy to identify that for that summer
day the maximum electrical net output is not reached. This is caused by the hot
ambient temperature (at that day roughly 39 �C) and is typical for the chosen design of the power plant with an ACC, whereby a solution could be to overdesign the
ACC. The high ambient temperature yields to a large steam turbine outlet pressure
with an ACC. For the shown example the maximum steam turbine outlet pressure is
reached. For that reason the fossil input is lowered to the technical lowest level,
e.g. steam turbine wetness limitation. Therefore the steam turbine inlet temperature
is even at high DNI not at 540 �C but rather at 490 �C (12:00), which is typical for the summer period. The drop in the transferred heat through the SSG between 12:00
and 13:00 indicates that supportive the solar field is defocussed in order to lower the
power plant load. After 13:00 there is a sudden insolation drop (753 Wh/(m2h)! 111 Wh/(m2h)), which is why the HTF-heater starts its operation and enables a
steady transferred heat to the water/steam cycle. In the late afternoon the DNI is
raising again, so that the HTF-heater is turned off.
The distribution of all base case power plant operating points with a positive net
power output are shown in Figs. 36.7 and 36.8. Based on these two diagrams the
functionality of the developed operational logic will be discussed in detail.
In Fig. 36.7 the steam turbine exhaust pressure is plotted against the ambient
temperature. Due to the different part load status of the power plant a certain
ambient temperature leads to different steam turbine exhaust pressures. The
steam turbine exhaust pressure increases with rising power plant load. For that
Fig. 36.7 Annual distribution of steam turbine
(ST) outlet pressure with
respect to the ambient
temperature
486 T. Vogel et al.
reason two curves form out, which represent the curve for min load (point 3) and
curve for full load (point 2) of the power block as function of the ambient
temperature. As already mentioned the maximum tolerable turbine exhaust pressure
is 0.23 bar. This limitation is trespassed at high ambient temperatures with concur-
rent high load status of the power block. Through the operating logic these critical
operating points are transferred into an operating point where this limitation is
satisfied. Herefrom the perpendicular in the upper right part of the passel in
Fig. 36.7 indicated by point 1, is formed out. The volume factor of the volume
flow at steam turbine outlet is limited to 1.5. This limitation is most critical at low
condenser pressure with simultaneously high part load status and is depicted in
Fig. 36.7 by the notch in the passel at point 4.
Figure 36.8 shows the dependency of live steam pressure versus steam quality at
steam turbine outlet at ELEP for the operating points. The steam quality describes
the share of saturated steam (vapor) in a saturated condensate (liquid) and saturated
steam (vapor) mixture. The passel at point 1, with operating points corresponding to
a steam turbine inlet pressure of lower than 40 bar and a steam quality at steam
turbine outlet of lower than 0.87, located in the lower left part in Fig. 36.8
represents the solar only operating points. In the morning as long as the steam
wetness limitation is satisfied the power plants runs in solar only mode. When the
load is increasing due to higher solar insolation with respect to the simultaneously
raising live steam pressure, caused by the sliding pressure mode of the steam
generator, the steam wetness is also increasing. For that reason the booster goes
into operation. The minimum allowed steam wetness at ELEP is 15%, which
corresponds with a steam quality of 0.85. Because of the booster’s min load of 5% the set point of the controller regulating the boosters load is set to adapt the
booster load in order to enable a steam quality at ELEP of 0.86. For that reason is at
a steam quality of 0.86 a perpendicular (point 2). But when the booster is already at
full load and delivers a live steam temperature of 540 �C and owing to a relatively low ambient temperature a low condenser pressure arises the booster cannot fulfill
the steam wetness limitation. In order to fulfill the requirement the load of the
Fig. 36.8 Annual distribution of steam quality
at the steam turbine
(ST) outlet with respect to
the live steam pressure
36 Hybridization of Parabolic Trough Power Plants with Natural Gas Through. . . 487
power block must be reduced for example by reducing the solar heat through
defocussing. The upper end of the passel at 100 bar (point 4) indicates the power
blocks full load. There the steam quality is only depending on the ambient
temperature.
In conclusion the annual yield simulation for the base case power plant has
shown so far, that due to the chosen operating logic and the process layout nearly all
operating points differ from each other. Therefore it is very important to perform
the annual yield simulations with a fully thermodynamically model and not by
characteristic curves.
Cross Comparison
A cross comparison of the results from the annual yield simulation for the four
examined configurations of the case study is given with their main performance
parameters in Table 36.3.
As a common constraint the incident solar energy is in all configurations the
same, owing to the identical solar field and the uniform site. The yearly operating
hours of all configurations are very similar and lay in a range of 3231–3246 h per
year. For that reason the theoretical as well as the used solar heat input to the HTF
are also in a similar magnitude. Referring to the incident solar energy the amount of
Table 36.3 Comparison of the simulation results of the annual yield analysis for the configura- tions of the case study
Simulation results Solar only BC BCþGTa) BCþGTb) Units Available DNI 1889.38 1889.38 1889.38 1889.38 kWh/(m2 a)
Net aperture area 627,786.55 627,786.55 627,786.55 627,786.55 m2
Incident solar energy 783.72 783.72 783.72 783.72 GWhth/a
Operating hours 3241 3231 3243 3246 h
Theoretical available
solar heat input to HTF
682.63 682.27 683.30 683.51 GWhth/a
Used solar heat input to
HTF
636.46 635.99 637.26 637.54 GWhth/a
Total gross electricity
steam turbine
234.57 282.45 286.84 285.64 GWhel/a
Total net electricity gas
turbine
0.00 0.00 26.05 28.98 GWhel/a
Net electricity 220.65 266.55 296.99 298.72 GWhel/a
Supplied energy from
natural gas
13.38 126.05 198.29 195.22 GWhth/a
Design-point net plant
efficiency
18.89 21.65 22.75 22.66 %
Annual net plant
efficiency
18.40 20.31 21.45 21.62 %
Annual solar fraction 97.94 83.46 76.27 76.56 %
488 T. Vogel et al.
used solar heat input to HTF ranges between 81.2% (solar only) to 81.3%
(BCþGT configurations). The gross electricity of the BCþGT configurations is elevated based on the BC model by 3.2–4.4 GWhel/a owing to the gas turbine’s waste heat integration. Comparing the BCþGT configurations, the larger available waste heat amount for GTa) yields to a 1.2 GWhel/a larger steam turbine gross
electricity output. Due to the better electrical efficiency of GTb) the benefit of GTa)
in terms of steam turbine gross electricity output has been overcompensated so that
the overall produced net electricity of GTb) is 1.7 GWhel/a larger than the one for
GTa). The net electricity output of the solar only system amounts to 220.65 GWhel/
a. The BC offers a 20.8% higher net electricity output whereby the supplied energy
from natural gas is raised by the factor 9.4. Through an additional GT-integration
the net electricity output is additional raised by 11.4–12.1%, while the gas con-
sumption is increased by 50%. The solar only model has because of the lower live
steam temperature the lowest design-point net efficiency of 18.89%. Following the
hybridization the live steam temperature is elevated from 380 to 540 �C which leads for the BC to a 2.76%-points higher design-point net efficiency. Through the
further combination with gas turbines the design-point net efficiency could be
raised by additional 1–1.1%-points. For the solar only model the design point net
plant efficiency and the annual net plant efficiency differ with absolute 0.5%-points
not that much, owing to very constant process parameters. For the hybrid config-
urations the difference between design-point and the annual value is larger and
ranges between 1- and 1.3%-points. This is especially caused by different process
parameters between different operating states, e.g. the live steam temperature varies
during operation between 380 and 540 �C. In analogy to the supplied energy from natural gas the annual solar fraction decreases beginning with 97.9% for the solar
only model upon further hybridization to 83.5% (BC) and finally round about
76.3–76.6% for the BCþGT configurations. For the energetic comparison between the hybrid configurations the conversion
efficiency of fuel into electricity ηfuel is introduced, which is defined by Eq. (36.1).
ηf uel ¼ ΔPnet,hybrid�solar Δ _Q hybrid�solar
¼ Pnet,hybrid � Pnet, solar _Q hybrid � _Q solar
ð36:1Þ
Therefore the difference of the produced net electricity of the hybrid power plant
and the solar only benchmark model is divided by the difference of the used fuel,
whereby also the hybrid case is subtracted from the solar only benchmark model.
The resulting ηfuel for the hybrid configurations is visualized in Fig. 36.9. Referring to the solar only bench mark model described in chapter 5 and the
results of the performed annual yield simulation the ηfuel amounts for the base case power plant to 40.74%. Through integrating industrial gas turbines the overall
conversion efficiency of fuel into electricity could be elevated compared to the base
case power plant. The highest increase, with absolute 2.20%-points could be
achieved by integrating GTb) in the BC. But even with the configuration
BCþGTa) an enhancement of ηfuel could be realized with a plus of 0.55%-points. Comparing these numbers, while taking the 3.8%-points better electrical efficiency
36 Hybridization of Parabolic Trough Power Plants with Natural Gas Through. . . 489
of GTb) at the design-point into account, the absolute advantage is lessened through
the integrated configuration. This effect is mainly caused by the fact, that the gas
turbine GTa) with a lower electrical efficiency offers at design point a 19% higher
waste heat potential than the GTb). Following this, the amount of bled steam for the
configuration BCþGTa) could be lowered, which leads to the higher steam turbine gross electricity of round about 1.2 GWhel/a.
As mentioned in the introduction a certain amount of peaker gas turbines is
installed in the UAE. For the evaluation of the advantage of a combined usage in
comparison to a separated configuration the electricity to fuel ratio is used. For the
separated production the gas turbine’s waste heat is not integrated into the base case power plant. Due to missing information on the operation scheme of the peaker gas
turbines in UAE, this evaluation was simplified in that way, that the operating hours
of the peaker gas turbine are similar with the base case power plant. The following
values are also based on the yearly values.
As Fig. 36.10 shows, within a combined production the electricity to fuel ratio
could be elevated depending on the configuration round about 0.17–0.19 MWhel/
Fig. 36.9 Annual conversion efficiency of fuel into electricity for the three hybrid configurations BC, BCþGTa) and BCþGTb) of the case study
Fig. 36.10 Fuel to efficiency ratio for the two BCþGT configurations for separated and com- bined production
490 T. Vogel et al.
MWhth. Based on the above mentioned assumptions for the two BCþGT config- urations 4.4–5 MtCO2/a could be saved towards a separated production.
Conclusions
In the present publication the hybridization of parabolic trough power plants using
state of the art thermal oil as HTF with natural gas has been evaluated based on the
power plant configuration of Shams One. In a first step for this base case model a
detailed operational logic has been developed in order to fulfill all technical
constraints. In a second step a further hybridization through integrating gas turbines
in the performance class of 10–20 MWel has been done, whereby two different gas
turbines has been used in order to cover the range. For this purpose of evaluating the
fuel to electricity conversion efficiency in addition a solar only reference model has
been prepared. For all these configurations annual yield simulations have been
performed.
It is shown, by example of the base case model, that through the developed
operational logic the identified main technical boundary conditions are satisfied.
Through the hybridization done in the base case model, based on Shams One, the
net efficiency could be raised by 2.76%-points for design-point and 1.92%-points
for annual view in comparison to the solar only reference model. The annual fossil
fuel to electricity conversion efficiency amounts to 40.74%. By integrating addi-
tionally a gas turbine this efficiency value could elevated by another 2.2%-points
up to 42.94%. Supplementary to this absolute efficiency improvement, the com-
bined production has versus to the separate production a better electricity to fuel
ratio and thereby saves CO2. Here it should be noted, that therefore the assumptions
for gas turbine operation are deciding. Furthermore, the operation flexibility of the
peaker gas turbine is in the combined approach not affected.
All in all the hybridization of parabolic trough power plants using a HTF limited
to 400 �C with natural gas offers the opportunity to improve the power plant in terms of live steam parameters, efficiency and flexibility.
As brief outlook on the economy it has to be noted, that a gas turbine integration
in the evaluated arrangement offer a reduction potential for the levelized costs of
electricity, which amounts with the used assumptions to round about 5–6%.
Acknowledgements The authors would like to thank the German Federal State of North Rhine- Westphalia and the European Regional Development Fund for the financial support of the project
TURIKON in the frame of the program progress. NRW and the goal 2-program 2007–2013, Phase
VI (Grant No. 64.65.69-EN-2019).
36 Hybridization of Parabolic Trough Power Plants with Natural Gas Through. . . 491
Nomenclature
ACC Air-cooled condenser
BC Base case
CSP Concentrating solar power
DNI Direct normal irradiance, W/m2
ELEP Expansion line end point
GT Gas turbine
HTF Heat transfer fluid
HP High pressure
FH Feed heater
IP Intermediate pressure
ISCC Integrated solar combined cycle
LP Low pressure
p Pressure, bar or kPa
P Power output, W
Q Thermal output, W
SSG Solar steam generator
ST Steam turbine
T Temperature, �C UAE United Arab Emirates
Greek Letters
Δ Difference ηel Efficiency, %
Subscripts
out Outlet
in Inlet
hybrid Hybrid configuration
net Net
solar Solar configuration
el Electrical
fuel Fuel
mech Mechanical
s Isentropic
492 T. Vogel et al.
References
Al Mirfa Power Company. http://www.ampc.ae/en/production/. Retrieved November 27, 2014.
Balan, R. (2014). Simulation des transienten Verhaltens von Parabolrinnenkraftwerken. Master thesis. Essen: University of Duisburg-Essen.
BP. (2014). BP energy outlook 2035. bp.com/energyoutlook. Retrieved March 16, 2015. Gas Turbine World. (2011).Gas turbine world 2011-Performance Specs. Pequot Publishing. ISSN
0746–4134, (27th ed., Vol. 41 No.1).
Goebel, O. (2010). Shams one 100 MW CSP plant in Abu Dhabi—Update on Project Status.
Proceedings of the SolarPACES 2010 Conference. Perpignan, France. Goebel, O., & Luque, F. (2012). Shams One 100 MW CSP Plant in Abu Dhabi. Update on
Proceedings of the SolarPACES 2012 Conference. Marrakesch: Marocco.
Lechner, C., & Seume, J. (2010). Station€are Gasturbinen. e-ISBN 978-3-540-92788-4. (2nd ed.). Heidelberg: Springer-Verlag Berlin.
MAN. http://www.corporate.man.eu/man/media/content_medien/images/global_corporate_website/
presse_und_medien/mdt/2013_2/T_Turbinenlaeufer.jpg. Retrieved December 29, 2014.
Pawellek, R., L€ow, T., & Hirsch, T. (2009). EbsSolar—a solar library for Ebsilon®Professional. Proceedings of the SolarPACES 2009 Conference. Berlin, Germany.
Reuß, N. (2012). Modern gas and steam turbines in solarthermic applications. 14th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC).
Honolulu, HI, USA.
Schr€oder, K. (1966). Große—Dampfkraftwerke—Planung Ausf€uhrung und Bau, Dritter Teil A. Berlin: Springer.
Servert, J. F., Cerrajero, E., Lopez, D., Yagüe, S., Gutierrez, F., Lasheras, M., & San Miguel, G.
(2014). Base case analysis of a HYSOL power plant. Proceedings of the SolarPACES 2014 Conference. Bejing, China.
SOLUTIA. Product data sheet—therminol VP-1. http://twt.mpei.ac.ru/TTHB/HEDH/HTF-VP1. PDF. Retrieved May 6, 2013.
TRANSCO. (2014). Seven year electricity planning statement (2014–2020)—report. http://www. transco.ae/media/docs.htm. Retrieved November 27, 2014.
Turchi, C. S., Ma, Z., Erbes, M. (2011).Gas turbine/solar parabolic trough hybrid designs. ASME Turbo Expo 2011. Vancouver, Canada.
United Arab Emirates. (2012). Annual statistical report—electricity and water 2012. Ministry of Energy. Abu Dhabi, Dubai.
Vogel, T., Oeljeklaus, G., G€orner, K. Dersch, J., & Polklas, T. (2013). Hybridization of parabolic trough power plants with natural gas. Energy Procedia 49 (2014)—Proceedings of the SolarPACES 2013 Conference. (pp. 1238–1247). Las Vegas, USA.
36 Hybridization of Parabolic Trough Power Plants with Natural Gas Through. . . 493
Part X
Energy Technologies and Their Effect on Global Warming
Thermodynamic System Analysis and Optimization
Specific cases of system analysis and optimization
Chapter 37
Performance Analyses of CO2-N2O Cascade System for Cooling
Fatih Yılmaz, Reşat Selbaş, Arif Emre €Ozgür, and M. Tolga Balta
Introduction
Because of environmental issues associated with the global warming and ozone
layer depletion attributed to the application of synthetic refrigerants chlorofluoro-
carbons (CFC’s), hydrochlorofluorocarbons (HCFC’s) and hydrofluorocarbons (HFC’s), the return to the usage of natural materials for cooling system appears to be an appropriate alternative. Accordingly, the natural refrigerants such as
ammonia, carbon dioxide and hydrocarbons, have recently received increasing
attentions (Dopazo et al. 2009). Amongst the natural refrigerants, the suggested
of the use of CO2 seems to be the most promising especially as the natural
refrigerant (Lorentzen and Petterson 1993). The CO2 including that non-toxic,
easily available, excellent thermophysical properties and not explosive. N2O refrig-
erant, which is alternative of CO2 in terms of thermophysical properties. N2O
refrigerants’ disadvantage is, its global warming potential (GWP) is higher than CO2.
The cooling systems involving a high temperature difference between the
condenser and the evaporator, employing a single stage cooling system is not
F. Yılmaz (*) Department of Energy, Vocational Schools of Technical Sciences, Aksaray University,
68100 Aksaray, Turkey
e-mail: [email protected]
R. Selbaş • A.E. Özgür
Department of Energy Systems Engineering, Faculty of Technology, Suleyman Demirel
University, 32100 Isparta, Turkey
e-mail: [email protected]; [email protected]
M.T. Balta
Department of Mechanical Engineering, Faculty of Engineering, Aksaray University,
68100 Aksaray, Turkey
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_37
499
economical because of the corresponding high pressure ratio leads to a low volu-
metric efficiency of the compressors and consequently low coefficient of perfor-
mance of the system. In conditions cascade cooling cycle is more appropriate.
Cascade cooling cycles are generally in low evaporating temperature applications,
which is evaporating temperature between�40 �C and�130 �C. A commonly used refrigerants pair in the past has been R12, R502 in high temperature cycle and R13
in low temperature cycle of cascade refrigeration system. These refrigerants have
been phased out since 1996 in the developed countries, and should be totally phased
out by 2010 in developing countries as per Montreal Protocol and its amendments
from the United Nations Environment Programme (UNEP 1987, 2007). Currently,
many manufacturers tend to use natural refrigerants due to environmental problems
and harmful effects synthetic refrigerants. CO2/N2O cascade system uses N2O in
the high temperature cycle and CO2 in the low temperature cycle. N2O is natural
refrigerant.
Ratts and Brown (2000) shows that the entropy generation method to analyze the
cascade cycle. In their work, relationships were developed for the specific heat and
temperature ratio terms and the results were investigated for a cascade system in
two low temperatures of 0.684 and 0.681, with the refrigerant R-134a and finally,
the optimum temperature distribution was found. The study the optimum temper-
ature in a cascade condenser, maximized the coefficient of performance and
minimized the exergy destruction of the system, CO2 is using the evaporation
temperature and NH3 is condensation temperature carried out by (Lee et al. 2006).
Energy and irreversibility analysis of a cascade refrigeration system employing
various refrigerant couples using a computer code carried out by (Kilicarslan and
Hosoz 2010). Bansal and Jain (2007) shown that evaluated the optimum cascade
condensing temperature of CO2 when different refrigerants such as NH3, propane,
propylene and ethanol are used in the high temperature circuits of a subcritical
cascade system. Bhattacharyya et al. (2005) shows that an optimization research of
the CO2/C3H8 cascade system for cooling and heating. Analyzed a vapor compres-
sion heat pump working with R11 and a vapor compression refrigeration system
operating with R12 cascaded to produce heating and cooling effects simultaneously
carried out by (Murthy and Murthy 1985). Bhattacharyya et al. (2009) give in that
thermodynamic analysis and optimization of a novel N2O–CO2 cascade system for
refrigeration and heating. They study, a natural refrigerant based cascaded system,
with nitrous oxide as the low temperature fluid and carbon dioxide as the high
temperature fluid, is analyzed for simultaneous cooling and heating applications.
In literature generally CO2 and NH3 refrigerants in cascade cooling system were
compared. In this study, a cascade system for cooling with N2O as the high
temperature fluid and CO2 as the low temperature fluid is theoretical analyzed.
Thermodynamic analysis of cooling system as evaporator temperature variations
and pumps inlet pressure variations are investigated. Also, the effects of operating
parameters on system performance are studied and illustrated in tables. The effect
on the system performance of the heat exchangers are also investigated and given in
figures.
500 F. Yılmaz et al.
Performance Analyses of CO2-N2O Cascade
A schematic diagram of a cascaded CO2 and N2O cooling system is given in Fig. 37.1
and the corresponding P–h diagram is shown Fig. 37.2. This cooling system includes
two separate circuits, one high temperature circuit (HTC) with N2O as the refrigerant
and the other one, low temperature circuit (LTC) with CO2 as the refrigerant. The
analysis was carried out as subcritical cycle. HTC of condenser as water cooler
condenser is discussed. These two circuits are thermally coupled using a heat
exchanger which acts as an evaporator for the HTC and a condenser for the LTC.
The natural fluid N2O has a triple point �90.82 �C. Furthermore similarity between critical temperature N2O and CO2. Table 37.1 given in thermodynamic
properties of CO2 and N2O.
Each refrigeration system consists of a compressor, a condenser, an expansion
valve, and an evaporator. In this study N2O is the refrigerant in HTC, whereas CO2 is the refrigerant in LTC. The circuits are thermally connected to each other through
a heat exchanger, which acts as an evaporator for the HTC and a condenser for the
LTC. The evaporator of LTC absorbs the cooling load from the cooling space. The
condenser in HTC rejects heat flow at condensing temperature.
The cascade cooling system components shown in Fig. 37.1 can be treated as a
control volume. The thermodynamic analysis of the cascade cooling system was
performed based on the following general assumptions;
Fig. 37.1 Schematic diagram of the CO2-N2O cascade refrigeration system
37 Performance Analyses of CO2-N2O Cascade System for Cooling 501
• Refrigerants at the cascade heat exchanger and outlet for HTC cycle and
evaporator for LTC cycle outlet are saturated.
• The changes in kinetic and potential energy are negligible.
• Adiabatic and irreversible compression in HTC with an isentropic efficiency of
0.8.
• Negligible pressure and heat losses in the pipe networks or system components.
• All system components operate under steady-state conditions.
• NH3Heat transfer processes in cascade heat exchanger, condenser and evapora-
tor are isobaric.
• Ambient (dead state) temperature (T0) 21 �C and ambient pressure (P0) 1 bar.
The thermodynamic properties of CO2 and NH3 were determined using Engi-
neering Equations Solver (EES). EES can generate publication-quality plots, do
optimization, provide linear and non-linear regression, solve equations and simplify
uncertainty analyses.
Taking into account the assumptions previously made, mass and energy balances
are given by Eqs. (37.1) and (37.2), respectively.
For the steady-state process, the mass, energy and exergy balance for the each
control volume can be expressed as follows;
N2O
CO2
102
3
4
0.2 0.4 0.6 0.8
7 6
2 5
1 1
8
103
h [kJ/kg]
P [
B ar
] 104
Fig. 37.2 A schematic P-h diagram of the CO2-N2O cascade refrigeration system
Table 37.1 Thermodynamic properties of CO2 and N2O
Property CO2 N2O
Critical pressure (bar) 73.77 72.45
Critical temperature (�C) 30.98 36.37 Triple point temperature (�C) �56.56 �90.82 Molecular weight (kg/kmol) 44.01 44.01
502 F. Yılmaz et al.
X _m in ¼
X _mout ð37:1Þ
where _m: is the mass flow rate, and the subscript in stands for inlet and out for outlet. The mass balance equation can be expressed in the rate form as with all energy
terms as follows (Cengel and Boles 2008)
_Q � _W þ X
_m inh� X
_mouth ¼ 0 ð37:2Þ
The general exergy balance can be expressed in the rate form as;
_Exin � _Exout ¼ _Exdest ð37:3Þ _Exheat � _Exwork þ _Exmass, in � _Exmass,out ¼ _Exdest ð37:4Þ
Using Eq. (37.4), the rate form of the general exergy balance can also be written
as
X 1� T0
Tk
� � _Q k � _W þ
X _m inψin �
X _moutψout ¼ _Exdest ð37:5Þ
where _Q k is the heat transfer rate through the boundary at temperature, Tk at
location k, _W: is the work rate, I ? is the flow (specific) exergy, h is enthalpy, s is entropy, and the subscript zero indicates properties at the restricted dead state of P0 and T0.
The specific exergy (flow exergy) of refrigerant (or water) is calculated by;
ψ ¼ h� h0 � T0 s� s0ð Þ ð37:6Þ
The exergy rate is calculated by;
_Ex ¼ _m ψ ð37:7Þ
Energy (or first law) efficiency of the cascade cooling system and exergy
efficiency are determined as follows, respectively,
COP ¼ _Q ev
_WN2O þ _WCO2 ð37:8Þ
ε ¼ _Exout _Exin
ð37:9Þ
where out refers to “net output” or “product” or “desired value”, and in refers to
“given” or “used”.
For LTC compressor (I);
37 Performance Analyses of CO2-N2O Cascade System for Cooling 503
_mCO2 ¼ _m1 ¼ _m2 ð37:10Þ
PrCO2 ¼ P2
P1 ð37:11Þ
ηCO2 isen ¼ 0, 815þ 0, 022 * PrCO2 � 0, 0041 * P2rCO2 þ 0, 0001 * P3rCO2 ð37:12Þ
ηCO2 isen ¼ h2s � h1 h2 � h1 ð37:13Þ
where the heat transfer versus the environment was neglected. Equation (37.12)
depending on the LTC of compressor isentropic efficiency the compressor outlet
enthalpy is calculated (Robinson and Groll 1998).
_WCO2 ¼ _mCO2 h2 � h1ð Þ ð37:14Þ _Exdest, comp ¼ _mCO2 ψ1 � ψ2ð Þ þ _WCO2 ð37:15Þ
For LTC condenser–HTC evaporator (heat exchanger) (II);
_mCO2 ¼ _m2 ¼ _m3 ð37:16Þ _mN2O ¼ _m8 ¼ _m5 ð37:17Þ
_Q hexc ¼ _mN2O h5 � h8ð Þ ¼ _mCO2 h2 � h3ð Þ ð37:18Þ _Exdest, hexc ¼ _mCO2 ψ3 � ψ2ð Þ þ _mN2O ψ8 � ψ5ð Þ ð37:19Þ
The heat rate exchanged and exergy destruction from LTC to HTC in the heat
exchanger is called _Q hexc and can be calculated by Eqs. (37.18) and (37.19). For expansion valve (III)
_mCO2 ¼ _m3 ¼ _m4 ð37:20Þ h3 ¼ h4ð Þ ð37:21Þ
_Exexp ¼ _mCO2 ψ3 � ψ4ð Þ ð37:22Þ
The expansion valve exergy destruction is calculated with Eq. (37.22). Where
expansion valve of heat transfer is neglected.
For LTC evaporator (IV);
_mCO2 ¼ _m4 ¼ _m1 ð37:23Þ _Q ev ¼ _mCO2 h1 � h4ð Þ ð37:24Þ
_Exdest, evap ¼ _mCO2 ψ4 � ψ1ð Þ þ _Q ev 1� To
TEV
� � ð37:25Þ
504 F. Yılmaz et al.
The evaporator heat rate and exergy destruction is calculated with Eqs. (37.23)
and (37.24). Where is the T0 is ambient temperature (dead state), TE is evaporator
temperature.
For HTC compressor (v);
_mN2O ¼ _m5 ¼ _m6 ð37:26Þ _WN2O ¼ _mN2O h6 � h5ð Þ ð37:27Þ
_Exdest, comp ¼ _mN2O ψ6 � ψ5ð Þ þ _WN2O ð37:28Þ
The HTC compressor exergy destruction is calculated with Eq. (37.28).
For HTC condenser (VI);
_mN2O ¼ _m6 ¼ _m7 ð37:29Þ _Q con ¼ _mN2O h6 � h7ð Þ ð37:30Þ
_Excon ¼ _mN2O ψ4 � ψ1ð Þ � _Q con 1� To
TCON
� � ð37:31Þ
The condenser heat rate and exergy destruction is calculated with Eqs. (37.30)
and (37.31). Where is the T0 is ambient temperature (dead state), Tc is condenser
temperature.
For expansion valve (VII)
_mN2O ¼ _m7 ¼ _m8 ð37:32Þ h7 ¼ h8ð Þ ð37:33Þ
_Exexp ¼ _mN2O ψ7 � ψ8ð Þ ð37:34Þ
The expansion valve exergy destruction is calculated with Eq. (37.34). Where
expansion valve of heat transfer is neglected.
Results and Discussion
A performance analysis of the cascade cooling with CO2-N2O system is investi-
gated using energy and exergy analysis. Under the assumptions, the calculated
properties for cascade cooling system are given in Table 37.2. The cooling coeffi-
cient of performance and exergy efficiency of the cascade system (COP) is calcu-
lated from Eqs. (37.8) and (37.9) and is found to be 2.061% and 35%, respectively.
Figure 37.3 displays the effect of evaporator temperature on COP and exergy
efficiency cycle. As can be seen in Fig. 37.3. The cycle of evaporator temperature
25 �C, by increasing evaporator temperature the system of COP and exergy efficient has increased. While evaporator temperature �50 �C, COP and exergy efficiency
37 Performance Analyses of CO2-N2O Cascade System for Cooling 505
are 1.055% and 25%, respectively. In Fig. 37.3, the systems are represented COP
and the exergy efficiency trends with increases in evaporator temperature.
The systems of the COP and exergy efficiency effect on condenser temperature
can be observed in Fig. 37.3.
Table 37.2 Exergy analysis results of the cascade cooling system studied for one representative unit
State
no Fluid Phase
Temperature
(�C) Pressure
(bar)
Specific
enthalpy
(kJ/kg)
Specific
entropy
(kJ/kg K)
Exergy
rate
(kW)
1 CO2 saturated
vapor
�23 14.28 �62.17 �0.7095 11.81
2 CO2 Super-
heated
vapor
66.58 45.02 0.2552 �0.6806 14.28
3 CO2 Comp.
liquid
15.72 45.02 �264.6 �1.596 20.42
4 CO2 Mixture �30 14.28 �264.6 �1.542 19.28 5 N2O saturated
vapor
10 33.7 408.9 1.594 13.45
6 N2O Super-
heated
vapor
52.14 56.51 435.4 1.611 14.88
7 N2O Comp.
liquid
20 56.51 212.5 0.87 15.58
8 N2O Mixture 3 33.7 212.5 0.8839 15.29
-50 -45 -40 -35 -30 1
1.2
1.4
1.6
1.8
2
2.2
0.24
0.26
0.28
0.3
0.32
0.34
0.36
e
C O
P
TEV (°C)
TCON = 25 (°C)
Fig. 37.3 Effect of evaporator temperature on COP and exergy efficiency
506 F. Yılmaz et al.
In this system with increases condenser temperature, COP and exergy efficiency
is decreases shown in Fig. 37.3. While evaporator temperature �30 (�C) and the condenser temperature is 20 (�C), the cycle of COP and exergy efficiency are shown 2.28% and 39%, respectively.
Figure 37.4 given in the effect of N2O compressor isentropic efficiency on the
cycle COP and exergy efficiency. While condenser and evaporator temperature are
fixed respectively 25 (�C), �30 (�C), with HTC compressor isentropic efficiency increases, COP and exergy efficiency are increases can be observed in Fig. 37.5. As
the compressor isentropic efficiency up to 90% on, the cycle of COP value rise up
to 2.14. The figurate result in understand that if the compressor isentropic efficiency
is increases, the system of increases COP and exergy efficiency.
The system effect of heat exchanger efficiency on COP and exergy efficiency
illustrated in Fig. 37.6. When the refrigeration cycle of heat exchanger efficiency is
rise up from 60% to 95%, the system of increases COP and exergy efficiency.
Figure 37.5 shows that evaporator temperature and condenser temperature are fixed
“�30 (�C), 25 (�C)”, while heat exchanger efficient is 75%, the systems of COP and exergy efficiency are calculated 1.986 34%, respectively.
Figure 37.6 shows that heat exchanger efficiency and evaporator temperature
changed on the system COP and exergy efficiency. The system of condenser
temperature 25 (�C) is fixed, as the heat exchanger efficiency is increases, which is fixed evaporator temperature, the system increases of COP. When the system of
heat exchanger efficiency and evaporator temperature are increased, the system is
increases of COP value observed in Fig. 37.6.
Figure 37.7 demonstrates the variation in the exergy destruction of different
components of the cascade refrigeration system. According to this figure, the
Fig. 37.4 Effect of condenser temperature on COP and exergy efficiency
37 Performance Analyses of CO2-N2O Cascade System for Cooling 507
highest amount of exergy destruction rate takes place in the evaporator (18.08 kW).
The lower amount of destruction rate take place in HTC and LTC expansion valves
is are calculated 0.029 and 0.06 respectively.
The effect on evaporator temperature on the exergy destruction at the system
components and COP the whole system at different evaporator temperature values
are demonstrated at Fig. 37.9. The exergy destruction occurs given in figurate HTC
0.8 0.82 0.84 0.86 0.88 0.9 2.06
2.08
2.1
2.12
2.14
2.16
0.355
0.36
0.365
0.37
0.375
e
C O
P
ηcomN2O
TCON = 25 (°C)
TEV = -30 (°C)
Fig. 37.5 Effect of N2O compressor isentropic efficiency on COP and exergy efficiency
0.6 0.65 0.7 0.75 0.8 0.85 0.9 0.95 1.6
1.7
1.8
1.9
2
2.1
2.2
2.3
0.28
0.3
0.32
0.34
0.36
0.38
0.4
h hexc
e
C O
P
TCON = 25 (°C)
TEV = −30 (°C)
Fig. 37.6 Effect of heat exchanger efficiency on COP and exergy efficiency
508 F. Yılmaz et al.
compressor, LTC compressor and heat exchanger. The system COP increases from
1.33 to 2.88 with evaporator temperature increase from �40 �C to �10 �C. But the system of HTC and LTC compressor exergy destruction rate are decreases with
increase of evaporator temperature shown that Fig. 37.9.
Fig. 37.7 Effect of heat exchanger efficiency and evaporator temperature on COP and exergy efficiency
Fig. 37.8 The exergy destruction values in different components of cascade refrigeration system
37 Performance Analyses of CO2-N2O Cascade System for Cooling 509
Conclusion
In this paper, a cascade system for cooling is with N2O-CO2 fluids as theoretical
performance analyzed according to thermodynamic assessment in order to investi-
gate cascade system COP and exergy analysis. According to condenser and evap-
orator temperature exchanges the system of COP and exergy efficiency are
investigated. This paper as a refrigerants environmentally friendly fluids CO2 and
N2O are used. The main concluding remarks have been given as follows;
• This cascade refrigeration cycle is subcritical and therefore water-cooled con-
denser was adopted.
• While the system of condenser temperature at 25 (�C) is fixed, evaporator temperature�30 (�C), the system of COP and exergy efficiency are respectively 2.1% and 36%.
• As the system of evaporator temperature is increased, COP and exergy efficiency
are increases.
• Evaporator temperature in �30 (�C), if the condenser temperature is increases the system of COP and exergy efficiency are decreased.
• Exergy efficiency have been calculated to be between 28% and 39%.
• COP and exergy efficiency are increased as the heat exchanger efficiency is
increased. Therefore, the more highly efficient heat exchanger are used, the more
exergy efficiency highly.
-45 -40 -35 -30 -25 -20 -15 -10 -5 0
1
2
3
4
5
1
1.5
2
2.5
3 E
xe rg
y D
es tr
uc tio
n R
at e
(k W
)
Heat exchanger LTC comp.HTC comp.
C O
P
COP
TEV(°C)
Fig. 37.9 Exergy destruction at the system components and COP the whole system at different evaporator temperature values
510 F. Yılmaz et al.
Nomenclature
COP Coefficient of performance
Ex Exergy flow rate (kW)
Exdes Exergy destruction
h Specific enthalpy (kJ/kg)
_m Mass flow rate (kg/s) _Q Heat flow rate (kW)
s Specific entropy (kJ/kg K)
T Temperature (K or �C) _W Work rate or power (kW)
ψ Specific exergy (kJ/kg) η Efficiency (dimensionless) ε Exergy (second law) efficiency (dimensionless) in Inlet
out Outlet
des Destruction
ev Evaporator
con Condenser
exp Expansion valve
comp Compressor
hexc Heat exchanger
isen Isentropic
LTC Low temperature cycle
HTC High temperature cycle
References
Bansal, P. K., & Jain, S. (2007). Cascade systems: Past, present, and future. ASHRAE Trans- actions, 113(1), 245–252.
Bhattacharyya, S., Garai, A., & Sarkar, J. (2009). Thermodynamic analysis and optimization of a
novel N2O–CO2 cascade system for refrigeration and heating. International Journal of Refrig- eration, 32, 1077–1084.
Bhattacharyya, S., Mukhopadhyay, S., Kumar, A., Khurana, R., & Sarkar, J. (2005). Optimization
of a CO2–C3H8 cascade system for refrigeration and heating. International Journal of Refrig- eration, 28, 1284–1292.
Cengel, Y. A., & Boles, M. A. (2008). Thermodynamics: An engineering approach (6th ed.). New York: McGraw-Hill.
Dopazo, J. A., Fernández-Seara, J., Sieres, J., & Uhı́a, F. J. (2009). Theoretical analysis of CO2-
NH3 cascade refrigeration system for cooling applications at low temperatures. Applied Thermal Engineering, 29, 1577–1583.
Kilicarslan, A., & Hosoz, M. (2010). Energy and irreversibility analysis of a cascade refrigeration
system for various refrigerant couples. Energy Conversion and Management, 51(12), 2947–2954.
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Lee, T. S., Liu, C. H., & Chen, T. W. (2006). Thermodynamic analysis of optimal condensing
temperature of cascade-condenser in CO2/NH3 cascade refrigeration system. Refrigeration, 29, 1100–1108.
Lorentzen, G., & Petterson, J. (1993). A new efficient and environmentally benign system for car
air-conditioning. International Journal of Refrigeration, 16(1), 4–12. Murthy, S. S., & Murthy, M. V. K. (1985). Experiments on a cascaded R11–R12 vapour
compression system for cogeneration of heat and cold. Journal of Heat Recovery Systems, 5 (6), 519–526.
Ratts, E. B., & Brown, J. S. (2000). A generalized analysis for cascading single fluid vapor
compression refrigeration cycles using an entropy generation minimization method. Refriger- ation, 23, 353–365.
Robinson, D. M., & Groll, E. A. (1998). Efficiencies of transcritical CO2 cycles with and without
an expansion turbine. International Journal of Refrigeration, 21(7), 577–589. UNEP. (1987). Montreal protocol on substances that deplete the ozone layer. United Nations
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Chapter 38
Comparison of Thermal Repowering Alternatives for Thermal Power Plants
M. Zeki Yilmazoglu
Introduction
Electricity consumption increases rapidly due to the increasing population and
industrialization. Greenhouse gas emissions, mainly CO2, increase in order to offset
the increasing energy demand. Approximately half of the electricity demand is
obtained from fossil fuels combustion. Efficient use of energy, renewable energy,
clean energy generation systems, CO2 capture and storage, energy harvesting
systems etc. current research topics in power generation. Many regulations have
been implemented by the governments to decrease the greenhouse gases. On the
one hand, the energy demand increases rapidly, and on the other hand GHGs have
to be decreased. In Turkey, low rank lignite is generally used for power generation
in thermal power plants which most of them were installed in 80s. These old
thermal power plants are still in operation with lower net electrical efficiencies.
The net electrical efficiency of these power plants decrease with time due to the
aging and operational problems. Therefore, repowering of these power plants can
increase their energy efficiency and reduce their contribution to the global warming
potential.
Repowering can be defined as increasing the installed capacity, the net electrical
efficiency, and decreasing the emissions per installed capacity of an existing
thermal power plant (Yilmazoglu et al. 2012, 2013a, b). Generally, a gas turbine
is added to the cycle in thermal repowering applications. Feedwater heating, hot
windbox and parallel repowering are three of the most commonly implemented
repowering options (Escosa and Romeo 2009; Yilmazoglu and Durmaz 2013a, b).
M.Z. Yilmazoglu (*) Department of Mechanical Engineering, Faculty of Engineering, Gazi University,
Maltepe, Ankara, Turkey
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_38
513
In feedwater heating, steam turbine extraction points are repealed and heating of
feedwater is supplied from a heat recovery steam generator or a solar field (Popov
2011; Yilmazoglu et al. 2012). In thermal power plants, repowering reduces CO2 emissions per installed capacity (Schenk and Ehren 2003; Walters 2008). The most
important parameter in repowering applications is the expected life time of the
equipment. Therefore, a detailed life expectancy analysis has to be carried out
before repowering. In addition, gas turbine and heat recovery steam generator
selection are crucial for the operation of thermal power plant after repowering
(D’Yakov et al. 1998; Mathieu 1998).
Gas turbine leverage and repowering efficiency are the decisive parameters in
the analysis of a repowering application. Repowering efficiency can be defined as
the rate of increment in electricity generation to increment in heat added to the
cycle which is given in Eq. (38.1). The subscripts, ar and br symbolize after
repowering and before repowering, respectively. After repowering the electricity
generation is increased due to the additional power from gas turbine and steam
turbine. Moreover, the natural gas consumption and consequently, the heat added to
the cycle are increased. Gas turbine leverage can be defined as the rate of increment
in electricity generation to the gas turbine installed capacity which is given in
Eq. (38.2). In a typical combine cycle power plant with an installed capacity of
400 MWe, approximately 67% of electricity generation capacity is supplied from
the gas turbine. However, in the case of repowering it is approximately 10–25% as
a result of smaller gas turbine selection.
ηrep ¼ ΔPel ΔQg
¼ Par � Pbr Qin,ar � Qin,br
ð38:1Þ
λGT ¼ ΔPel Pel,GT
¼ Par � Pbr Pel,GT
ð38:2Þ
Lignite is the main fuel source in electricity generation in Turkey and low rank
lignite is used generally for power generation. Most of the thermal power plants are
firstly operated in mid 80s. Therefore, the net electric efficiency and availabilities of
these power plants are decreased with time due to the ageing of components.
In this study, Soma A thermal power plant was examined and the application of
different repowering alternatives, feedwater heating, hot windbox, and parallel
repowering, were compared by a commercial software, Thermoflex. Soma A
thermal power plant was decommissioned in 2010. Currently, the installed capacity
of the power plant is 44 MWel with two units. One unit of the power plant was
simulated for different repowering alternatives. This study sums up and summarizes
the results of previous studies and compares different alternatives in terms of the
installed power increment, CO2 reduction potential per installed capacity and unit
electricity generation price.
514 M.Z. Yilmazoglu
Repowering Alternatives
Feedwater Heating
In Fig. 38.1, the connection schema for feedwater heating repowering application is
shown.A gas turbine and two feedwater heaters are added to the thermal power plant.
Dashed lines indicate components added to the thermal power plant after repowering.
Bled steam is only taken for deaerator and others are repealed. The waste heat of gas
turbine is utilized by two economizers. Natural gas or syngas can be used as the fuel
source in gas turbine. Also, a gasifier island can be added to the cycle to obtain
syngas. In this study natural gas is accepted as the fuel source in gas turbine.
Hot Windbox
Hot windbox repowering can be implemented in three different methods. In the first
method, the exhaust gas of gas turbine is fed to the burners. In this method, feedwater
heating is supplied by two economizers installed after the boiler. In direct hot windbox
application, burners and other related components have to bemodified due to the high
temperatures of exhaust gases of gas turbine. As a result, first investment cost of
repowering increases. In addition, due to the low O2 content which is approximately
13–14%, some combustion problems i.e. flame stabilization, can occur in the steam
boiler. Therefore, fresh air dilution is a necessity to lower the investment cost and
Fig. 38.1 Feedwater repowering of a thermal power plant
38 Comparison of Thermal Repowering Alternatives for Thermal Power Plants 515
prevent combustion problems. The fresh air dilution application is shown in Fig. 38.2.
In thismethod fresh air ismixedwith flue gases ofGT to increase theO2 content and to
decrease the burner inlet temperature. In the third method, a pre-cooling system is
installed after the gas turbine. This precooling system acts as an evaporator and
produces extra steam for the steam turbine. It is directly connected to the drum. The
temperature of the flue gas of GT is reduced to an acceptable range. However, the first
investment cost of pre-cooling system is higher than fresh air dilution application.
Therefore, fresh air dilution is used in the simulations.
Parallel Repowering
In parallel repowering, a gas turbine and a HRSG are installed and additional steam
is fed to the steam turbine. Parallel repowering application with additional gas
turbine stack brings the power plant operation flexibility (Yilmazoglu and Durmaz
2011). In all applications installed capacity of the power plant is increased with a
properly selected gas turbine and heat recovery steam generator (HRSG) combina-
tion (Carapellucci 2009; Elmasri 2008).
Design Parameters of Soma A Thermal Power Plant
Soma A thermal power plant was designed according to the data, given in
Table 38.1, in 1957. The power plant was operated at constant maximum load, at
Fig. 38.2 Hot windbox repowering with fresh air dilution
516 M.Z. Yilmazoglu
operation #4. The ultimate analysis of coal, used in the power plant, is given in
Table 38.2. The lower heating value and ash melting temperature of the coal are
3550 kcal/kg and 1400 �C, respectively. Three closed type feed water heaters and a deaerator is designed to preheat the condensed working fluid. Condenser pressure is
0.063 bar and a cross flow type cooling tower with fans is used to transfer the
condenser heat to the environment. An air preheater unit is also designed to send the
air into the combustion chamber at 220 �C. Flue gases are emitted to the atmosphere by a 55 m stack at 160 �C. The thermal efficiency of the boiler is 87.2% and stack losses are 8.4% of the total energy input. Bled steam, for preheating of the water in
feed water heaters, are taken from 4th, 8th, 11th and 13th stages, of a 15 stage
turbine. First bled steam is taken from 10–13 bar at 350 �C. The others are taken 4.5–4.8 bar at 250 �C for 8th stage, 1.7–1.8 bar at 175 �C for 11th stage and 0.3–0.35 bar at 110 �C for 13th stage (Fig. 38.3).
Table 38.1 Design data of Soma A thermal power plant
Operation conditionsa 1 2 3 4 5
Turbine power [MW] 7 12 17 22 NA
Water/steam pressures [bar]
Inlet of economizer 62 62.6 65.7 70 72
Outlet of dome 59.6 61.5 64 68 69.8
Outlet of superheater 59.4 60.7 62.4 65 66.2
Temperatures [�C] Steam temperature at outlet of superheater 489.7 487.7 487 486.5 486.4
Water temperature at inlet of economizer 139 165 180 192 196
Water temperature at outlet of economizer 197 216 230 242 245
Gas temperature at inlet of superheater 826 872 922 980 1000
Gas temperature at outlet of economizer 239 261 278 296 302
Air temperature at outlet of air pre-heater 206.5 213 222.5 226.5 228
Stack temperature 129 142 152 160 162.5
Mass flow rates [t/h]
Fuel 6.96 11.4 15.6 20.3 22
Combustion gas 60.6 93.3 121.4 150.8 161.5
Steam mass flow rate 30 51 72 96 105 aOperation conditions—1: Technical minimum, 2: Constant minimum load, 3: Normal load, 4:
Constant maximum load, 5: Transient maximum load
Table 38.2 Ultimate analysis of Soma coal
Ultimate analysis [wt.%] As received Dry
C 39.48 52.8
H 2.95 3.94
O+N 13.42 18
S 0.53 0.71
W 25.22 0
A 18.4 24.55
38 Comparison of Thermal Repowering Alternatives for Thermal Power Plants 517
Results
Aero-derivative type gas turbines, with a capacity of 12–35% of the existing power
plant, give the optimum results for feedwater heating repowering applications. The
limit is determined by the condenser mass flow rate increment percentage which is
taken as 20% greater than the initial total mass flow rate for all repowering
applications. In Figs. 38.4, 38.5, and 38.6 the effects of the feedwater repowering
application was presented. The ratio of gas turbine power to initial power indicates
the installed power or capacity of the selected gas turbine for repowering. For
instance, 20% ratio means that the GT installed power is 4.4 MWel. It is clear from
Fig. 38.4 the net power of the TPP was increased substantially after repowering.
Also, the condenser mass flow rate was increased due to the repealing of extraction
points of the steam turbine which also increased the mass flow rate of steam
entering the steam turbine and consequently, a 10% increment in net power
generation was obtained by steam turbine. For 30% GT ratio the total plant
capacity was found to be 30.2 MWel and the net electrical efficiency was increased
from 31.7% to 33.87%. Around 5% GT ratio ST net power and net electrical
efficiency was decreased as shown in Fig. 38.4. The reason of this decrement can be
explained by the lower capacity GT selection. Repowering efficiency and GT
leverage for different ratios were given in Fig. 38.5. It is shown that the minimum
gas turbine capacity has to be greater than 10% of the initial power. Figure 38.6
shows the CO2 emissions of the TPP after repowering. In the modeling of the
current state the CO2 emission was found to be 7.019 kg/s. After repowering with a
30% GT ratio, the CO2 emission was found to be 8.146 kg/s. It is an expected result
that the installed capacity of the TPP was increased. However, the CO2 emission per
installed capacity shows an interesting result. In the current state the CO2 emission
per installed capacity was found to be 0.321 and after repowering it was found to be
0.27 which indicates that repowering of old TPP can be used to decrease the CO2 emissions in short term.
Fig. 38.3 Parallel repowering application
518 M.Z. Yilmazoglu
For hot windbox repowering application a GT was installed. Flue gas was
diluted by fresh air to support combustion or flame stability. The results were
given in Figs. 38.7, 38.8, and 38.9. In Fig. 38.7 the effects of hot windbox
repowering application on TPP performance was shown. The net electrical effi-
ciency was slightly changed. However, when Figs. 38.4 and 38.7 were compared
The ratio of GT power to initial power [%]
0 10 20 30 40
V ar
ia tio
n pe
rc en
ta ge
[% ]
-10
0
10
20
30
40
50 Net power Heat rate variation ST net power variation Condenser mass flow rate Net electrical efficiency
Fig. 38.4 Effects of the feedwater heating repowering application in TPP
The ratio of GT power to initial power [%]
0 5 10 15 20 25 30 35
R ep
ow er
in g
ef fic
ie nc
y [%
]
0,0
0,2
0,4
0,6
0,8
1,0
1,2
1,4
G T
le ve
ra ge
[- ]
0,0
0,2
0,4
0,6
0,8
1,0
1,2
1,4
Repowering efficiency [%] GT leverage [-]
Fig. 38.5 Variation of repowering efficiency and gas turbine leverage
38 Comparison of Thermal Repowering Alternatives for Thermal Power Plants 519
The ratio of GT power to initial power [%]
0 5 10 15 20 25 30 35
C O
2 em
is si
on v
ar ia
tio n
pe r
in st
al le
d po
w er
[% ]
-20
-15
-10
-5
0
5
10
CO2 mass flow rate [kg/s]
CO2 emission per installed power [kg/MW.s]
Decrement percentage of CO2 emission [%]
Fig. 38.6 Variation of CO2 emissions and fuel consumption
8 10 12 14 16 18 20 22 24
V ar
ia tio
n [%
]
-4
-2
0
2
4
6
8
10
12
14
16
18
20
22
24
26
28
Gas turbine power ratio [%] vs Rate of increase in net power [%] Gas turbine power ratio [%] vs Variation of net heat rate [%] Gas turbine power ratio [%] vs Rate of increase in steam turbine power [%] Gas turbine power ratio [%] vs Rate of increase in condenser mass flow rate [%] Gas turbine power ratio [%] vs Variation of net electric efficiency [%]
Gas turbine power ratio[%]
Fig. 38.7 Effects of hot windbox repowering application in TPP
520 M.Z. Yilmazoglu
the increment in net electrical efficiency is distinctive in feed water heating
application. The auxiliary power consumption of the hot windbox application is
greater than feed water heating application due to the increased forced draught fan
power. GT leverage and repowering efficiency was found to be 1.3 and 0.32,
respectively for 22% GT ratio. In the case of CO2 emissions the coal consumption
was increased due to the increased mass flow rate of air. Approximately half of the
total mass flow rate of inlet air was selected as fresh air to decrease the temperature
of the flue gas and increase the O2 content of the inlet air. It is also obvious from
Fig. 38.9 that CO2 emission per installed power was decreased.
Parallel repowering of TPP was also investigated and the effects of repowering of
TPP performance were presented in Fig. 38.10. In parallel repowering it is clear that
the selection range of GT power was significantly increased. Because of the structure
of the system steam was generated separately via a heat recovery steam generator
(HRSG), located after the GT. Therefore, steam mass flow rate increment is the
limiting factor in this kind of repowering application. Steam can be produced with
different pressure levels in a multi-pressure HRSG. However, in this case initial and
operational costs will be significantly increased. Instead of multi-pressure HRSG,
single pressure HRSGwas located and same pressure with live steamwas obtained in
order to mix these streams before steam turbine inlet. According to Fig. 38.10 the net
power of the TPP was doubled and the net electrical efficiency was increased from
31.7% to 38.26%. In this case repowering efficiency and GT leverage were found to
be 47.3% and 1.174, respectively. CO2 mass flow rate was increased. However, CO2 emission per installed power was significantly decreased (Fig. 38.11).
Gas turbine power ratio [%]
8 10 12 14 16 18 20 22 24
V ar
ia tio
n [%
]
0,2
0,4
0,6
0,8
1,0
1,2
1,4
Gas turbine power ratio [%] vs Repowering Efficiency*100 [%] Gas turbine power ratio [%] vs Gas turbine leverage [-]
Fig. 38.8 Variation of repowering efficiency and gas turbine leverage
38 Comparison of Thermal Repowering Alternatives for Thermal Power Plants 521
The ratio of GT power to initial power [%]
0 20 40 60 80 100 120
V ar
ia tio
n pe
rc en
ta ge
[% ]
-40
-20
0
20
40
60
80
100
120 Net power Heat rate ST net power variation Condenser mass flow rate Net electrical efficiency
Fig. 38.10 The effects of parallel repowering application in TPP
Gas turbine power ratio [%] 0 2 4 6 8 10 12 14 16 18 20 22 24
V ar
ia ti on
[ %
]
-10
-8
-6
-4
-2
0
2
4
6
Gas turbine power ratio [%] vs Rate of decrease in CO2 emissions per MWel [%] Gas turbine power ratio [%] vs Rate of increase in coal consumption [%] Gas turbine power ratio [%] vs Variation of coal consumption [kg/s]
Fig. 38.9 The variation of CO2 emissions and fuel consumption
522 M.Z. Yilmazoglu
According to the results given above, repowering of the old TPPs can signifi-
cantly increase the net electrical efficiency, net energy generation and decrease the
CO2 emissions per installed power. Repowering offers a short term solution for CO2 decrement while new power plants have been installed.
An economical comparison was carried out to determine the unit electricity cost.
Table 38.3 summarizes the situation after repowering for different cases. The cost
of repowering, specific cost of repowering, unit electricity generation cost and with/
without first investment costs were given. According to the limiting factors best GT
ratios were compared. For feed water heating, hot windbox and parallel repowering
applications GT ratios were selected as 30%, 22% and 100%, respectively.
The ratio of GT power to initial power [-]
0 20 40 60 80 100 120
C O
2 em
is si
on v
ar ia
tio n
pe r
in st
al le
d po
w er
[% ]
-40
-30
-20
-10
0
10
20
CO2 mass flow rate [kg/s] CO2 emission per installed power [kg/MWs] Decrement percentage of CO2 emission [%]
Fig. 38.11 The variation of CO2 emissions and fuel consumption
Table 38.3 Economic comparison of repowering alternatives
Technoeconomic parameters Current case FWH HWB PR
Net power [MW] 21.877 30.207 27.67 45.5
Net electrical efficiency [%] 31.70 33.87 31.68 38.26
Heat rate [kJ/kWh] 11,355 10,609 11,363 9410
CO2 mass flow rate [kg/s] 7.02 8.15 8.17 9.18
CO2 mass flow rate per inst. power [kg/s/MW] 0.321 0.270 0.295 0.202
Coal consumption [kg/s] 4.843 4.821 5.033 3.813
First investment cost (FIC) [1000�USD] 10,940 5,700 4,210 15,940 Specific repowering cost [USD/kWel] 500 685 726.4 674.6
Unit electricity generation cost [cent/kWh] 4.24 5.38 5.36 6.57
Unit electricity gen. cost without FIC [cent/kWh] 0.00 4.9 4.83 6.24
38 Comparison of Thermal Repowering Alternatives for Thermal Power Plants 523
It is clear from the table that CO2 mass flow rate increases. However, CO2 mass
flow rate per installed power decreases. In parallel repowering application coal
consumption was found to be the lowest. However, it must be noted that natural gas
consumption was found to be four times more than FWH and HWB repowering. In
the economic analyses first investment cost of the TPP was calculated according to
the design data with specific investment cost value. After, additional costs of each
repowering application were calculated. It is obvious that the calculated highest
repowering investment cost is parallel repowering application due to GT and HRSG
costs. Unit electricity generation costs were also calculated with and without FIC.
According to the results, HWB repowering with fresh air dilution slightly increases
the unit electricity cost when compared to current case costs.
Conclusions
In this study comparison of repowering applications were performed. Net power, net
electrical efficiency, CO2 emissions and unit electricity generation costs were com-
pared. Feedwater heating, hot windbox and parallel repowering applications were
simulated in order to compare the results. SomaA thermal power plant with a capacity
of 2� 22MWelwas selected as the case study. According to the results, net power and net electrical efficiency were increased. Total CO2 mass flow rate was increased.
However, CO2 mass flow rate per installed capacity was sharply decreased. There-
fore, repowering of old thermal power plants can be a short term solution in decreas-
ing the CO2 emissions while the electricity demand increasing continuously.
Nomenclature
P Electric power, kW
Q Thermal power, kW
FWH Feedwater heating
HWB Hot windbox
PR Parallel repowering
Greek Letters
η Efficiency, % λ Leverage, –
Subscripts
El Electricity
ar After repowering
524 M.Z. Yilmazoglu
br Before repowering
rep Repowering
GT Gas turbine
g Inlet
References
Carapellucci, R. (2009). A unified approach to assess performance of different techniques for
recovering exhaust heat from gas turbines. Energy Conversion and Management, 50, 1218–1226.
D’Yakov, A. F., Nechaev, V., Olkhovsky, R., & Gurgen, G. (1998). Repowering existing thermal
power stations. Proceedings of the American Power Conference, 2, 1033–1037. Elmasri, M. A. (2008). Design of gas turbine combined cycle and cogeneration systems. Milan,
Italy: Thermoflow Inc. Seminar.
Escosa, M. J., & Romeo, M. L. (2009). Optimizing CO2 avoided cost by means of repowering.
Applied Energy, 86, 2351–2358. Mathieu. P. F. (1998). Repowering options for existing power plants. In Proceedings of the NATO
advances study institute on thermodynamics and optimization of complex energy systems (pp. 251–260).
Popov, D. (2011). An option for solar repowering of fossil fuel fired thermal power plants. Solar Energy, 85, 344–349.
Schenk, H., & Ehren, G. (2003). Gas turbine based power plants repowering reduces emissions and
increase efficiency of existing plants while re-utilizing available assets. In Proceedings of the international gas turbine congress.
Walters, A. B. (2008). Power plant topping cycle repowering. Energy Engineering, 92, 49–71. Yilmazoglu, M. Z., & Durmaz, A. (2011). Parallel repowering of Soma A thermal power plant, 18.
In National conference on thermal science and technology, Zonguldak, Turkey. Yilmazoglu, M. Z., & Durmaz, A. (2013a). Hot windbox repowering of coal-fired thermal power
plants. Turkish Journal of Engineering and Environmental Sciences, 37, 33–41. Yilmazoglu, M. Z., & Durmaz, A. (2013b). Technoeconomic analysis of feed water heating
repowering of Soma A thermal power plant. Journal of Science and Technology of Dumlupınar University, 32, 79–90.
Yilmazoglu, M. Z., Durmaz, A., & Baker, D. (2012). Solar repowering of Soma A thermal power
plant. Energy Conversion and Management, 64, 232–237.
38 Comparison of Thermal Repowering Alternatives for Thermal Power Plants 525
Chapter 39
Experimental Study of Heat Transfer for a Non-Newtonian Fluid in a Heated Cylindrical Pipe
Mounir Mellal, Hacina Abchiche, and Sabrina Ait Ouazzou
Introduction
During these last decades, the authors were interested in analyzing the problem of
transfer of heat during the flows of the non-Newtonian fluids, in cylindrical pipes
[Benslimane, 2012]. Thanks to its implication in numerous natural phenomena and
industrial process, the researchers are more and more interested in this problem and
more specifically in the transfers of heat which develop in the cylindrical pipes, in
forced convection. Numerous researchers dealt with the understanding of the
phenomenon of transfer of heat in laminar flow which the object of our work.
Materials and Methods
The setup of eviction which was of use to our experiment was specially designed
within our laboratory, for the rheologic, thermo-rheologic study of the laminar
flows of the various fluids. It consists of:
A storage tank made of stainless steel with a capacity of 15 L in double wall
(isotherm) equipped with a sensor of pressure (manometer) with a membrane, an
electric resistance, two gates of subjection, followed by a 3 m long cylindrical
conduct, a heating conduct in the form of a tube in stainless steel altered by five
prickings of temperature and two prickings of pressure, an electric resistance is
wrapped around the tube to maintain a constant flow at the end of this installation.
M. Mellal (*) • H. Abchiche • S. Ait Ouazzou Laboratoire des Phénomènes de Transfert, Faculté de Génie Mécanique et Génie des Procédés,
Université des Sciences et de la Technologie Houari Boumediene (USTHB), BP 32 El Alia,
Bab Ezzouar, 16111 Algiers, Algeria
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_39
527
A recycling tank for the product is placed out of the section of measure provided
with a centrifugal pump allowing to feed again the main tank through a feeding pipe
and a conduct of expulsion allowing the mixture of the product before its use, also, a
thermo regulator is there in order to regulate and to fix the temperature of the
external wall of the heating conduct (Fig. 39.1).
Conception of the Heating Conduct
We designed a heating conduct with resistance to warm the model fluid we had used
for the thermo-rheologic study also to favor the flow by reducing the effects of
sliding into the conduct; it is also convenient with the study of the transfer of heat to
make a heating conduct which answers our expectations, we used a number of
equipments, which the most important are:
A 2 m tube in stainless steel with prickings of pressure and temperature, around
the tube we, a heat insulator was placed which is the Teflon in the form of an
adhesive tape, afterward it was wrapped into an electric resistance of first class type
Nickel/Chrome, then aluminum in the form of an adhesive tape, we provided the
tube with electric cables for the supply, plastic and metallic rings for the tightening,
Fig. 39.1 The installation of eviction
528 M. Mellal et al.
then we wrapped up the whole system in an insulating material which is the
glass wool and for the new conducts we put the foam rubber, then sheets of
aluminum, also, a sensor for thermocouple and finally of two transformers and a
thermoregulator.
Our study was made on three heating conducts of different diameters, one of the
conceptions was later changed; the main insulating material, the glass wool was
replaced by the foam rubber, a comparative study was also made. The conception of
two new heating conducts was made according to one method as follows:
We began with the making of the prickings, then we set up sensors of thermo-
couple, followed by a primary insulation then the implantation of the resistance,
then we placed the secondary insulation, then we prepared the grips of supply we
finalized the whole by a tertiary insulation.
Figure 39.2 represents a generalized plan by the heating conduct which was of
use to our thermo-rheologic study, it to study the thermal transfer which occurs
there.
Used Product
The product used for the thermo-rheologic study which was of use to the study of
the thermal transfer is the Carboxymethyl Cellulose. The study was made on
concentrations of 0.5%, 0.8%, 1% and 1.5%.
Results and Discussion
Rheological Characterization of the Flowing Suspension
Having drawn the graphs of the logarithm of the difference of pressure according to
the flow, we deducted that the fluid presents a rheo-fluidifying behavior of Oswald’s model. The results which follow were obtained from the relations of Rabinowitch
Résistance
P T
2m
0,5m 0,49m 0,49m 0,23m 0,15m 0,14m
T T T T P
Mousse de caoutchouc
Téflon
Sortle Entrée
Fig. 39.2 Generalized plan by the heating conduct
39 Experimental Study of Heat Transfer for a Non-Newtonian Fluid in a Heated. . . 529
Mooney, from there we succeeded in drawing rheogrammes giving the evolution of
the constraint of parietal cutting according to the speed of parietal cutting for
various concentrations to several temperatures and various diameters.
Figures 39.3, 39.4, 39.5, and 39.6 represents the evolution of the constraint of
parietal cutting according to the speed of parietal cutting for a diameter of 10 mm
“we chose to present the results of a single diameter of 10 mm”.
From the results shown on Figs. 39.4, 39.5, and 39.6 we notice ascending curves
passing by the origin towards an asymptotic value, these curves take a look in the
form of curve of power which answers the mathematical model which follows
τp ¼ K _γ n 0 ð39:1Þ
From this equation we can deduct the type of the rheologic model which follows
the used fluid, this model is the model of OSTWALD.
The treatment of the experimental results by the relation of Rabinowitch
Mooney shows that the suspension in the range of the rate of studied cutting can
have a behavior rheo-fluidizing of Oswald’s model.
Fig. 39.3 Evolution of the constraint of cutting
according to the speed of
parietal cutting for a 0.5%
concentration, a diameter
10 mm
Fig. 39.4 Evolution of the constraint of cutting
according to the speed of
parietal cutting for a 0.8%
concentration, a diameter
10 mm
530 M. Mellal et al.
This behavior can be modeled using the following relation:
τ ¼ k€γn ð39:2Þ
The pile of curves shows that the more we increase in the temperature of the
regulator; the more there is decrease of the speed of cutting, thus the viscosity
decreases.
Heat Transfer of in the Flow of Non Newtonien Fluids
Because of the number of Richardson, we were able to demonstrate that it is the
forced convection which takes the flow on the natural convection.
The correlation Nu ¼ 11 48 � 1
2
X1 m¼1
exp �γ2m xþð Þ Am γ4m
" #�1 allowed us to confirm the con-
stant parietal flow, we found a value of Nu¼ 4,36 with one m varying from 1 to 1000 where m represents a constant of precision, the higher m is, the better the
Fig. 39.5 Evolution of the constraint of cutting
according to the speed of
parietal cutting for a 1%
concentration, a diameter
10 mm
Fig. 39.6 Evolution of the constraint of cutting
according to the speed of
parietal cutting for a 1.5%
concentration, a diameter
10 mm
39 Experimental Study of Heat Transfer for a Non-Newtonian Fluid in a Heated. . . 531
precision will be, thus according to the literature this value of Nusselt found using
FORTRAN (software), is represented for a flow of telling heat.
The thermal study was made on typical correlations for a forced convection on
Oswald’s fluid to constant parietal flow and it to study the evolution of the number of Nusselt according to the length, to Graetz and to the indication of the flow.
Nusselt Number Effect
Having calculated the number of Nusselt and the number of Graetz, we were able to
draw graphs Figs. 39.7 to 39.8, which represents the evolution of the number of
Nusselt according to the length for a diameter of 10 mm.
The number of Nusselt represents the total thermal transfer with regard to the
thermal transfer by conduction throughout the conduct, thus according to the graphs
of Figs. 39.8, 39.9, and 39.10, we notice the decrease of the number of Nusselt with
the increase of the length, also we distinguish two zones. The first zone into which
the number of Nusselt drops until a value of L¼ 0,7 m, this is because of the consequent exchange which is made in the entry of the zone with the aim of the
Fig. 39.7 Evolution of the number of Nusselt
according to the distance for
a 0.5% concentration and
one diameter of 10 mm
Fig. 39.8 Evolution of the number of Nusselt
according to the distance for
a 0.8% concentration and
one diameter of 10 mm
532 M. Mellal et al.
importance of the gradient of temperature, between the fluid and the wall. The
second zone where the number of Nusselt stabilizes until an asymptotic value, we
also notice that according to these graphs the number of Nusselt is important with
the increase of the temperature. Thus the warmer it is, the bigger the exchange is.
Profile of the Number of Nusselt According to the Number of Graetz
According to Figs. 39.11, 39.12, 39.13, and 39.14 the evolution of the number of
Nusselt according to the number of Graetz, we notice an increase of the number of
Nusselt with the increase of the number of Graetz, also a superimposing of curves
with various temperatures, concentrations and various diameters. We deduct that
the length has no effect, seen that Graetz depends of the length. It confirms the
works done before which also concluded that the length has no influence on the
thermal transfer.
Fig. 39.9 Evolution of the number of Nusselt
according to the distance for
a 1% concentration and one
diameter of 10 mm
Fig. 39.10 Evolution of the number of Nusselt
according to the distance for
a 1.5% concentration and
one diameter of 10 mm
39 Experimental Study of Heat Transfer for a Non-Newtonian Fluid in a Heated. . . 533
Determination of the Number of Asymptotic Nusselt
We studied the number of asymptotic Nusselt according to the index of the flow for
all the concentrations, the temperatures and the diameter, the following results
(profits) concern all the concentrations for a diameter of 10 mm.
Fig. 39.11 Evolution of the number of Nusselt
according to the number of
Graetz for a 0.5%
concentration and one
diameter of 10 mm in
various temperatures
Fig. 39.12 Evolution of the number of Nusselt
according to the number of
Graetz for a 0.8%
concentration and one
diameter of 10 mm in
various temperatures
Fig. 39.13 Evolution of the number of Nusselt
according to the number of
Graetz for a 1%
concentration and one
diameter of 10 mm in
various temperatures
534 M. Mellal et al.
Figures 39.15, 39.16, 39.17, and 39.18 express the variation of the number of
asymptotic Nusselt for the case “isoflux” according to the index of flow n, for the
concentrations of 0.5, 0.8, 1 and 1.5%, diameter 10 mm and for various tempera-
tures of the thermoregulator, we notice that n is between 0< n< 1, which corre- sponds to the pseudoplastic fluids, we also notice that Nu1 decreases with the increase of the index of flow (n) until stabilization. We can confirm that the rate of
transfer of heat is more important within the pseudoplastic fluids n< 1.
Fig. 39.14 Evolution of the number of Nusselt
according to the number of
Graetz for a 1.5%
concentration and one
diameter of 10 mm in
various temperatures
Fig. 39.15 Evolution of the number of Nusselt
according to the index of
flow for a 0.5%
concentration and one
diameter of 10 mm
Fig. 39.16 Evolution of the number of Nusselt
according to the index of
flow for a 0.8%
concentration and one
diameter of 10 mm
39 Experimental Study of Heat Transfer for a Non-Newtonian Fluid in a Heated. . . 535
Study of the Conduction
For this study, we proceeded by the method of harbinger’s Law, for reasons of
non-availability of all the parameters to study the conduction of the source towards
the ambient air, we made an reverse study, we studied at first the flow absorbed by
the fluid, by using harbinger’s law of the source towards the fluid, afterward
knowing the loose flow we proceeded with a subtraction to find the lost flow
through insulations. The results are grouped in Table 39.1.
Fig. 39.17 Evolution of the number of Nusselt
according to the index of
flow for a 1% concentration
and one diameter of 10 mm
Fig. 39.18 Evolution of the number of Nusselt
according to the index of
flow for a 1.5%
concentration and one
diameter of 10 mm
Table 39.1 Flux lost through insulation
T¼ 70 �C C % D mm
8 10 « rubber foam
»
10 « glass wool
»
12
0.5 3.8535 11.0690883 11.6255
0.8 3.3732 8.8967 10.8866
1 3.3843 11.9229125 9.2730
1.5 3.1618 10.8272789 3.239845 10.4824
536 M. Mellal et al.
Figure 39.19 represents a multi-cylindrical conduct sleep, where, Rint internal
radius of the conduct and Rext the external radius, the distance between them
representing the thickness of the teflon, eR the thickness of the resistance and finally
eMC the thickness of the foam rubber. The following table represents the lost flow
through insulations in different diameters and concentrations as well as the com-
parison of both insulations made on a diameter of 10 mm and for a concentration of
1.5% in 70 �C. Another study was made to confirm that the insulating material of glass wool is
more successful than the foam rubber. We compared the temperatures of the fluid
and the wall of two various insulations according to the distance, for a temperature
of the thermoregulator of 50 and 60 �C [Gacem, 2010]. Figures 39.20 and 39.21 represent the evolution of the temperature of the fluid
and the wall for both cylindrical conducts, we notice an increase of the temperature
with the increase of the length, on the other hand we notice that for the temperature
of the fluid and the wall for the glass wool, insulation is higher than foam rubber,
thus the fluid stores more heat in glass wool insulation than foam rubber this is the
same for the temperature of the wall, what leads us to say that the glass wool is more
hermetic.
Fig. 39.19 Plan representing a cylindrical
conduct
Fig. 39.20 Evolution of the fluid temperature and the
wall for the glass wool and
foam rubber according to
the distance x, to a
concentration of 1.5%, a
diameter of 10 mm to
TTR¼ 50 �C
39 Experimental Study of Heat Transfer for a Non-Newtonian Fluid in a Heated. . . 537
Figures 39.22 and 39.23 represent the evolution of the average temperature of
wall according to the length for two various insulations “Foam rubber” and “Glass
wool”. We notice an increase of the temperature with the increase of the length by
both insulations, we also notice that the curve which represents the glass wool
insulating material is higher than the one which represents the foam rubber insu-
lating material to the temperature of 50 �C and 60 �C of the thermoregulator, that leads us to confirm that the glass wool insulation is more hermetic.
Figures 39.24 and 39.25 present the evolution of the average temperature of the
wall according to the flow, for both insulations “glass wool” and “foam rubber”, for
a 1.5% concentration, one diameter of 10 mm and the temperature of the thermo-
regulator of 50 and 60 �C, these curves present a decrease of the temperature of the
Fig. 39.21 Evolution of the fluid temperature and the
wall for the glass wool and
foam rubber according to
the distance x, to a
concentration of 1.5%, a
diameter of 10 mm to
TTR¼ 60 �C
Fig. 39.22 Evolution of the wall temperature averages
according to the distance x,
for both insulations “glass
wool” and “foam rubber”,
for a 1,5% concentration,
one diameter of 10 mm and
TTR¼ 50 �C
538 M. Mellal et al.
wall average with the increase of the flow, we also notice that the temperature of
wall average for the glass wool insulation is bigger than that of the foam rubber
insulation, it can be explained by the fact that the glass wool isolates better that the
foam rubber, thus heat losses are lesser.
Fig. 39.23 Evolution of the wall temperature averages
according to the distance x,
for both insulations “glass
wool” and “rubber foam”,
for a 1,5% concentration,
one diameter of 10 mm and
TTR¼ 60 �C
Fig. 39.24 Evolution of the temperature of wall
averages according to the
outflow, for both insulations
“glass wool” and “foam
rubber”, for a 1,5%
concentration, one diameter
of 10 mm and TTR¼ 50 �C
Fig. 39.25 Evolution of the temperature of wall
averages according to the
outflow, for both insulations
“glass wool” and “foam
rubber”, for a 1.5%
concentration, one diameter
of 10 mm and TTR¼ 60 �C
39 Experimental Study of Heat Transfer for a Non-Newtonian Fluid in a Heated. . . 539
Conclusion
The thermo-rheological study allowed us to show that the non-Newtonian fluid
used, can be defined by establishing Oswald Devaele pseudoplastic type.
The testing made in the heated cylindrical pipe (HCP) has allowed us to promote
transfer mode through the relation of Richardson, which happens to be less than
1, so it is the forced convection that outweighs the natural convection.
Therefore, this study was conducted on a forced convection using Oswald fluid
for a laminar flow regime in a cylindrical pipe with constant heat and parietal flux at
different concentrations 0.5%, 0.8%, 1% and 1.5% and different diameters 8, 10
and 12 mm. From these results we were able to assess the Nusselt number with
different correlations, from one correlation we confirmed that we are in constant
flux compared with the literature, we obtained a value. We have also plot graphs of
the Nusselt number depending upon the length, and the Graetz number of flow.
To study the evolution of the Nusselt number in reference to the length, we found
that the Nusselt number drops with increasing length, and then stabilizes at an
asymptotic value. This result in the exchange therefore occurs at the entrance to the
heating pipe and caused by the elevation of the temperature gradient in the etching
area between fluid and wall.
The study of the evolution of the Nusselt number according to Graetz, allowed
us to observe an increase in the Nusselt number with the increase in the number of
Graetz, as we noticed a stack of curves at different temperatures the temperature
controller we found that the length of the pipe has no effect on the thermo-
rheological behavior.
Two of our pipes were insulated with two different insulation at the main
insulation, one insulated glass wool, the other rubber foam, for this we have
made a comparative study between the two insulators, by studying the fluid
temperature, the wall and the flow lost through these insulators, the results allowed
us to infer that the glass wool insulation is more airtight than the foam rubber.
Acknowledgement Thermal transfer, thermo rheology, carboxymethylcellulose, cylindrical pipe.
References
Benslimane, A. (2012). « Rhéologie et Ecoulement de Fluides Chargés: Application aux Réseaux
d’Assainissement Urbains. Etude Expérimentale et Modélisation ». Mémoire de Doctorat, décembre 2012.
Gacem, M. (2010/2011). « comparaison entre l’isolation thermique Extérieure et Intérieure d’une pièce d’un Habitat situé dans le Site de Ghardaı̈a », mémoire de magister, 2010–2011 (convection forcée).
Lachemet, A. (1997). « Rheologie et Transfert de Chaleur en Milieu non-Newtonien », mémoire
Magister, avril 1997.
540 M. Mellal et al.
Sacadura, J. F. (1995). « Initiation aux Transferts Thermiques ». Centre d’Actualisation Scientifique et Technique INSA de LYON, janvier 1995.
Taine, J., Iaconna, E., Petit, J. P. (2009). « Transfert Thermique », 4eme Edition.
39 Experimental Study of Heat Transfer for a Non-Newtonian Fluid in a Heated. . . 541
Chapter 40
The SOC Estimation of LCO Battery Based on BP Neural Network
Sy-Ruen Huang, Yen-Huai Ma, Jheng-Shyun Li, and Jun-Han Chan
Introduction
Improvements in battery technology have led to the development of batteries with
greater energy yield, efficacy, and capacity. Currently, the weight and energy
density of batteries, in addition to battery capacity and weight, have facilitated in
providing sufficient energy for machines requiring high-power output (e.g., electric
vehicles, electric boats, and power motors). Previous batteries for use in high
energy-consumption machines were generally too heavy or large for most practical
applications. However, the energy density of conventional lithium batteries can
exceed 120 W·h/kg. Consequently, this type of battery has been used as an energy
source in various types of machine.
Current battery technologies have led to the development of lithium ion batteries
that provide up to 190 W·h/kg in energy density and 1000 charge cycles (80%
depth of discharge). The lifetime of a lithium ion battery varies according to how it
is used. State of charge (SOC) is typically used to represent battery capacity and is
equivalent to the percentage of energy stored in a battery. Generally, maintaining
the SOC of a lithium ion battery at 20–80% can prolong its lifetime. Therefore,
accurately determining battery SOC is a crucial goal in battery research. Previous
studies on batteries have indicated that accurately estimating a battery’s SOC is a crucial topic in the fields of battery balancing and battery management systems
(Burkett et al. 1970; Linden and Reddy 2007).
S.-R. Huang • J.-S. Li • J.-H. Chan
Department of Electrical Engineering, Feng Chia University, No. 100, Wenhwa Road,
Seatwen, Taichung 40724, Taiwan, ROC
Y.-H. Ma, Ph.D. (*) Ph. D. Program of Electrical and Communications Engineering, Feng Chia University,
No. 100, Taichung 40724, Taiwan ROC
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_40
543
Artificial neural networks (ANNs) are a family of equation models and algo-
rithms proposed by McCulloch and Pitts in 1943. These mathematic models imitate
the neuron structures and behaviors of organisms, and perform calculations
according to a network comprising numerous artificial neurons. ANNs are a type
of parallel calculation system that utilizes equations to emulate the processes of a
biological neural system and various types of numerical estimation, including
classification, identification, and prediction. Previous studies have used ANNs in
numerical analysis in various fields such as engineering, science, finance, and
literature. An ANN is composed of an input layer, one or more hidden layers, and
an output layer. Each hidden layer consists of a parallel array of neurons, in which
an input is multiplied by the weights assigned to the layer, added to the bias values
of the layer, and then transferred to the next layer through a transfer function. The
hidden layers of an ANN continually transfer input values to the lower layers until
the value reaches the output layer, at which point the calculated result is obtained
(Hagan).
Types of Lithium Ion Batteries
The prevalent use of lithium ion batteries have led to improvements to the charac-
teristics of such cathode materials as lithium cobalt oxide (LCO), lithium manga-
nese oxide, lithium iron phosphate, and lithium nickel manganese cobalt oxide.
Table 40.1 illustrates a comparison of various cathode materials. The safety of
lithium ion batteries has been improved, and the charge cycle of such batteries can
exceed 1000 charges. Consequently, lithium ion batteries have been applied in
electric cars and hybrid electric cars. Studies on lithium ion batteries have been
conducted since 1980. The oxide structure of such batteries is classified as an
α-NaFeO2 layered structure, which is relatively stable compared with other battery types. Characteristics such as high battery density, low discharge rate, absence of
memory effect, long cycle life, antioxidation, and acid-corrosion resistance enable
various types of electrolyte to be used in lithium ion batteries. Additionally, such
batteries have a long storage life when not in use. Lithium ion batteries have
become a mature and primary cathode material product that features higher capac-
ity and more stable performance compared with other cathode material products.
However, lithium ion batteries also possess several disadvantages. Overcharging
such a battery can permanently fixate lithium ions in its crystal lattices, thereby
Table 40.1 Comparisons of cathode materials
LiCoO2 LiMn2O4 LiMnO2 LiFeO4
Density of energy 190–240 100–120 200 130–140
Voltage 3.6 3.8–3.9 3.4–4.3 3.2–3.7
Cut-off voltage 4.2 4.2 4.2 3.6
Life cycle >500 >500 Bad >1000
544 S.-R. Huang et al.
reducing the lifetime of the battery. By contrast, overdischarging such batteries can
release excess lithium ions and collapse the crystal lattices, thereby decreasing the
battery lifetime. Therefore, when charging and discharging a lithium ion battery, its
SOC must be accurately measured for the protection mechanism to prevent
overcharging and overdischarging.
Methods for Measuring SOC
Current methods for measuring SOC include the discharge method, open circuit
voltage (OCV) method, coulomb counting method (CC method), direct current
(DC) impedance method, and ANNs. The discharge method is advantageous
because of its accuracy; under a constant current, a battery is discharged and its
current and voltage are then multiplied by time duration to measure the amount of
energy expended by the battery for a specific period (W·h). However, the discharge
method is an offline approach, and thus cannot be applied to measure the SOC while
a battery is in use. The OCV method involves measuring the relationship between a
battery’s capacity and voltage. Under an open-circuit condition, battery voltage represents the battery’s remaining capacity. To measure the OCV of a battery, the target battery must stand until the reaction of the battery plate is complete, and then
the voltage becomes stable and is measured as the OVC of the battery. This method
is time-consuming and cannot be applied to measure the SOC of a battery in real
time. The discharge method and OCV method are commonly used to estimate the
full capacity of a battery (Lee et al. 2007).
The CC method is a simple and prevalent method that involves multiplying
battery current by time duration to measure the cumulative capacity (A·h), which
represents the amount of electric charge in a battery for 1 A of current to flow for 1 h
discharge. However, this method can build up cumulative errors that reduce its
accuracy. Specifically, when the CC method is applied to continually estimate the
SOC of a battery, the method can yield values exhibiting small but consistent errors;
eventually, the cumulative error reduces the accuracy of the method (Leksono
et al. 2013). The DC impedance method involves measuring how the functioning
region of a battery equivalent circuit is reduced when the electrolyte level
decreases. This method is commonly used to determine a battery’s state of health (SOH).
ANNs involves various methods. Generally, a battery’s voltage, current, and capacity can be used as training data for an ANN. Battery capacity can serve as a
target matrix for training the weight and bias value of each neuron, and an ANN can
then be constructed to estimate the SOC of the battery (Liu et al. 2011; Eddahech
et al. 2011; Sarvi and Adeli 2010).
40 The SOC Estimation of LCO Battery Based on BP Neural Network 545
Battery Charge/Discharge Test and Experimental Data Storage
NCR18650 LCO batteries were used in the present study. The output voltage of
LCO batteries is stable and relatively high compared with that of other lithium
batteries. The rated capacity and maximum voltage of an NCR18650 are 3200 mAh
and 4.2 V, respectively (Table 40.2).
This study employed the constant current–constant voltage (CC–CV) method to
charge the target battery. During the initial stage of charging, a constant current was
applied to the battery, and the voltage of the battery increased. Once the battery
voltage value reached the preset voltage value, the CC–CV charging method was
initiated, during which the current decreased until reaching the preset minimum
value, at which point the charging process was completed.
To accurately measure the capacity of the target battery, the OCV method and
CC method were applied to acquire its basic data. Specifically, we plotted the
current–voltage curve of the battery. The OCV values of the battery estimate the
corresponding capacity values. The cumulative capacity values of the battery were
determined using the CC method to measure the current flowing through the
battery. LabVIEW was used to collect the data during the process of charging.
Figure 40.1 depicts the configuration of the system architecture and the human
machine interface. During the charging process, 0.34 A of current was applied to
charge the battery from 2.8 V (the minimum voltage of the battery) to 4.2 V. The
voltage of a battery can increase or decrease during the process of charging and
discharging. Consequently, the current was set at a low value (0.34 A) to ensure that
the differences in voltage were sufficiently small to approximate an OCV–capacity
curve. Figure 40.1 illustrates the current–voltage curve of the battery.
The arithmetic mean of the charging curve and discharging curve were applied
to plot the average voltage–capacity curve, in which the voltage values can be
perceived as the OCV values of the target battery (Fig. 40.2). The capacity values
(A·h) in Fig. 40.2 were calculated using the CC method to determine the battery’s cumulative current across a time duration. During the charging process, the initial
capacity value of the battery was incremented. By contrast, the initial capacity
Table 40.2 Battery parameters of NCR18650B
Rated capacity 3200 mAh
Capacity Min: 3250 mAh
Std: 3350 mAh
Rated voltage 3.6 V
Charger condition CC-CV, 1625 mA, 4.20 V, 4.0 h
Weight 48.5 g
Temperature Charging: 0 toþ 45 �C Discharging: �20 to þ 60 �C Steady: 20 to þ 50 �C
Density of energy Capacity: 676 Wh/l
Weight: 243 Wh/kg
546 S.-R. Huang et al.
value was decreased during the discharging process. Equation (40.1) illustrates how
the capacity values of the battery were determined through the CC method.
Ah tnð Þ ¼ Ah t0 � ð itdt ð40:1Þ
Design and Training of Back Propagation Neural Network
In a back-propagation neural network (NN), an input unit is multiplied by the
weights of the layer and the error of the target value. Next, a stochastic gradient
descent method is applied to minimize the input-value error, and then the input
Fig. 40.1 Battery charging, discharging, and average voltage curves at 0.34 A
Fig. 40.2 OCV–capacity curve
40 The SOC Estimation of LCO Battery Based on BP Neural Network 547
value is multiplied by the learning rate. Subsequently, the modified input value is
transferred to the previous layer to correct the weights and bias values of that layer.
The input value propagates backward in the network until it reaches the input layer,
thereby modifying the overall network and ensuring that the errors of the network
are within a given tolerance range. The initial weights of the neurons can be
modified through the backward propagation of the input value; hence, such a
network learning process is called a back-propagation NN.
A back-propagation NN can be regarded as a multilayer network (Fig. 40.3).
Such NNs can be used to accurately train any continuous function, of which the
accuracy is determined according to the number of neurons present in the hidden
layers of the network. Generally, a network with 10 nodes of neurons can result in
undesirable training errors. Increasing the number of neurons can improve the
accuracy of the output functions. Specifically, the presence of 20–50 neurons in a
network can effectively increase the training speed and ensure that the accuracy of
output functions is within a given tolerance range. However, a high amount of
memory is required to process a network containing many neurons. Therefore, a
network comprising 20 neurons was used in the present study.
This study employed a single-layer NN. The data were inputted through the
input layer, and then transferred through the neurons of the hidden layers and
modified according to the neuron weights. Through a hyperbolic tangent transfer
function, the data were successively transferred to the subsequent layers until
reaching the output layer. Finally, the data were modified according to the output
layer weights, yielding the output function a3, which is expressed as (40.2).
a3 ¼ f3 W3f2 W2f1 W1Pþ b1� �þ b2� �þ b3� � ð40:2Þ Expanding the hidden layers of the network yields (40.3):
amþ1 ¼ fmþ1 wmþ1am þ bmþ1� � m ¼ 0, 1, . . . ,M � 1 ð40:3Þ
where M is the number of layers in the NN.
D
b1
W1
n1
b2
W2
n2 f1
P
f2
b3
W3
n3 f3
a1 a2 a3
)( 1111 bpWfa += )( 21222 baWfa += )( 12333 baWfa +=
Fig. 40.3 The architecture of a multilayer ANN
548 S.-R. Huang et al.
Through training, a back-propagation NN can generate accurate functions. The
NN training parameters are inputted into the network and the mean squared error
(MSE) of the training samples can then be obtained using (40.4). The MSEs are
used to modify the weights and bias values of the neurons.
F xð Þ ¼ E eTe � ¼ E t� að ÞT t� að Þh i ð40:4Þ Through network back-propagation, the updated weights and bias values are
obtained using (40.5) and (40.6).
sM ¼ �2 _FM nM� � t� að Þ ð40:5Þ sm ¼ _Fmþ1 nmð Þ Wmþ1� �Tsmþ1 m ¼ M � 1, . . . , 2, 1 ð40:6Þ
The least mean squares (LMS) algorithm and an estimated gradient value was
used to approximate the LMS value. As shown in (40.7) and (40.8), this method is
similar to the least gradient descent method and is used to update the weights and
bias values of the layers (Fig. 40.4).
Wm kþ 1ð Þ ¼ Wm kð Þ � αsm am�1� �T ð40:7Þ bm kþ 1ð Þ ¼ bm kð Þ� / sm ð40:8Þ
where α is the learning rate. Figure 40.5 depicts the MSE of the training process. When the number of
iterations reached 240, the LMS was reduced to 9.41� e�0.9. Network training took 1 min and 26 s to complete.
0 10−6
10−4
10−2
100
50 100
Iterations
M ea
n S
q u
ar ed
E rr
o r
(M S
E )
150 200
Fig. 40.4 The MSE curve of the iteration number
40 The SOC Estimation of LCO Battery Based on BP Neural Network 549
Estimation of Battery SOC Through ANN
The weights and bias matrices obtained through the back-propagation training
method were inputted into the NN, and a mathematical model for estimating the
SOC of the target battery was then obtained. The current and voltage of the battery
were measured and then inputted into the NN to estimate its real-time capacity.
Subsequently, the real-time capacity was divided by the peak capacity to obtain the
SOC of the target battery, as expressed in (40.9).
SOC ¼ a V; Ið Þ Q0
ð40:9Þ
a(V, I): Real-time capacity
Q0: Maximum capacity
To evaluate the applicability of the proposed estimation method, we used a 1-A
constant current to charge the NCR18650 battery. Subsequently, the NN estimation
and CC methods were applied to obtain the SOC of the target battery. Figure 40.5
shows the voltage–SOC curves, in which the red curve represents the SOC values
(estimated through the NN), whereas the black curve indicates the actual SOC
values (measured through the CC method). The estimated and actual curves
exhibited similar trends, indicating that the proposed NN method can accurately
estimate battery SOC. Table 40.3 lists the numerical values for plotting the voltage–
SOC curves. The errors of the estimated SOC values and the actual SOC values
were negligible (Table 40.3).
3 3.2
Estimate SOC
Actual SOC
100
90
80
70
60
50
40
30
20
10
0 3.4 3.6 3.8 4.24
Voltage (V)
S O
C (%
)
Fig. 40.5 Estimated capacity versus actual capacity of the target battery
550 S.-R. Huang et al.
Conclusion
The present study was conducted to develop a back-propagation NN for estimating
battery SOC. The proposed model can be employed to estimate the SOC of a battery
in a closed-loop system. Specifically, the measured voltage and current of a target
battery can be inputted into the model to calculate the real-time capacity of the
battery, and the SOC of the battery can then be estimated. Compared with the CC
method, the NN method is more complex; however, the NN method can be applied
to continuously measure battery SOC without generating cumulative errors. The
results of the present study show that the errors of the estimated SOC and actual
SOC are within the tolerance range. Consequently, increasing the number of
neurons in the NN is unnecessary unless the number of input items is increased.
Through measuring various types of battery parameters for modifying the
weights and bias values of a trained NN, a mathematical model can be obtained
for estimating battery capacity. Such an estimation method can be applied to
measure the capacity of batteries of various characteristics. Future studies should
consider applying temperature parameters to estimate a change in battery capacity
relative to a change in temperature. In addition, the number of parameters can be
increased to improve the accuracy of battery capacity estimation.
Acknowledgement This study received financial support from the Ministry of Science and Technology under the grants NSC101-2632-E-035-001-MY3.
References
Burkett, W. B., Palisades, P., & Jackson, R. V. (1970, June). Rapid charging of batteries.
U.S. Patent 3,517,219.
Eddahech, A., Briat, O., & Vinassa, J.-M. (2011). Neural networks based model and voltage
control for lithium polymer batteries. In IEEE international symposium, 5–8 Sept 2011. Hagan, M. T., Demuth, H. B., & Beale, M. H. Neural network design. Princeton University Press.
Lee, S. J., Kim, J. H., Lee, J. M., & Cho, B. H. (2007). The state and parameter estimation of an
li-ion battery using a new OCV-SOC concept. In IEEE power electronics specialists confer- ence, 17–21 June, 2007.
Table 40.3 Estimated capacity versus actual capacity of the target battery
Voltage (V) Current (A) Estimate SOC Actual SOC Error
3.34 0.9887 2.10% 2.20% 0.10%
3.57 0.9885 21.70% 21.40% 0.30%
3.68 0.9824 40.50% 40.30% 0.20%
3.86 0.9881 59.70% 59.20% 0.50%
4.08 0.9879 80.00% 79.90% 0.10%
40 The SOC Estimation of LCO Battery Based on BP Neural Network 551
Leksono, E., Haq, I. N., Iqbal, M., Nugroho Soelami, F. X., &Merthayasa, I. G. N. (2013). State of
charge (SoC) estimation on LiFePO4 battery module using Coulomb counting methods with
modified Peukert. In Rural information & communication technology, 26–28 Nov 2013. Linden, D., & Reddy, T. B. (2007). Battary Handbook
Liu R.-h., Sun Y.-k., & Ji X.-f. (2011). Battery state of charge estimation for electric vehicle based
on neural network. In IEEE 3rd international conference (p. 493–496). Sarvi, M., & Adeli, S. (2010). A neural network method for estimation of battery available
capacity. In UPEC2010, 31st Aug–3rd Sept 2010.
552 S.-R. Huang et al.
Chapter 41
Investigating the Effect of Different Refrigerants on the Performance of a Supercritical Organic Rankine Cycle
Duygu Melek Çakıcı and Can €Ozgür Çolpan
Introduction
Consumption of fossil fuels leads to some environmental problems such as pollu-
tions, depletion of the ozone layer and global warming. There has been a high
interest in the renewable energy resources after the oil crisis in the 1970s. Geother-
mal, biomass, wind, solar, and ocean energy resources instead of fossil fuel such as
coal, natural gas, and oil are preferred as they are domestic, clean, economic, and
sustainable resources. One of these renewable energy sources is geothermal energy.
Geothermal energy is thermal energy under the earth. The thermal energy (heat)
from the Earth’s core continuously flows outward. Temperature close to the center of the Earth is around 5500 �C. Scientists estimate that 42 million megawatts (MW) of power flow through the Earth’s interior (http://www.geothermal.org/ what.html). The potential of geothermal energy in Turkey is 31,500 MW (http://
www.eie.gov.tr/yenilenebilir/turkiyede_jeo.aspx). Turkey lies in a highly active
tectonic region. It is located on the Alpine-Himalayan orogenic belt, which has
high geothermal potential. In Turkey, there are high enthalpy grabens and high
reservoir temperature fields. Some of these fields are Büyük Menderes Graben,
Gediz Graben and Simav Graben (DiPippo 2012).
Geothermal energy has been used for different purposes since ancient times such
as bathing, cooking, balneological and health spas, district heating, cooling, green-
houses heating, heat pump and power generation. Geothermal energy can be
classified according to the temperature of the resources. Geothermal resources
can be divided into three groups according to the temperature: Low temperature
fields (<70 �C), moderate temperature fields (70–150 �C), and high temperature
D.M. Çakıcı (*) • C.Ö. Çolpan Department of Mechanical Engineering, Dokuz Eylul University,
Tınaztepe Yerleskesi, Buca, Izmir 35397, Turkey
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_41
553
fields (more than 170 �C) (Acar 2010). High temperature fields are suitable for electricity generation applications. However, it is possible to generate electricity at
lower temperatures with the new technologies. Most of the world’s geothermal power plants were built in the 1970s and 1980s after the oil crisis. The first
geothermal researches in Turkey were started by Directorate of the Mineral
Resource and Exploration of Turkey (called MTA in Turkey) in 1962 (Acar
2010). In Turkey, the first geothermal power plant was built in Kızıldere, in Denizli,
in 1984. According to 2013 data, total installed generating capacity in the world is
11,772 MWe (http://www.geothermal-energy.org/electricity_generation.html).
The potential for electricity generation from these fields are 1500 MWe in Turkey
(http://www.eie.gov.tr/yenilenebilir/turkiyede_jeo.aspx). The short-term forecast
indicates an installed capacity of 18,500 MWe by the year 2015 (Zarrouka and
Moon 2014). The major types of power plants are as follows: Dry-steam power
plants, flash-steam power plants and binary power plants. Binary power plants are
appropriate for electricity production from low and medium temperature geother-
mal sources. Binary power plant consists of two different cycles. In these plants, it
is aimed to increase the efficiency by increasing the temperature of the geothermal
fluid. Organic Rankine cycle and Kalina cycle can be given as examples to this
cycle. Organic Rankine cycle (ORC) is a Clausius Rankine cycle in which an
organic working fluid is used instead of water-steam. In the last years it has become
quite popular due to its suitability for electricity generation in the low-medium
temperatures fields. The processes in ORC are similar to the processes in the
Rankine cycle with steam as the working fluid. In the cycle, thermal energy of
geothermal brine is transferred to the second working fluid.
Some parameters must be considered for optimization of organic Rankine cycle
such as energy and exergy efficiencies of the cycle, the type of the working fluid,
mass flow rate of a working fluid, temperature, pressure and chemical composition
of the geothermal fluid, the reinjection temperature, the ambient temperature, heat
supplied at evaporator or heat exchanger, heat transfer coefficients, pressures drops,
net work output of turbine, cooling load of the condenser, subcritical and super-
critical parameters. The reason for the consideration of these parameters is to find
the optimum operating condition. Franco and Villani (2008) studied medium and
low-temperature water-dominated system. The authors introduced the geothermal
field analyzed, and proposed a methodology for optimizing the geothermal binary
plants. They considered the fundamental variables as follows: Selection of the
working fluid; temperature, pressure and chemical composition of the geothermal
fluid, the reinjection temperature, the ambient temperature and the maximum rate
of energy destruction. Borsukiewicz-Gozdur and Nowak (2007) studied several
ways of increasing the power output of a geothermal power plant based on organic
working fluid. Several types of organic working fluid were used in the analysis.
Hettiarachchia et al. (2007) presented optimum design criterion for organic Ran-
kine cycle using the low temperature geothermal sources. During the optimization
process, objective function is minimized by varying evaporation and condensation
temperature, geothermal water velocity in the evaporator and the cooling water
velocity in the condenser. After their analyses, heat rejection at the condenser, the
554 D.M. Çakıcı and C.Ö. Çolpan
Rankine cycle efficiency, working fluid mass flow rate, heat supplied at evaporator,
exergy efficiency for binary power plant, heat transfer coefficients, pressures drops,
total heat exchanger area, geothermal and cooling water pumping power and
net-power for the cycle were found.
Fluid selection is important for design of the organic Rankine cycle. Basaran and
Ozgener (2013) investigated different refrigerants on the performances of the cycle.
Energy and exergy efficiency were calculated for 12 refrigerants on binary cycle
R236ea, R600, R600a and R227ea (dry type fluid) showed higher energy and
exergy efficiencies. R143a, R415A, R290, and R413a that are wet fluids indicated
lower energy and exergy efficiencies. However, the investigation of supercritical
fluid parameters is high importance. Schuster et al. (2010) compared subcritical and
supercritical fluid parameters. They chose more than one refrigerants for geother-
mal power plant using organic Rankine cycle such as R134a, R227ea, R152a,
isobutane, isopentane. Calculations showed supercritical cycle yields better than
efficiency subcritical cycle. Vetter et al. (2012) worked with different refrigerants
for comparing subcritical and supercritical parameters. In another study,
Borsukiewicz-Gozdur and Nowak (2010) presented theoretical calculations of an
Organic Rankine cycle power plant with supercritical parameters. The temperature
of geothermal water ranged from 95 �C to 120 �C and mass flow rate was taken as 15 kg/s. Four organic fluids were selected as the working fluids in ORC (R115,
R125, R143a, and Propylene). As a result of the calculations, propylene was found
to give the best performance.
In this study, the effect of different refrigerants on performance of supercritical
organic Rankine was investigated. Power output and electrical efficiency of the
supercritical cycle were found for different refrigerants (R134a, R143a, R142b,
R124, R227ea). The equations based on the energy balances of the components of
the system were solved using Engineering Equations Solver (EES). The refrigerant
giving the best performance for the organic Rankine cycle was found.
System Description
Gümüşk€oy geothermal power plant is located in Aydın, Turkey. The plant has been operated and managed by BM Holding since 2013. The geothermal fluid is pro-
duced at a temperature of 178 �C and a pressure of 7.1 bar and the net power output is 5.5 MW. Power plant is based on a supercritical organic Rankine cycle in which
R134a is the working fluid. Operating data is given Table 41.1.
Working principle is as follows: Geothermal wells produce a mixture of steam-
liquid. The temperature of brine is 178 �C and 7.1 bar, respectively. High pressure geothermal fluid from the well is separated as saturated liquid and superheated
vapor in a separator. Superheated vapor enters the heat exchanger. The geothermal
brine transfers its heat to R134a stream in the heat exchanger. The temperature of
R134a reaches the supercritical state before entering the turbine. Then R134a enters
the turbine at a temperature of 151.8 �C and a pressure of 43.7 bar, and power is
41 Investigating the Effect of Different Refrigerants on the Performance. . . 555
produced. R134a leaves the turbine and enters the desuperheater (regenerator). The
aim of desuperheater is to increase the efficiency of the ORC by increasing the
temperature of the working fluid entering the heat exchanger. Working fluid then
enters the air cooled condenser and leaves as saturated liquid. Air enters the
condenser at 18 �C and air leaves at 30 �C. The R134a enters the pump with the 9.47 bar pressure. R134a is pumped into the desuperheater. Then refrigerant enters
the heat exchanger group. Finally, geothermal liquid is sent back to the reinjection
wells. Reinjection wells provide the longevity of geothermal resources. Process
flow diagram is shown in Fig. 41.1.
Modeling
Mathematical modeling of the system is presented in this section. The equations
developed were programmed using Engineering Equations Solver (EES). The input
data in the code used the actual operating data taken from the power plant.
Modeling of the heat exchanger is presented first. Then the energy analysis of the
overall system is presented.
Three shell and tube heat exchangers are used in the system. ε-NTU (effectiveness-number transfer units) method is used in the modeling of the heat
exchanger. To define effectiveness of heat exchanger, we must determine the
maximum possible heat transfer rate, _qmax for the heat exchanger. In the ε-NTU method (Bergman et al. 2006; Ramesh and Dušan 2003), the heat transfer rate from
the hot fluid to the cold fluid in the exchanger is defined as:
_qmax ¼ Cmin � ðTh, i � Tc, iÞ ¼ Cmin � ΔTmax ð41:1Þ
Table 41.1 Operating data of Gümüşk€oy power plant
Parameter Value
Temperature of production well 178 �C Temperature of geothermal fluid entering the heat exchanger-1 164 �C Temperature of R134a entering the turbine 151.8 �C Temperature of geothermal fluid entering the heat exchanger-2 160.6 �C Temperature of air entering the air cooled condenser 18 �C Temperature of air outlet the air cooled condenser 30 �C Pressure of geothermal fluid entering the heat exchanger-1 6.82 bar
Pressure of geothermal fluid entering the heat exchanger-2 7.8 bar
Pressure of R134a entering the turbine 43.7 bar
Pressure of R134a outlet the turbine 9.47 bar
Mass flow of R134a 213.33 kg/s
Mass flow of air 3240 kg/s
Isentropic efficiency of the turbine 0.8
Isentropic efficiency of the pump 0.8
556 D.M. Çakıcı and C.Ö. Çolpan
Th,i is inlet temperature of hot fluid, Tc,i is inlet temperature of cold fluid. Cmin is equal to Cc or Ch, whichever is smaller.
Cc ¼ _mwf � cp,wf ð41:2Þ
Ch ¼ _mgeof luid � cp,geof luid ð41:3Þ
Cc is heat capacity of cold fluid, and Ch is heat capacity of hot fluid. Cold fluid is R134a and hot fluid is the geothermal brine. Effectiveness ε is a measure of thermal performance of a heat exchanger. ε is define as a ratio of the actual heat transfer rate from the hot fluid to the cold fluid to the maximum possible heat transfer rate:
ε ¼ q qmax
ð41:4Þ
Then, for any heat exchanger it can be shown that:
ε ¼ f NTU; Cmin Cmax
� � ð41:5Þ
Cmin Cmax
is equal to CcCh or Ch Cc
. NTU is dimensionless parameter that is widely used for
heat exchanger analysis and is defined as:
NTU ¼ A � U Cmin
ð41:6Þ
HX-1
HX-2
HX-3
Production well
Reinjection well
Turbine
6
5 4
Air cooled condenser
Desuperheater
Pump
Geothermal fluid Working fluid
Air
b
a
7
8 32
1
Fig. 41.1 Schematic diagram of Gümüşk€oy geothermal power plant
41 Investigating the Effect of Different Refrigerants on the Performance. . . 557
A is area; U is overall heat transfer coefficient.
1
U ¼ 1
ho þ do
di � 1 hi
� � þ ln do
di
� � � do
2ktube
� � ð41:7Þ
do is outer diameter of the tube, di inner diameter of the tube, ktube is conductivity of the tube, hi is convection heat transfer coefficient inside the tube, ho is convection heat transfer coefficient outside the tube.
The main assumptions made in the energy analysis are as follows:
• The system runs at steady state conditions.
• Pressure drop and heat loss in pipeline are all neglected.
• Kinetic and potential energies are ignored.
The supercritical organic Rankine cycle is modeled based on the mass and
energy conservation laws. Energy balance of the control volume can be given as:
_Q � _W ¼ X e
_m � _h � X i
_m � _h ð41:8Þ
The power output of the turbine is given by:
_WT ¼ _mwf � h1 � h2ð Þ ð41:9Þ
In the air cooled condenser, _Wfan is calculated as follows:
_Wfan ¼ _mwf � h4 � h3ð Þ þ _mair � h8 � h7ð Þ ð41:10Þ
The power output of the pump is given by:
_WP ¼ _mwf � ðh5 � h4Þ ð41:11Þ
Net work output the system:
_Wnet ¼ _WT � _WP � _Wfan ð41:12Þ
The total heat input of the system:
_Qin ¼ _mgeo � ðha � hbÞ ð41:13Þ
The net electric power generated is defined as:
nel ¼ _Wnet _Qin
ð41:14Þ
558 D.M. Çakıcı and C.Ö. Çolpan
Results and Discussion
The effect of different fluids on the performance of the system is studied. R134a,
R143a, R124, R227ea, and R142b are chosen as the working fluids. Selection
of working fluid has been done considering the turbine inlet temperature as super-
critical. In addition, reinjection well temperature should be at least 60 �C as the minerals found in the brine precipitate below this temperature (Yıldırım and
Şimşek 2003). T-s diagrams for these working are shown fluids in Figs. 41.2, 41.3,
41.4, 41.5, and 41.6.
Thermal analysis was conducted separately for each fluid type. Result of calcu-
lations, reinjection well temperature (Tb), entering temperature of the turbine (T1),
net work output of the system, power input of the pump, power output of the
turbine, electrical efficiency of the system were found. These results are shown in
Table 41.2 for all working fluid.
A parametric study was done with EES. In Fig. 41.7, the effect of condenser
pressure on the work output of the system is shown. Wnet values were calculated for
condenser pressure between to 9 and 15 bars. It is found that as condenser pressure
increases, power output is decreased for all chosen working fluid. The effect of
condenser pressure on the electrical efficiency of the system is shown in Fig. 41.8.
The results show that R143a gives the best performance in Figs. 41.7 and 41.8.
R227ea, R124 and R142b are similar values in Fig. 41.8. R227ea gives the worst
performance. Condenser pressure increases and net fan work increases for the cool.
So that net work output and electrical efficiency decreased.
Fig. 41.2 T-s diagram of the ORC that uses R134a as the working fluid
41 Investigating the Effect of Different Refrigerants on the Performance. . . 559
The effect of production well temperature on the net work output of the system
was studied. Wnet values were calculated for temperature of production well
between 100 and 200 �C in Fig. 41.9. The results show that as the production well temperature increases; power output also increases for all working fluid. The
effect of production well temperature on the electrical efficiency of the system is
Fig. 41.3 T-s diagram of the ORC that uses R143a as the working fluid
Fig. 41.4 T-s diagram of the ORC that uses R142b as the working fluid
560 D.M. Çakıcı and C.Ö. Çolpan
Fig. 41.5 T-s diagram of the ORC that uses R124 as the working fluid
Fig. 41.6 T-s diagram of the ORC that uses R227ea as the working fluid
Table 41.2 The results of the thermal analysis
Working fluids Tb [ �C] T1 [�C] Tcritic [�C] P1 [bar] Pcritic Wnet [Mw] ηel
R134a 77.57 147.7 101 43.7 40.59 6.49 0.1522
R143a 78.55 149.3 72.7 43.7 37.61 8.29 0.1969
R142b 79.06 150 137.1 43.7 40.55 5.30 0.1266
R124 90.77 158.9 122.3 43.7 36.24 4.62 0.1286
R227ea 97.78 159.8 102.8 43.7 29.99 3.94 0.1218
Fig. 41.7 The effect of condenser pressure on the net work output
Fig. 41.8 The effect of condenser pressure on the electrical efficiency
562 D.M. Çakıcı and C.Ö. Çolpan
given in Fig. 41.10. The results show that R143a gives the best performance. The
electrical efficiency of system was calculated for different temperatures of the
production well. This efficiency decreases because of the increase in the reinjection
well temperature.
Fig. 41.9 The effect of production well temperature on the net work output
Fig. 41.10 The effect of production well temperature on the electrical efficiency
41 Investigating the Effect of Different Refrigerants on the Performance. . . 563
Conclusions
In this study, the effect of different working fluids on the performance of an existing
geothermal power plant is investigated. Energy balances developed were
programmed using EES. Using this code, the power output of the turbines, the
power demand of the pumps, the heat input to the heat exchanger, and the net power
output and the electrical efficiency of the cycle are determined. The main conclu-
sions derived from the results of the analyses conducted are listed below:
• The results for net work of the system and electrical efficiency, entering tem-
perature of the turbine and reinjection well temperature are given in Table 41.2.
It is found that R143a gives the best performance.
• Electrical efficiency from highest to lowest, respectively, is as follows: R143a,
R134a, R124, R142b, R227ea.
• As production well temperature increases, electrical efficiency decreases for all
working fluids. As condenser pressure increases electrical efficiency decreases
for all working fluid.
• Although R143a gives the best performance, we suggest that R134a that gives
the second highest performance should be selected as the working fluid in the
Gümüşk€oy power plant. This is due to the fact that the working fluid R134a is non-flammable, non-toxic and yields better performance compared to other
refrigerants (R124, R142b, R227ea).
Acknowledgments The author would like to thank Anıl Erdo�gan, G€okhan Fidan, Ömer Katırcı and the engineers and managers in the Gümüşk€oy plant for their technical contributions.
Nomenclature
A Heat exchanger area, m2
c Specific heat capacity, kJ/kg K
d Diameter of heat exchanger tube, mm
ε Effectiveness hi Convection heat transfer coefficient inside the tube, W/m
2 K
ho Convection heat transfer coefficient outside the tube, W/m 2 K
hair Specific enthalpy of air, J/kg hgeo Specific enthalpy of the geothermal fluid, J/kg k Conductivity of exchanger tube
_m Mass flow rate, kg/s NTU Number transfer units
U Overall heat transfer coefficient, W/m2 K _Wnet Net work output of the system, W
_WT Power output of the turbine, W
_WP Power input of the pump, W
564 D.M. Çakıcı and C.Ö. Çolpan
_Wfan Power input of the fans in the air cooled condenser, W
_q Heat transfer rate per tube area, W/m2
_Q Net heat gain rate, W
Qin Total heat input rate, W nel Electrical efficiency wf Working fluid
References
Acar, H. I. (2010). A review of geothermal energy in Turkey. Energy Sources, 25, 111083–111088.
Basaran, A., & Ozgener, L. (2013). Investigation of the effect of different refrigerants on
performances of binary geothermal power plants. Energy Conversion and Management, 76, 483–498.
Bergman, T. L., Lavine, A. S., Incropera, F. P., & DeWitt, D. P. (2006). Fundamentals of heat and mass transfer. New York: Wiley.
Borsukiewicz-Gozdur, A., & Nowak, W. (2007). Maximising the working fluid flow as a way of
increasing power output of geothermal power plant. Applied Thermal Engineering, 27, 2074–2078.
Borsukiewicz-Gozdur, A., & Nowak, W. (2010). Geothermal power station with supercritical
organic cycle. In Proceedings world geothermal congress, Bali, Indonesia. DiPippo, R. (2012). Geothermal power plants: Principles, applications, case studies and envi-
ronmental impact. Amsterdam: Elsevier. Franco, A., & Villani, M. (2008). Optimal design of binary cycle power plants for water-
dominated, medium-temperature geothermal fields. Geothermics, 38, 379–391. Hettiarachchia, H. D. M., Golubovica, M., Woreka, M. W., & Ikegamib, Y. (2007). Optimum
design criteria for an organic Rankine cycle using low-temperature geothermal heat sources.
Energy, 32, 1698–1706. Ramesh, K. S., & Dušan, P. S. (2003). Fundamentals of heat exchanger design. New York: Wiley. Retrieved December 5, 2014, from http://www.geothermal.org/what.html.
Retrieved December 5, 2014, from http://www.eie.gov.tr/yenilenebilir/turkiyede_jeo.aspx.
Retrieved November 30, 2014, from http://www.geothermal-energy.org/electricity_generation.
html.
Schuster, A., Karellas, S., & Aumann, R. (2010). Efficiency optimization potential in supercritical
Organic Rankine Cycles. Energy, 35, 1033–1039. Vetter, C., Wiemer, H., & Kuhn, D. (2012). Comparison of sub- and supercritical Organic Rankine
Cycles for power generation from low-temperature/low-enthalpy geothermal wells, consider-
ing specific net power output and efficiency. Applied Thermal Engineering, 51, 871–879. Yıldırım, N., & Şimşek, Ş. (2003). Determination of appropriate injection conditions for Kizildere
geothermal waste fluid to avoid scale formation and cooling. In European geothermal conference.
Zarrouka, S. J., & Moon, H. (2014). Efficiency of geothermal power plants: A worldwide review.
Geothermics, 51, 142–153.
41 Investigating the Effect of Different Refrigerants on the Performance. . . 565
Part XI
Environmental Technologies Related to Global Warming
Carbon Capture and Storage (CCS) and Geotechnology Issues
Chapter 42
CaO-Based Sorbents for Post Combustion CO2 Capture via Carbonate Looping
Zinovia Skoufa, Andy Antzara, Ioannis Milios, Eleni Heracleous,
and Angeliki A. Lemonidou
Introduction
In 2007, the Intergovernmental Panel on Climate Change (IPCC) concluded that
worldwide temperature rise is primarily caused by the increase in anthropogenic
greenhouse gases. CO2 is by far the most important of these gases, mainly due to its
abundance (Blockstein and Shockley 2006, Fan 2010). Among several industrial
processes, electricity production sector holds the lion share in CO2 emissions; in
Greece its contribution in CO2 emissions climbs to ~50% (United Nations 2012). In
that context, research aiming at mitigating CO2 emissions particularly from power
plants has received a lot of attention, so that a pure stream of CO2 is collected from
flue gases and subsequently sequestrated in appropriate geological formations.
Among several available processes for carbon dioxide capture, CO2 capture with
amines is a well-established technology that however suffers from serious problems
Z. Skoufa (*) • A. Antzara • I. Milios Department of Chemical Engineering, Aristotle University of Thessaloniki, Thessaloniki
54124, Greece
e-mail: [email protected]; [email protected]; [email protected]; [email protected]
E. Heracleous
Chemical Process and Energy Resources Institute (CPERI), Centre for Research and
Technology Hellas (CERTH), 6th km Charilaou-Thermi Road, P.O. Box 361, Thessaloniki
57001, Greece
e-mail: [email protected]
A.A. Lemonidou
Department of Chemical Engineering, Aristotle University of Thessaloniki, Thessaloniki
54124, Greece
Chemical Process and Energy Resources Institute (CPERI), Centre for Research and
Technology Hellas (CERTH), 6th km Charilaou-Thermi Road, P.O. Box 361, Thessaloniki
57001, Greece
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_42
571
of energetic/economic and environmental importance. First of all, high energy
demands, leading to high operational costs, are associated with the regeneration
of the amine solution. Moreover, there are problems associated with the degrada-
tion of sorbents at higher temperatures, the reactions of amines with compounds
present in the flue gases such as oxygen and SO2 and finally the corrosive nature of
amines and their degradation products (Mandal and Bandyopadhyay 2006, Blamey
et al. 2010, Wang et al. 2014). Therefore, alternative processes for CO2 separation
are extensively investigated, including reactive CO2 separation using dry, solid
sorbents such as limestone, alkali zirconates/silicates and sodium carbonates
(White et al. 2003, Park et al. 2010). Unlike liquid adsorbents, solid adsorbents
can be used over a wider temperature range from ambient temperature to 700 �C. Moreover, they yield less waste during cycling, while the spent solid adsorbents can
be disposed more easily and in an environmentally friendly way (Harrison 2005).
The choice of suitable materials depends mainly on the type of the application that
CO2 capture is intended for. Considering CO2 removal from flue gases, sorbent
properties such as heat tolerance, sorption capacity and stability, fast kinetics are
very important for the economic viability of the process. Cost is also a major factor
for such large scale applications. In this context, calcium oxide is a very attractive
material for carbon dioxide capture, mainly due to high theoretical CO2 capture
capacity of 0.786 g CO2/g sorbent (17.8 mmol CO2/g sorbent) and fast kinetics of
the CO2 capture and release reaction (Broda et al. 2014). Carbonate Looping (CaL)
is an ex-situ, post-combustion CO2 capture technology in which CO2 from flue
gases is captured by a CaO-based sorbent in the carbonator. The carbonate cycle for
post combustion CO2 capture has been chosen by The Technology Task Force of
the European Technology Platform for Zero-Emission Power Plants as one of the
two highest priorities for future research and development (EU 2014). Moreover,
preliminary techno-economic calculations show that calcium looping can separate
CO2 from flue gases at a cost of 25 USD/ton CO2 compared to 50 USD/CO2 that
removal with amine scrubbing currently costs (Epple 2010).
CO2 capture with calcium looping (CaL) is based on the reversible reaction of
calcium oxide with carbon dioxide to produce calcium carbonate, according to the
following reaction:
CaOþ CO2 Ð CaCO3
In a calcium looping cycle (CaL), the CaO-based sorbent is continuously
transferred between two reactors: the carbonator, where the flue gases are stripped
from CO2 by the forward reaction of CO2 uptake, and the calciner, where the
formed CaCO3 is decomposed to regenerated CaO producing at the same time a
concentrated CO2 stream ready to be sequestrated or used as raw material in
downstream chemical processing units. The carbonation reaction is exothermic
and the heat released can be integrated for the realization of the endothermic
reverse reaction (calcination) for sorbent regeneration. The optimal operating
temperatures of both steps are thermodynamically determined from CO2 partial
pressure. Achieving fast CO2 sorption and desorption rates is also a matter of
572 Z. Skoufa et al.
concern. The conditions in the carbonator must strike a balance between the
increased equilibrium conversion obtained at lower temperatures and the faster
reaction rate at higher temperatures. The conditions in the calciner must compro-
mise between the increased rate of the decomposition reaction at higher tempera-
tures and the reduced rate of degradation of sorbent at lower temperatures (Blamey
et al. 2010). Based on the above, the typical temperature window for CO2 capture
from a gas-fired flue gas stream ranges between 600 and 650 �C in the carbonator and above 850 �C in the calciner (Park et al. 2010; Broda et al. 2014).
Key for the large scale deployment of this process is sorbent development. In
view of the carbonation reaction, CO2 sorption process can be divided into two
distinct steps: (1) an initial fast surface reaction controlled by the reaction kinetics
and (2) a slower reaction restricted by the diffusion of CO2 in the CaCO3 product
(Mandal and Bandyopadhyay 2006). An important aspect of the carbonation reac-
tion is the difference in the molar volume of CaO and the product CaCO3.
Therefore, the formation of CaCO3 results in the formation of a product layer of
high molar volume which in turn leads to pore blockage (Broda et al. 2014). Taking
the above into consideration, it is obvious that the sorption capacity of a CaO-based
material greatly depends on its morphological and structural characteristics, mainly
its surface area and porosity. Moreover, taking into account that in practice such a
process comprises several consecutive carbonation/calcination cycles, sorbent
cyclic stability in multi-cycle operation is prerequisite for the successful industrial
implementation of the calcium looping process. Good mechanical properties are
also required for an efficient sorbent material, due to a number of important issues
of solids handling, associated with cohesive particles, attrition and agglomeration,
electrostatic charge effects, etc. (White et al. 2003). CaO derived from the decom-
position of naturally occurring limestone, although cheap, has the major drawback
of rapidly decreasing CO2 capture capacity with a number of repeated carbonation
and calcination cycles (Grasa and Abanades 2006). Several efforts to enhance
physicochemical and sorption characteristics of calcium oxide have been
employed: preparation of synthetic CaO, improvements in the synthesis methods
and synthesis of CaO-based mixed oxides. These efforts, recently reviewed thor-
oughly (Liu et al. 2012), include preparation of synthetic pure CaO sorbents via
different Ca-precursors, different preparation methods as well as doping with a
second metal and/or incorporation of inert materials. These efforts have indeed
proved to be efficient, especially in terms of cyclic stability enhancement
(Martavaltzi and Lemonidou 2008; Angeli et al. 2014).
The majority of published literature on the field reports multi-cyclic evaluation
of novel synthetic and/or natural sorbents in a thermogravimetric apparatus (TGA),
while a few recent papers concern pilot-scale operation of a carbonator/calciner
system (Diego et al. 2014; Dieter et al. 2014; Str€ohle et al. 2014). It is generally accepted that operating conditions, including for example reactor system employed,
carbonation/calcination temperature and feed composition, affect to a significant
extent the evaluation results on sorption capacity and stability (Alonso et al. 2014).
Steam, which is anyway present in flue gases, is reported to enhance sorption
capacity (Manovic and Anthony 2010; Kavosh et al. 2014), whereas no positive
42 CaO-Based Sorbents for Post Combustion CO2 Capture via Carbonate Looping 573
effect was reported in other studies (Sun et al. 2008). Steam has been also used for
regeneration attempts of the sorbents, usually via the incorporation of a hydration
step in the calcium looping cycle (Sun et al. 2008; Li et al. 2014; Coppola
et al. 2014).
In this work, we report the development, preliminary evaluation and bench-scale
testing of synthetic and natural mixed CaO-based sorbents for post-combustion
CO2 capture from industrial plants flue gases. The synthetic materials consist of
CaO-based mixed oxides with Al, Zr, La and Mg, prepared via sol-gel auto-
combustion synthesis using citric acid as a combustion agent. Concerning the
natural CO2 sorbents, we investigated the effect of different pre-treatments on the
sorption capacity and stability of industrial hydrated lime. Mixing with inert
minerals, such as kaolin, bauxite and magnesia, was attempted in an effort to reduce
sintering and degradation under consecutive sorption/desorption cycles. The most
promising materials were further studied at bench-scale in a fixed bed reactor, under
a flow of CO2, O2, H2O and N2 simulating typical flue gases composition from a
power plant. The possibility of hydration-induced regeneration and the effect of
steam in flue gases are also investigated for selected materials.
Experimental
Sorbent Preparation
Four CaO-based powders promoted with Al, Zr, La and Mg were prepared by
sol-gel auto-combustion synthesis using citric acid as combustion agent. The
starting material was Ca(NO3)2·4H2O (J.T. Baker) and the corresponding precursor
for each promoter (Al(NO3)3·9H2O (Carlo Erba), La(NO3)3·6H2O (Merck), Mg
(NO3)2·6H2O (J.T. Baker) and ZrO(NO3)2·xH2O (Acros)). All sorbents were pre-
pared with a constant 66 wt% concentration of free CaO. The required amounts of
calcium nitrate and the precursor of each promoter were dissolved in distilled water
under continuous heating and stirring. Subsequently, the required amount of citric
acid was added to the aqueous solution in order to maintain a constant nitrate salts/
combustion agent molar ratio of 3. The new solutions were heated on a heating plate
to promote water evaporation. After gelation occurred, the formed gel was trans-
ferred to a preheated furnace at 300 �C, where after a few minutes the gel was combusted in a self-propagating combustion manner. The as synthesized powders
were then calcined at 900 �C for 1.5 h under air flow. The sorbents are denoted as Ca-X, where X refers to the promoter (Zr, La, Mg or Al).
Hydrated lime, Ca(OH)2, provided by CaO Hellas was investigated as CaO source for natural CO2 sorbents. Three different pre-treatment protocols were tested
for the activation of raw Ca(OH)2: Protocol 1: the raw material was calcined at 900 �C for 1.5 h under air flow (Ca(OH)2-C900), Protocol 2: the calcined sample was then hydrated with water at 70 �C for 4 h to increase the surface area and as a
574 Z. Skoufa et al.
result the sorption capacity, and was finally recalcined at 600 �C for 3 h in order to decompose the formed Ca(OH)2 during hydration (Ca(OH)2-W-C600) and Proto- col 3: same as protocol 2, excluding final calcination step which was conducted at 900 �C (Ca(OH)2-W-C900). Three natural heat resistant binders were used as means to increase cyclic stability, namely kaolin, bauxite and magnesia obtained
from Prolat, S&B and Grecian Magnesite respectively. Three methods were inves- tigated for the incorporation of the binders: Protocol 4: Ca(OH)2-W-C600 sample obtained from protocol 2 was mixed with Kaolin (Ca(OH)2-KAOL), Bauxite (Ca (OH)2-Baux) or MgO (Ca(OH)2-MgO) in distilled water at 70
�C under continuous stirring for 4 h. The materials were filtered, dried overnight at 120 �C and calcined at 900 �C for 1.5 h under air flow; Protocol 5: raw Ca(OH)2 instead of Ca(OH)2-W- C600 was used as the CaO-precursor, and MgO (Ca(OH)2-MgO-RW) or Bauxite
(Ca(OH)2-Baux-RW) was added following the same procedure as in protocol 4; Protocol 6: raw Ca(OH)2 and MgO were grinded in a mortar for 20 min and the resulting mechanical mixture was calcined at 900 �C for 1.5 h under air flow.
Mixed natural sorbents were all prepared with a constant 66 wt% concentration
of free CaO. Kaolin is a mineral composed mainly of Al2O3 and SiO2 with a general
formula of Al2O3·2SiO2·2H2O, bauxite is composed mainly of Al2O3 and Fe2O3 while the magnesia was mainly MgO with less than 3% impurities, as tabulated in
Table 42.1.
Physicochemical Characterization
Surface areas of the samples were determined by N2 adsorption at 77 K, using the
multipoint BET analysis method, with an Autosorb-1 Quantachrome flow apparatus.
Prior to the measurements, the samples were dehydrated in vacuum at 250 �C overnight.
X-Ray diffraction (XRD) patterns were obtained using a Siemens D500 diffrac-
tometer, with Cu-Kα radiation. The morphology of the synthesized materials was examined by scanning electron microscopy (SEM) on a JEOL 6300 microscope,
coupled with energy-dispersive X-ray analysis (EDX; Oxford Link ISIS-2000) for
local elemental composition determination.
Table 42.1 Chemical composition of MgO, Kaoline and Bauxite binders
MgO-Grecian Magnesite wt% Kaoline-Prolat wt% Bauxite-S&B wt%
MgO 97.30 SiO2 46.55 SiO2 0.87
SiO2 0.50 Al2O3 39.50 Fe2O3 15.27
CaO 1.90 H2O 13.95 TiO2 3.12
Fe2O3 0.05 CaO 0.09
Al2O3 0.25 L.O.I. 14.46
Al2O3 65.77
S 0.03
Zn (ppm) 26
42 CaO-Based Sorbents for Post Combustion CO2 Capture via Carbonate Looping 575
Preliminary Evaluation in TGA
An SDT Q600 (TA Instrument) thermal gravimetric analysis (TGA) instrument was
used for the preliminary evaluation of all sorbent in 100 consecutive carbonation/
calcination experiments. SDT Q600 works in conjunction with a controller and
associated software to make up a thermal analysis system. A small quantity of the
material (5–10 mg), placed in an aluminum sample cup, was pretreated at 850 �C, in the presence of 100 cm3/min pure N2, for 10 min to remove possible humidity and
CO2 absorbed. The CO2 capacity of the sorbents was tested under 15% CO2 flow in
N2 for 30 min at 650 �C while desorption took place under 100% N2 flow for 5 min
at 850 �C. Results are presented in terms of sorption capacity of the materials (mol CO2/kg of sorbent) and CaO conversion. CaO conversion can be expressed as a
function of the weight increase of the sorbent due to CO2 absorption:
X tð Þ,% ¼ MWCaO MWCO2
*%weight increase tð Þ* 1 wCaO
ð42:1Þ
where MWCaO and MWCO2 are the molecular weight of CaO and CO2 respectively,
and wCaO is the weight fraction of free CaO present in the sorbent.
Bench-Scale Testing
The most promising synthetic and natural sorbents according to preliminary eval-
uation in TGA were tested in a bench scale flow unit for 20 consecutive CO2 sorption/desorption cycles. A fixed bed quartz reactor with 18 mm external diam-
eter of the reactor tube in the reaction zone and equipped with coaxial thermocouple
for temperature monitoring was used for testing. The reactor was heated electrically
by a tubular furnace, with three independently controlled temperature zones.
Carbonation was conducted at 650 �C under a 10% CO2/20% H2O/3.2% O2/N2 feed. Calcination was conducted at 800 �C in a 30%H2O/N2 flow. The CO2 concentration in the reactor exit was monitored online by a CO2 analyzer (Horiba,
VIA 510). Sorption capacity of the sorbents, expressed as mol CO2/kg of sorbent, %
CaO conversion and sorption rate (mmol CO2/kg/s) were calculated as follows:
Sorption capacity, molCO2=kgsorbent ¼
ð t 0
MCO2dt
winit ð42:2Þ
X tð Þ,% ¼
ð t 0
MCO2dt
nCaO *100% ð42:3Þ
576 Z. Skoufa et al.
Sorption rate, mmol=kgsorbent= sec ¼ MCO2*10
3
winit ð42:4Þ
where MCO2 are the moles of CO2 captured (mol CO2/s), winit is the initial weight of
the sorbent material (kg) and nCaO are the initial moles of CaO in the sorbent
sample.
Results and Discussion
Physicochemical Characterization
According to XRD analysis (not shown here for brevity), the main crystal phase
formed in all synthetic CaO-based sorbents is CaO, accompanied by minor peaks of
low intensity corresponding to Ca(OH)2 in Ca-Mg, Ca-Al and Ca-Zr samples.
Formation of mixed Ca3Al2O6 and CaZrO3 was observed in Ca-Al and Ca-Zr
sorbents, respectively. On the contrary no mixed phase was formed between CaO
and Mg or La, where the precursor nitrate salts decomposed to MgO and La2O3 respectively (Antzara et al. 2015). Concerning the textural properties of the syn-
thetic sorbents, summarized in Table 42.2, it can be observed that the nature of the
dopant affects the surface area of the final material. Surface areas ranging from
28 m2/g for Mg-doped CaO to 9 m2/g for La-doped CaO were recorded.
The as delivered industrial material (Ca(OH)2) is composed of almost pure
calcium hydroxide, presenting only a small XRD reflection corresponding to
calcium carbonate. After thermal pre-treatment at 900 �C (Ca(OH)2-C900), Ca (OH)2 was almost completely decomposed to CaO with minor Ca(OH)2 reflections.
When the calcined sample was subjected to water treatment and calcined, only
Table 42.2 BET surface area and pore volume of the synthetic and natural CaO-based sorbents
Sorbent Surface area (m2/g) Pore volume (cm3/g)
Ca-Mg 28.37 0.112
Ca-La 8.78 0.138
Ca-Zr 15.28 0.051
Ca-Al 11.93 0.062
Ca(OH)2-C900 5.04 0.041
Ca(OH)2-W-C600 17.24 0.181
Ca(OH)2-W-C900 16.82 0.149
Ca(OH)2-KAOL 3.22 0.023
Ca(OH)2-Baux 5.22 0.0198
Ca(OH)2-MgO 23.25 0.427
Ca(OH)2-Baux-RW 5.29 0.029
Ca(OH)2-MgO-RW 25.49 0.199
Ca(OH)2-MgO-GM 18.7 0.13
42 CaO-Based Sorbents for Post Combustion CO2 Capture via Carbonate Looping 577
reflections at the angular positions of Ca(OH)2 appear, despite the high temperature
used in calcination either at 600 �C or at 900 �C, that was expected to favor hydroxide decomposition to CaO. The addition of kaolin leads to the formation of a mixed phase
Ca3Al2Si2, together with pure Al2O3 and SiO2. Regardless of the preparation method,
in the case of the use of bauxite or MgO as binders, the XRD patterns revealed the
existence of CaO and MgO or Al2O3 crystalline phases, together with low intensity
peaks corresponding to Ca(OH)2 in the case of Ca(OH)2-Baux and Ca(OH)2-Baux-
RW samples, without any formation of mixed components. The surface area and pore
volume of all natural CaO-based sorbents is presented in Table 42.2. Hydration of the
calcined sample leads to an increase in surface area and porosity compared to Ca
(OH)2-C900 sample (Li et al. 2014). Concerning the mixedmaterials, the nature of the
binder seems to affect the textural properties of the final sorbent. The introduction of
kaolin or bauxite in industrial hydrated lime decreases the surface area. On the
contrary, the use of MgO greatly increases the surface area to ~25 m2/g which can
be partly attributed to the high surface area of pure MgO (70 m2/g). Overall, it can be
concluded that basic physicochemical characterization of the natural sorbents
revealed no important effect of the preparation method, whereas doping with MgO
seems to greatly affect both surface area and porosity.
Preliminary Evaluation in TGA
The performance of the four promoted synthetic CaO sorbents is presented in
Fig. 42.1. Although a wide range of surface areas was observed, all the promoted
sorbents (with the exception of Ca-La) achieved very high CaO conversions
Fig. 42.1 CO2 sorption capacity of the synthetic CaO-based sorbents as a function of the number of cycle in TGA
578 Z. Skoufa et al.
(>80%) that could be attributed mainly to the nature of the dopants and the formed structure of the final materials during combustion synthesis (Antzara et al. 2015).
All of the doped sorbents, except Ca-La, exhibit a very stable performance during
the first 70 cycles, unlike the pure CaO prepared with citric acid which deactivates
very fast in the first 20 cycles. Among the different dopants, doping with Zr leads to
the development of the most stable sorbent, followed closely by Al. Moreover, Al
exhibits the highest initial sorption capacity.
Natural sorbents consisting of pure CaO were tested in TGA for 50 carbonation/
calcination cycles. It can be observed (Fig. 42.2a) that water treatment of the
industrial hydrated lime greatly increases the initial CO2 sorption capacity com-
pared to the sample directly calcined at 900 �C, but unfortunately in expense of stability. Sample Ca(OH)2-C900 which presents the highest sorption capacity after
50 cycles was further tested for 100 cycles and the results are compared to those
obtained with doped natural sorbents in Fig. 42.2b. The use of kaolin, bauxite and
MgO binders leads to a decrease initial CO2 sorption capacity due to the lower
content of CaO in the materials, with the exception of Ca(OH)2-MgO-RW and Ca
(OH)2-MgO-GM samples. Nevertheless, CaO conversion increases for all doped
sorbents, indicating the beneficial effect of binders that seem to increase the
accessibility of active calcium oxide surface. Overall, the most promising results
were recorded for samples Ca(OH)2-C900 and Ca(OH)2-MgO-GM, that were
prepared via a solvent-free method. These two sorbents, together with Ca-Al and
Ca-Zr synthetic materials were chosen for further testing in a fixed bed reactor.
Table 42.3 summarizes the preliminary evaluation results for the above sorbents. It
becomes clear that the synthetic CaO-based sorbents exhibited almost twice the
initial sorption capacity of the natural sorbent and a very stable performance with
much lower deactivation after the same number of sorption/desorption cycles.
However, the use of natural sorbents presents important economic and environ-
mental advantages, since they are based on naturally occurring minerals. A feasi-
bility study of the use of either natural or synthetic sorbents exceeds the scope of the
present paper, and should in any case be based on sorbent properties derived after
tens of thousands of cycles (Abanades et al. 2004).
Fig. 42.2 CO2 sorption capacity of the natural CaO-based sorbents as a function of the number of cycle in TGA
42 CaO-Based Sorbents for Post Combustion CO2 Capture via Carbonate Looping 579
Bench-Scale Testing in a Fixed Bed Reactor
After initial sorbent screening in TGA, the most promising synthetic and natural
sorbents were tested in a fixed bed reactor, under realistic feed conditions.
Figure 42.3 presents the results for Ca-Al and Ca-Zr testing in 20 consecutive
carbonation/calcination experiments. It should be noted that the sorption capacity
refers to the amount of CO2 captured in the pre-breakthrough period, i.e. in the
carbonation stage controlled by surface reaction as will be discussed later on. Both
synthetic sorbents present high sorption capacity and satisfactory stability. Given
the differences between experimental set-ups, the sorption capacity recorded in
these experiments is similar to the results obtained in TGA, which refer to the
overall sorption capacity (not just in the pre-breakthrough period. Al-doped CaO
based sorbent presents only 12.5% deactivation after 20 cycles, compared to 23%
deactivation for Ca-Zr.
Carbonation profiles for the 1st and 20th cycle for Ca-Zr sorbent are presented in
Fig. 42.4, where CO2 concentration in reactor outlet and sorption rate, defined as
mmol CO2/kg/s, are plotted versus time. According to the carbonation profiles, CO2 capture proceeds via two distinctive stages. In the first stage, also known as the
pre-breakthrough period, the rate determining step of carbonation is the surface
reaction between CO2 and CaO. During this period, the CO2 concentration is
maintained at very low levels (<2%vol.), indicating a constantly high CO2 capture rate. In the experimental conditions used, both synthetic sorbents approach ther-
modynamic equilibrium CO2 conversion per pass. In the first cycle the duration of
Table 42.3 Preliminary evaluation results obtained from TGA the most promising synthetic and natural sorbents
Ca-Al Ca-Zr Ca(OH)2-C900 Ca(OH)2-MgO-GM
Initial capacity (mol CO2/kg sorbent) 11.64 10.63 5.22 4.54
Initial CaO conversion, % 99 90.3 29.6 38.6
Deactivation after 100 cycles (%) 20.7 13.7 36.5 30.9
Fig. 42.3 Sorption capacity versus number of
cycle for Ca-Zr
(GHSV¼ 318 h�1) and Ca-Al (GHSV¼ 311 h�1) synthetic sorbents in fixed
bed experiments
580 Z. Skoufa et al.
pre-breakthrough period for Ca-Zr sample is ~127 min (Fig. 42.4-left). At that time
~80% CaO conversion is achieved, corresponding to a sorption capacity of
9.02 mol CO2/kg sorbent. As the formation of CaCO3 proceeds, the overall CO2 capture process is governed by diffusion of CO2 through the CaCO3 layer. This step
is generally slower, and Fig. 42.4, it is characterized by fast decrease in the reaction
rate, accompanied by a fast increase of CO2 concentration in reactor outlet. As
already discussed, in a possible industrial implementation of the CaL concept, the
sorbent would exit the carbonator before gradual diffusion becomes rate-
controlling.
As shown in Fig. 42.4-right for Zr-doped CaO-based sorbent, after 19 cycles the
duration of the kinetically controlled period has decreased to 100 min in the 20th
cycle, leading to sorbent deactivation by 23%. Characterization of the spent
sorbent evidenced a 50% reduction in surface area (surface area of used sample:
11.1 m2/g). Characterization of the fresh and used samples with SEM revealed
significant agglomeration of the material after 20 cycles. As shown in Fig. 42.5a,b,
the fresh material is composed of small particles in the range of 10 μm, whereas in the used sample agglomeration led to the formation of larger particles, some of
which are as large as 500 μm (Fig. 42.5e). Nevertheless, it seems that the porous structure of the sorbent is retained to a significant extent, in line with the moderate
degree of deactivation that was recorded for Ca-Zr sorbent. Formation of CaZrO3 mixed phase seems to be the key for the avoidance of extended sintering phenom-
ena, as previously reported (Reddy et al. 2014), due to its high Tamman temperature
(Ruff et al. 1929). Characterization results of the used and fresh samples may
constitute the basis for enlightening the deactivation mechanism of the sorbent.
Due to surface area reduction, the carbonation reaction more quickly falls into
diffusion-controlled regime. Nevertheless, total sorption capacity, calculated as the
total amount of CO2 that was captured throughout carbonation and not just in the
pre-breakthrough period, is the same as in the first cycle. This result indicated that
sorbent did not suffer any loss of intrinsic activity. The stable porous structure
enables CO2 diffusion to the bulk of Ca-Zr particles, even if this step is completed
in a longer time after 20 cycles, as evidence by comparing the diffusion-controlled
period in the 1st and 20th cycle (Fig. 42.4).
Fig. 42.4 Carbonation profiles for the 1st (left) and 20th (right) cycle for Ca-Zr synthetic sorbent
42 CaO-Based Sorbents for Post Combustion CO2 Capture via Carbonate Looping 581
Ca-Al synthetic sorbent presented high sorption capacity, equal to 9.49 mol
CO2/kgsorbent in the pre-breakthrough period which lasted for 110 min, as shown in
Fig. 42.6-left. Compared to Ca-Zr sample, Ca-Al presents higher sorption rate,
leading to higher sorption capacity despite the smaller pre-breakthrough period. In
the 20th cycle, the surface reaction controlled step is reduced to 90 min. As
discussed for the Zr doped sample, the deactivation of Ca-Al sorbent is attributed
to a decrease in surface activity. The total active sites of the sorbent material do not
decrease judging from the fact that the same total amount of CO2 was captured in
cycles 1 and 20. Characterization of the used sample showed a marginal decrease in
surface area (from 12.5 m2/g to 9.3 m2/g) in line with a small deactivation rate of
12.5% after 20 carbonation/calcination cycles. The porous structure of the material
seems to remain almost intact, despite the formation of small agglomerates, as
shown in SEM micrographs (Fig. 42.7).
Fig. 42.5 SEM micrographs of fresh (a, b) and used (c–f) Ca-Zr sorbent
582 Z. Skoufa et al.
Fig. 42.6 Carbonation profiles for the 1st (left) and 20th (right) cycle for Ca-Al synthetic sorbent
Fig. 42.7 SEM micrographs of fresh (a, b) and used (c–f) Ca-Al sorbent
As expected, Ca(OH)2-C900 and Ca(OH)2-MgO-GM natural sorbents presented
significantly lower sorption capacity compared to synthetic sorbents, and intense
deactivation in the first five cycles, as shown in Figs. 42.8 and 42.9. The carbonation
profiles for both natural sorbents in the 1st cycle are shown in Fig. 42.10. Unlike
Fig. 42.8 Sorption capacity versus number of cycle for Ca(OH)2-C900 (GHSV¼ 286.5 h�1) natural sorbent in fixed bed experiments
Fig. 42.9 Sorption capacity versus number of cycle for Ca(OH)2-MgO (GHSV¼ 427 h�1) natural sorbent in fixed bed experiments
584 Z. Skoufa et al.
synthetic sorbents, it can be observed that for the natural sorbents, the breakthrough
period lasts longer than the pre-breakthrough period. In other words, the amount of
CO2 that is captured in the diffusion controlled regime is greater than in the
kinetics-controlled regime, indicating different morphology between natural and
synthetic sorbents. Indeed, pore size distribution evidenced the occurrence of
smaller pores (mesopores) for natural sorbents compared to synthetic samples
that mainly present macroporosity. Consequently, in natural sorbents the easily
accessible surface sites are presumably less compared to synthetic sorbents. More-
over, unlike synthetic sorbents, for which the same activity results were obtained
both in TGA and bench scale testing, both natural sorbents presented higher activity
in the fixed bed reactor experiments compared to the preliminary results in TGA, in
terms of total sorption capacity. This increase of total sorption capacity results from
both surface reaction- and diffusion controlled steps; however the pre-breakthrough
period contributes the most to the observed total capture activity of the solids. In the
TGA setup, the 15% CO2/N2 feed is inserted in the oven in a “flow over” mode as
opposed to “flow-through” conditions in the fixed bed reactor. Moreover, in bench
scale testing the presence of steam might affect the carbonation reaction, as
previously suggested (Manovic and Anthony 2010; Kavosh et al. 2014). According
the results reported in the present study, it can be deduced that the presence of steam
enhances both steps of the carbonation reaction. Overall, based on the above,
enhanced CO2 diffusion to less easily accessible surface sites is probably the reason
for the higher CO2 capture efficiency recorded in the bench-scale experiments for
natural sorbents.
Since the natural sorbents were significantly deactivated during the first five
cycles, two different approaches were studied in an attempt to investigate the
possibility of sorbent regeneration. Concerning Ca(OH)2-C900 sorbent, after the
7th, 8th and 9th cycle, the sample was cooled down from 800 �C (desorption temperature) to 80 �C, under a 30%Η2Ο/Ν2 flow. According to the thermodynamic equilibrium curve for CaO hydration, calcium oxide is hydrated to calcium hydrox-
ide at temperatures lower than 400 �C. The reaction is accompanied by an increase in specific volume, from 16.9 cm3/mol for CaO 33.1 cm3/mol for Ca(OH)2,
Fig. 42.10 Carbonation profiles for the 1st cycle for (a) Ca(OH)2-C900 (GHSV¼ 286.5 h�1) and (b) Ca(OH)2-MgO-GM (B) (GHSV¼ 427 h�1) natural sorbents
42 CaO-Based Sorbents for Post Combustion CO2 Capture via Carbonate Looping 585
ultimately resulting to an increase in surface area and porosity (Li et al. 2014).
As shown in Fig. 42.8, the hydration procedure led not only to containment of
sorbent deactivation, but also to a significant increase (~180%) in sorption capacity
from cycle 7th to 10th. It should be noted here, that in case of process scale-up the
addition of such a regeneration procedure would not be economically efficient, in
terms of energy needs for cooling down and re-heating the regenerated sorbent.
Cycles 10–15 were conducted without a hydration step, and as shown in Fig. 42.8,
the sample was again deactivated following roughly the same trend as in the first six
cycles. In order to investigate the effect of steam presence in the flue gases, cycles
16, 17 and 18 were performed in the absence of steam in the feed, leading to a sharp
decrease of the sorption capacity from 8.85 mol CO2/kg in cycle 15–2.51 mol CO2/
kg in cycle 18. Overall, the above results indicate that the presence of steam in the
feed increases CO2 capture efficiency and promotes sorbent stability, most probably
by facilitating CO2 diffusion.
As shown in Fig. 42.9, Ca(OH)2-MgO-GM sorbent presents an initial sorption
capacity of 6.03 mol CO2/kg, and is deactivated by ~33% within the first five
cycles. The second approach to regenerate the sorbents was then investigated for Ca
(OH)2-MgO-GM sorbent. After calcination at 800 �C, the sample was cooled down
to 300 �C and left to react towards Ca(OH)2 under a 55% Η2Ο/Ν2 flow for 3 h. This hydration process resulted in an increase in sorption capacity, as shown in Fig. 42.9.
For the next cycles up until cycle 20 the carbonation/calcination procedure was
repeated without any intermediate regeneration step and the sorbent continued to
deactivate; an overall ~49% deactivation was finally recorded.
Table 42.4 summarizes the bench-scale results for CO2 capture. It is obvious that
the synthetic sorbents prepared by sol-gel auto-combustion synthesis presented
superior capture activity and stability compared to the natural sorbents derived
from industrial hydrated lime. In view of the important conclusions derived from
the comparison of TGA and fixed bed reactor testing and characterization of spent
solids, it can be deduced that the superiority of synthetic sorbents lies in their
porous structure. On one hand, this porous structure enhances CO2 capture by
maximizing the available CaO surface. On the other hand, the addition of Zr and
Al leads to the formation of thermally stable CaZrO2 and Ca3Al2O6 mixed phases
that provide stability. The final choice on whether synthetic or natural sorbents
should be used in a potential scale up will be determined by techno economic
factors, taking into account the cost of sorbent development versus the need for
sorbent make-up due to deactivation.
Table 42.4 Summary of CO2 capture results (pre-breakthrough time) obtained in the fixed bed reactor for the four selected sorbents
Ca(OH)2-C900 Ca(OH)2-MgO-GM Ca-Zr Ca-Al
Initial sorption capacity,
mol CO2/kgsorbent
7.80 6.03 9.02 9.49
Initial CaO conversion, % 43.7 51.2 76.6 80.6
Deactivation after 20 cycles, % 13a 48.7a 12.5 23 aAfter (several) hydration steps, see text for details
586 Z. Skoufa et al.
Conclusions
CO2 capture from flue gases via carbonation calcination cycles over CaO-based
sorbents is a promising technology. In the present study, several synthetic and
natural sorbents were developed and preliminary evaluated in TGA. Synthetic
sorbents prepared by sol-gel auto-combustion technique exhibited high sorption
capacity and stability. Natural sorbents derived from industrial hydrated lime
presented promising results; the preparation procedure seems not to significantly
affect activity and stability. The most promising synthetic, Ca-Zr and Ca-Al, and
natural, pure CaO derived from Ca(OH)2 direct calcination and MgO-doped Ca
(OH)2, were tested in a fixed bed reactor under realistic flue gas feed composition.
Zr and Al-doped CaO based sorbents exhibited very high sorption capacity and
stability over 20 consecutive carbonation/calcination cycles, owing to the porous
structure obtained by the auto-combustion technique and retained due to the
presence of thermally stable Ca-Zr and Ca-Al mixed phases. The natural sorbents
presented inferior results, however their regeneration via hydration seems possible,
although most likely not economically viable. The presence of steam in the flue
gases seems to enhance sorption capacity and stability. Ca-Al synthetic sorbent
exhibited the most promising performance and shows great potential for process
scale up.
Acknowledgement We acknowledge the financial support from European Union-European Regional Development Fund and Ministry of Development, ESPA 2007–2013/EPAN II
programme, Action Synergasia11’.
Nomenclature
f Total flow rate, cm3/s
MCO2 Moles of CO2 captured, mol CO2/s
MWCaO Molecular weight of CaO
MWCO2 Molecular weight of CO2 nCaO Initial moles of CaO in the sorbent sample
wCaO Weight fraction of free CaO present in the sorbent
winit Initial weight of the sorbent, kg
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42 CaO-Based Sorbents for Post Combustion CO2 Capture via Carbonate Looping 589
Chapter 43
Kinetics of CO2 Capture by Carbon Dioxide Binding Organic Liquids
Ozge Yuksel Orhan, Hakan Kayi, and Erdogan Alper
Introduction
CO2 emissions from human activities are consistently rising with the increase of
population growth and industrialization (Couchaux et al. 2013). Industries such as
chemical and petrochemical manufacturing, cement and steel production and nat-
ural gas processing are responsible for the largest sources of CO2 emissions (Liu
et al. 2014). Since CO2 is regarded as a major greenhouse gas that causes the global
warming and climate change problems, effective and economic CO2 capture tech-
nologies have gained importance. The most common and proven approach to
capture CO2 from gas streams is chemical absorption (Kumar et al. 2014). There-
fore, aqueous solutions of alkanolamines, such as monoethanolamine (MEA),
diethanolamine (DEA) and methyldiethanolamine (MDEA) are widely used sol-
vents for the removal of acid gas impurities such as CO2 and H2S (Alexia Finotello
et al. 2008; Kierzkowska-Pawlak et al. 2013; Garđarsd�ottir et al. 2015). Solvents for such absorption processes absorb CO2 from gas streams efficiently at low temper-
atures by an exothermic reaction resulting either carbamate or bicarbonate salts.
Regeneration of traditional amine solutions can be achieved by desorption at near
atmospheric pressures but high temperatures such as 120–130 �C (Finotello et al. 2008) are required. Therefore, the energy-intensive stripping requirement
(especially, the reboiler duty) is one of the disadvantages for using aqueous
alkanolamines arising from high specific and latent heats of water. In addition,
O. Yuksel Orhan (*) • E. Alper Department of Chemical Engineering, Hacettepe University, Beytepe, 06800 Ankara, Turkey
e-mail: [email protected]; [email protected]
H. Kayi
Chemical Engineering and Applied Chemistry Department, Atilim University, İncek, 06836
Ankara, Turkey
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_43
591
thermal stripping of CO2 from aqueous alkanolamines at temperatures higher than
boiling point of the water leads to large evaporative losses of solvent. Further,
amines (especially MEA) at high concentrations have been reported to be respon-
sible for stress corrosion cracking. Accordingly, solvent loss, corrosive nature and
high energy intensive properties are major drawbacks of amine based technologies
(Guo et al. 2013).
Consequently, there are considerable on-going research and development to
design new solvents to reduce (or eliminate) the high latent heat requirement of
the aqueous systems. The key factors for solvent selection are high absorption
capacity, fast absorption rate, cost effectiveness, low corrosiveness, high solvent
stability and low energy requirement for regeneration (Liu et al. 2014). A new
approach to handle these conflicts is to employ a liquid absorbent medium of an
organic base in a non-aqueous, polar solvent. For instance, Jessop et al. (2005)
developed CO2-binding organic liquids (CO2BOLs).
CO2BOLs are smart solvents comprised of amidine/guanidine bases and organic
alcohols that capture CO2 and form amidinium or guanidinium alkyl carbonate
salts. It is presumed that the base of CO2BOL does not react directly with CO2, as
amines react to form carbamates. Conversely, the alcohol group in the CO2BOL
reacts firstly with CO2 to form an alkyl carbonic acid, and then protonates the base
to form a liquid alkylcarbonate (Mathias et al. 2013). Alkyl carbonate salts formed
are non-volatile ionic compounds and they do not contain as much hydrogen bond
as carbamate and bicarbonate salts do. Therefore, binding enthalpy of CO2 decreases and high stripping temperatures that amine systems need are no longer
required (Gordesli et al. 2013).
CO2BOLs can reversibly switch from non-ionic form to ionic form when
exposed to carbon dioxide and causes a notable increase in polarity (Jessop
et al. 2012). Then, CO2 is removed from CO2BOLs below the boiling point of
the mixture by simple heating or sweeping with an inert gas such as nitrogen.
They have tunable physicochemical properties; the solvent reverts back to its
less-polar non-ionic form and is ready for future CO2 uptake (Tao Yu et al. 2008).
The main advantages of these systems are high CO2 binding capacities, low heat
capacities and lower energy requirement for regeneration as compared to aqueous
alkanolamine solutions (Mathias et al. 2013). Wang et al. developed several
strategies to reduce volatility of superbase-derived absorbents by making them
such as alcohol-functionalized ionic liquids (Wang et al. 2010). Currently, several
CO2BOL systems are being investigated by us and one of these studies focuses on
reaction kinetics of CO2BOLs, composed of a mixture of 1,8-diazabicyclo [5.4.0]
undec-7-ene (DBU) amidine base in 1-hexanol or 1-propanol (Ozturk et al. 2012).
The others are focused on reaction performance and kinetics of CO2BOLs,
composed of a mixture of 1,1,3,3-Tetramethylguanidine (TMG) guanidine
base in 1-hexanol and 1-propanol, with carbon dioxide (Ozturk et al. 2014;
Yüksel Orhan et al. 2015). However, the observed rate constants reported in
these works are relatively low which can be enhanced by addition of
small amounts of activators such as piperazine and its derivatives (Moioli and
Pellegrini 2015).
592 O. Yuksel Orhan et al.
Analysis
Generally, the mechanism of the reaction between CO2 and amine systems can be
explained by two established mechanisms. These are the zwitterions mechanism,
originally proposed by Caplow in 1968, and then reintroduced by Danckwerts in
1979 and termolecular reaction mechanism proposed by Crooks and Donnellan
(1989) and modified by Ozturk et al. (2014).
The zwitterion mechanism, also known as a two-step mechanism, involves two
sequential reactions. In the first step, CO2 reacts with the amine (denoted here as
RNH2) and forms zwitterion intermediate product as in Eq. (43.1). In the next step,
this zwitterion reacts with a base (or bases) and a proton from zwitterion is
transferred to the base (B), resulting in a protonated base and carbamate ion. As
shown in Eq. (43.2), a water molecule, an additional amine, or any other basic
species can act also as the base.
CO2 þ RNH2 € k 2
k-1
RNþH2COO- ð43:1Þ
RNþH2COO- þ B ���! kB
RNHCOO- þ BHþ ð43:2Þ When the base is amine and the carbamate ion is stable, the resulting net reaction
is given in Eq. (43.3).
CO2 þ 2 RNH2 € RNHCOO- þ RNH3þ ð43:3Þ The termolecular reaction mechanism assumes that an amine reacts with both
one molecule of carbon dioxide and one molecule of a base in a single step as
illustrated in Fig. 43.1. It is also assumed that the reaction takes place via the
weakly-bound intermediate product as shown in Eq. (43.4).
CO2 þ RNH2� � �B € RNHCOO-� � �BHþ ð43:4Þ The modified termolecular reaction mechanism for CO2BOLs, containing
amidine/guanidine base and a linear alcohol, is shown in Eq. (43.5). While a
Fig. 43.1 Schematic drawing of a termolecular reaction mechanism (Crooks and Donnellan 1989)
43 Kinetics of CO2 Capture by Carbon Dioxide Binding Organic Liquids 593
fraction of this complex reacts with a second molecule of the amine or alcohol
molecule to form alkyl carbamate salt, a fraction of resulting intermediate breaks up
to form reactant molecules (CO2 and amine).
CO2 gð Þ þ B lð Þ þ ROH lð Þ € BHþ �
ROCOO-½ � lð Þ ð43:5Þ
Under pseudo-first order conditions where the solvent would be in excess, the
observed forward reaction rate can be expressed as in Eq. (43.6).
robs ¼ ko CO2½ � ð43:6Þ The observed reaction rate constant (ko) can be expressed by Eq. (43.7) in terms
of CO2BOL/alcohol system.
ko ¼ kB B½ � þ kROH ROH½ �f g B½ � ð43:7Þ Since, alcohol concentration is assumed to be in excess for the pseudo-first order
conditions, ROH can be considered constant and a new rate constant, k, can be
defined by Eq. (43.8).
k ¼ kROH ROH½ � ð43:8Þ
ko ¼ kB B½ � þ kf g B½ � ð43:9Þ
As seen in Eq. (43.9), if the amine and alcohol are comparably dominant bases,
degree of the reaction can change between 1 and 2. Also if the alcohol is the
dominant base, system exhibits a first-order reaction and Eq. (43.9) reduces to
Eq. (43.10).
ko ¼ k B½ � ð43:10Þ In summary, the rate constants of CO2BOLs were obtained by using Eqs. (43.9)
and (43.10).
Material and Method
Reagents
Reagent grade 1,5,7-Triazabicyclo[4.4.0]dec-5-ene (TBD) with purity of 99%
(CAS no. 5807-14-7) and 1,5-Diazabicyclo[4.3.0]non-5-ene with purity of 98%
(CAS no. 3001-72-7) were supplied by Sigma-Aldrich (St. Louis, MO, USA).
1-Hexanol with 98% purity (CAS no. 111-27-3) was also obtained by Sigma-
Aldrich. Carbon dioxide with a purity of 99.99%was obtained from Linde (Munich,
Germany). Reagent grade chemicals were used without further purification.
594 O. Yuksel Orhan et al.
Kinetic Measurement
The observed reaction rate constants of the amines with CO2 in 1-hexanol were
measured over a range of temperatures (278, 298 and 308 K) using a customised
stopped-flow instrument (Hi-Tech Scientific, UK, Model SF-61SX2). The
conductivity-detection system of the apparatus calculates directly the intrinsic
rate of a rapid homogeneous reaction by measuring the conductivity change during
the reaction. All parts of the flow circuit, with the exception of the stop/waste
syringe, are thermostated and the temperature control is better than �0.1 K. During an experimental run, amine (TBD or DBN)/1-hexanol solution and carbon dioxide
dissolved 1-hexanol solution were placed in the sealed drive syringes in the sample
unit. For each experimental run, equal volumes of the solutions were mixed
instantaneously in a stainless-steel cell for the reaction to occur and the flow was
stopped. The ion formation initiates a voltage change which is monitored as
function of time. Then, the equipment software calculates the pseudo-first order
reaction rate constants of the rapid homogeneous reaction based on least squares
regression. A typical experimental output from the standard stopped flow system is
shown in Fig. 43.2. To obtain consistent pseudo-first-order rate constants (ko), each
experimental set was repeated for an average ten times. The amine and alcohol
concentrations were always much in excess to that of CO2 (usually the molar ratio
was about 20:1) to satisfy the pseudo-first-order conditions. The main advantages of
the stopped-flow technique are easy operation, quick experiment run (~0.05 s),
small amount of solvent consumption for each experimental run (~ 0.1 mL) and
no effect of gas phase resistance (Liu et al. 2014). Further details of the equipment
and experimental procedure can be found elsewhere (Ume et al. 2012; Yüksel
Orhan et al. 2015).
Fig. 43.2 Combined avg. graphs of 5 wt% DBN/1-hexanol system at 298 K
43 Kinetics of CO2 Capture by Carbon Dioxide Binding Organic Liquids 595
Results and Discussion
In order to evaluate the potential integration of these switchable solvents to
industrial carbon dioxide capture applications, the reaction kinetics between
CO2BOLs and carbon dioxide were examined. In this work, as an amidine; DBN
(1,5-Diazabicyclo[4.3.0]non-5-ene) and as a guanidine; TBD (1,5,7-Triazabicyclo
[4.4.0]dec-5-ene) were used in 1-hexanol medium. Intrinsic reaction rates were
measured in “stopped flow” equipment for a temperature range of 298–308 K.
Experiments were carried out by varying organic base (amidine or guanidine)
percentage in a 1-hexanol medium from 5.0 wt% to 20.0 wt%.
Table 43.1 shows a summary of observed pseudo-first order reaction rate
constants for the CO2/TBD/1-hexanol system versus the weight-percent concentra-
tion of TBD at temperatures ranging from 288 K to 308 K. Table 43.1 shows clearly
that ko increases by increasing concentration or temperature.
In order to determine the reaction order of the CO2/TBD/1-hexanol system, the
natural logarithms of observed reaction rate constants versus TBD concentrations
were plotted as shown in Fig. 43.3. Empirical power law kinetics was fitted to lines
Table 43.1 Observed pseudo-first order rate
constants for the CO2/TBD/
1-hexanol system at different
temperatures
ko [s �1]
TBD [wt%] 5 10 15 20
288 K 253.1 420.6 526.4 690.7
298 K 463.5 645.4 912.8 1190.1
308 K 621.7 969.6 1190.1 1490.2
Fig. 43.3 Determination of the apparent reaction order for the CO2/TBD/1-hexanol system at various temperatures
596 O. Yuksel Orhan et al.
in Fig. 43.3 by using the least square method. Their slopes correspond to the
reaction orders of the CO2/TBD/1-hexanol system which are determined to be
approximately 0.6 with regression values of R2¼ 0.99 for the 5.0–20.0 weight percentages at a temperature range of 288–308 K. The experimentally observed
ko values were correlated using the termolecular mechanism to determine the
forward reaction rate constant k [m3 kmol�1 s�1]. The reaction rate constants vs. TBD concentration were plotted according to Eq. (43.6) in a very satisfactory
pseudo-first-order plot as seen in Fig. 43.4.
From the slopes of the fitted lines in Fig. 43.4, the first-order forward reaction
rate constants for CO2/TBD/1-hexanol systems were determined to be 451.21 m 3
kmol�1 s�1 at 288 K, 727.16 m3 kmol�1 s�1 at 298 K and 898.36 m3 kmol�1 s�1
at 308 K.
Similarly, observed pseudo-first order rate constants for the CO2/DBN/
1-hexanol system at 288, 298 and 308 K were determined. The summary of
obtained observed reaction rate constants versus the weight-percent concentration
of DBN at temperatures ranging from 288 K to 308 K are given in Table 43.2.
In Fig. 43.5, the natural logarithms of the observed rate constants (ko) are shown
as a function of versus DBN concentrations for the 5.0–20.0 weight percentages at a
temperature range of 288–308 K. By fitting empirical power law kinetics to lines in
Fig. 43.4 Pseudo-first order rate constant as a function of TBD concentration at various temperatures
Table 43.2 Observed pseudo-first order rate
constants for the CO2/DBN/
1-hexanol system at various
temperatures
ko [s �1]
DBN [wt.%] 5 10 15 20
288 K 79.8 211.5 271.9 360.5
298 K 145.4 409.3 521.9 699.4
308 K 216.1 548.5 689.1 891.2
43 Kinetics of CO2 Capture by Carbon Dioxide Binding Organic Liquids 597
Fig. 43.5, the reaction orders of CO2/DBN/1-hexanol system were found about 1.00
with high R-squared value. This result is in agreement with the pseudo-first-order
reaction suggestion of a single-step termolecular reaction mechanism for
CO2/DBN/1-hexanol system. In order to determine the forward reaction rate con-
stants k [m3 kmol�1 s�1], the experimentally observed ko values were correlated as seen in Fig. 43.6.
Fig. 43.5 Determination of the apparent reaction order for the CO2/DBN/1-hexanol system at various temperatures
Fig. 43.6 Pseudo-first order rate constant as a function of DBN concentration at various temperatures
598 O. Yuksel Orhan et al.
From the slopes of the fitted lines in Fig. 43.6, the first-order forward reaction
rate constants for CO2/DBN/1-hexanol systems were determined to be 271.75 m 3
kmol�1 s�1 at 288 K, 524.46 m3 kmol�1 s�1 at 298 K and 683.61 m3 kmol�1 s�1 at 308 K.
Activation Energies
In order to determine the activation energies, the Arrhenius diagrams were plotted
as shown in Figs. 43.7 and 43.8. Activation energies for both CO2/TBD/1-hexanol
system and CO2/DBN/1-hexanol were calculated by evaluating the Arrhenius
equation as in Eq. (43.11).
k ¼ A exp �Ea RT
� � ð43:11Þ
Figure 43.7 shows the Arrhenius diagram for CO2/TBD/1-hexanol system at 5.0,
10.0, 15.0 and 20 wt%, respectively. Using the slopes of these plots, activation
energies for the CO2/TBD/1-hexanol system were calculated as 33.25 kJ/mol at
5.0 wt%, 30.79 kJ/mol at 10.0 wt%, 30.46 kJ/mol at 15.0 wt% and 28.44 kJ/mol at
20.0 wt%. Figure 43.8 shows the Arrhenius diagram for CO2/DBN/1-hexanol
system at 5.0, 10.0, 15.0 and 20 wt%, respectively. Using the slopes of these
plots, activation energies for the CO2/DBN/1-hexanol system were calculated as
37.18 kJ/mol at 5.0 wt%, 35.37 kJ/mol at 10.0 wt%, 34.43 kJ/mol at 15.0 wt% and
33.54 kJ/mol at 20.0 wt%.
Fig. 43.7 Arrhenius diagram for the CO2/TBD/1-hexanol system
43 Kinetics of CO2 Capture by Carbon Dioxide Binding Organic Liquids 599
The stable lowest energy conformers of organic bases (TBD and DBN) obtained
from the B3LYP/6-31G(d) calculations are given in Figs. 43.9 and 43.10. As
expected, the activation energy of TBD is lower than the activation energy of
DBN since the amino group of TBD is not hindered (Figs. 43.9 and 43.10).
Finally, the obtained results of this work were compared with the published
papers of other CO2BOLs in 1-hexanol medium at 298 K are shown in Table 43.3.
However, the ko values are generally low in comparison with MEA or PZ
systems (Ume et al. 2012; Gordesli et al. 2013; Yuksel Orhan and Alper 2015),
they are comparable to DEA systems (Marta Siemieniec 2011).
Fig. 43.8 Arrhenius diagram for the CO2/DBN/1-hexanol system
Fig. 43.9 B3LYP/6-31G (d) optimized lowest energy
conformers of 1,5,7-
Triazabicyclo[4.4.0]dec-
5-ene (TBD) (atom types:
white¼H, gray¼C, blue¼N) (Color figure online)
600 O. Yuksel Orhan et al.
Conclusion
The reaction between organic bases (TBD or DBN) and CO2 was investigated and
modeled using a single termolecular reaction mechanism. Although, the observed
rate constants obtained in this work are lower than the other commercial carbon
dioxide capture agents, this can be enhanced by addition of small proportion of
activators such as piperazine and its derivatives as shown by Yuksel Orhan and
Alper (2015). CO2BOLs are potential candidates for industrial carbon dioxide
capture with beneficial properties, such as requiring a smaller reboiler duty in the
desorber. This work provided kinetic data for two of these novel CO2BOL systems
which are needed for rate-based modeling.
Acknowledgement This work was supported by a Turkish Scientific and Technological Research Council (TUBITAK) through a research project (Project No.: 213M390). Authors gratefully
acknowledge this financial support.
Nomenclature
CO2BOLs Carbon dioxide binding organic liquids
B Base (i.e., amine, water, or hydroxyl ion)
CO2 Carbon dioxide
DBN 1,5-Diazabicyclo[4.3.0]non-5-ene
Table 43.3 Comparison of kinetic properties of various CO2BOLs at 298 K
Amines
TBD/
1-hexanol
DBN/
1-hexanol
TMG/
1-hexanol
DBU/
1-hexanol
Reference This work This work Ozturk et al. (2014) Ozturk et al. (2012)
Reaction order 0.63 1.09 0.98 1.21
k (m3 kmol�1 s�1) 727.16 524.46 64.10 627.0 Ea (kJ mol�1) 30.74 35.13 9.76 13.7
Fig. 43.10 B3LYP/6-31G (d) optimized lowest energy
conformers of
1,5-Diazabicyclo[4.3.0]
non-5ene (DBN) (atom
types: white¼H, gray¼C, blue¼N) (Color figure online)
43 Kinetics of CO2 Capture by Carbon Dioxide Binding Organic Liquids 601
DBU 1,8-Diazabicyclo[5.4.0]undec-7-ene
DEA Diethanolamine
GHG Greenhouse gas
Ea Activation energy
kOH Rate constant for alcohol, m 3/kmol s
kB Rate constant for base according to Eq. (43.7), m 3/kmol s
ko Observed pseudo–first-order-rate constant, s �1
MDEA Methyldiethanolamine
MEA Monoethanolamine
SCC Stress corrosion cracking
TBD 1,5,7-Triazabicyclo[4.4.0]dec-5-ene
TMG 1,1,3,3-Tetramethylguanidine
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43 Kinetics of CO2 Capture by Carbon Dioxide Binding Organic Liquids 603
Chapter 44
Flue Gas CO2 Sequestration by Turkish Coal Fly Ashes and Anatolian Geothermal Hot Waters
Yıldırım _Ismail Tosun
Introduction
The increasing CO2 concentration in the Earth’s atmosphere, mainly caused by fossil fuel combustion, has led to concerns about global warming. A technology that
could possibly contribute to reducing carbon dioxide emissions is the in-situ
mineral sequestration (long term geological storage) or the ex-situ mineral seques-
tration (controlled industrial reactors) of CO2.
Carbonation of CO2 gas has many various advantages. Most distinct fact is that
carbonates have a lower energy state than CO2. Mineral carbonation is thermody-
namically occurs in nature (i.e., the weathering of rock over geologic time periods).
Further, the raw materials such as magnesium based minerals are abundant on earth.
The produced carbonates are basely stable and thus re-evolve of CO2 into the
atmosphere is not an issue. However, conventional carbonation reactions are slow
under ambient temperatures and pressures.
Forty percent of global electricity is generated in fossil fuel power plants per
annum, with emissions of about 33% (9.5 billion metric tons) of global energy
related CO2 emissions of approximately 28.8 Gt in 2010 (Minchener and McMullan
2007; IEA 2012). Over half of the electricity demand of the Turkey is supplied by
coal-fired power plants, with emissions of about 16 million metric tons of CO2 per annum, representing about 33% of Turkey energy-related CO2 emissions
(TKI 2009; TTK 2009).
Therefore, developing effective CO2 sequestration is one of the critical compo-
nents in addressing global climate change. Note that improving the efficiency of
energy production and utilization, and developing renewable energy sources will
certainly play a very important role in reducing CO2 emissions (5), however these
Y.İ. Tosun (*) Mining Engineering Department, Şırnak University, Şırnak, Turkey
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_44
605
measures alone cannot address the greenhouse emissions issue mainly because
world energy consumption will increase significantly as the living standard
improves in many parts of the world.
Three boreholes, one injection well, and two observation wells will be drilled,
about 50–100 m (160–330 ft) apart, into the flank of an anticlinal structure. A total
of up to 1 t/day of CO2, in gaseous state at the well head, will be injected at about
700 m (2300 ft) depth into a saline mudstone aquifer. Injection is planned to start at
the end of 2013 and last for approximately 2 years, during which the distribution
and fate of the injected gas will be monitored by surface geophysical surveys and by
downhole instrumentation. Various processes and subprojects and work packages
address the science and operational aspects of CO2 (IPCC 2005; Stangeland 2007;
Solomon 2006; O’conner et al. 2000; Siegenthaler and Oeschger 1987; Keeling
et al. 1995; Plasynski et al. 1999). The proposed part of the project is restricted to
the baseline survey and the injection and basic monitoring of CO2. The supply of
CO2 will be provided by near Coal Power Station in Şırnak. Other choice will be the
purchase of a pure CO2 originating from flue gas of hydrocarbon production at an
oil refinery. The CO2 will be delivered by truck in liquid phase, temporarily stored
at the well site, and conditioned before injection. The project proposed plans to
inject the CO2 at the well head in gaseous phase at a slightly supercritical pressure
and slightly supercritical temperature. The anticline at Şirnak-Silopi was used for
gas storage in the past in a shallower depth interval in Şırnak-Silopi pit mine field,
which also is an mining industry partner in CO2 sequestration and will be respon-
sible for the CO2-injection operations.
This paper discussed progress on reactor achieved by tests and search for fast
reaction methods using exhaust gas containing waste sulfur and carbon gases at the
stack of Power Stations. This experimental study demonstrates that 1 ton of fly-ash
could sequester up to near 20 kg of CO2, i.e. 50 ton of fly ash per ton of CO2 sequestered. This confirms the possibility to use this alkaline residue for CO2 mitigation. Other alkaline sources containing calcium, magnesium and magnesium
salts, supercritical CO2, water slurry, and additives were searched for optimum
sequestration methods and also in order to enhance mineral reactivity; and in
analyzing the structural changes to identify reaction paths and potential barriers.
Carbonation liquid and gaseous products may change to near 20%–45% yield
performances by time increase from 1 to 6 h.
CO2 Sequestration and Carbonation
Options for storing CO2 in deep underground geological formations need adequate
porosity and thickness for storage capacity and permeability for gas injection are
critical. The storage formation should be capped by extensive confining units such
as shale, salt caves or anhydrite beds to ensure that CO2 does not escape into
overlying, shallower rock units and ultimately to the surface. Geological storage of
CO2 requires compression of CO2 to allow injection. This is done by compressing
606 Y.İ. Tosun
the CO2 to a dense fluid state known as ‘supercritical’. This supercritical state is achieved by exposing the CO2 to temperatures higher than 31.1
�C and pressure greater than 73.9 bars. The density of CO2 will increase with depth, until about
800 m or greater, where the injected CO2 will be in a dense supercritical state (DOE
1998; Simbeck 2004; Burruss 2004; Oldenburg et al., 2001).
The mineral carbonation, a process of converting CO2 into stable minerals—
mineralization has been studied extensively to capture and store CO2 (Stevens
et al. 2001). However, most of the mineral carbonation studies have been largely
investigated at lab scale. Preliminary and pilot scale studies for accelerated mineral
carbonation (AMC) were conducted at one of the largest coal-fired power plants
(2120 MW) in the USA by reacting flue gas with fly ash particles in a fluidized bed
reactor. In the preliminary experiments, flue gas CO2 and SO2 concentrations
decreased from 13.0% to 9.6% and from 107.8 to 15.1 ppm, respectively, during
the first 2 min of reaction (Stevens et al. 1999). The flue gas treated by fly ash
particles, even mineralization hold high mercury (Hg) concentration of 0.22 mg/kg
in flue gas (Myer 2003; Zweigel et al. 2001).
Geothermal brine waters utilization and using CO2 as feed material in mineral
carbonation produce various environmentally benign products. However, many
challenges to any solution include technical feasibility, economic viability, envi-
ronmental soundness and long term sustainability for mineralization of CO2 (Pacala
2003; Hepple and Benson 2003).
Method of Mineral Sequestration
Mineral sequestration involves the reaction of CO2 with minerals to form geolog-
ically stable carbonates. This mineralization of CO2 was searched by different
studies using various materials (Lindeberg 2003; Rubin and Rao 2003). General
and specific global mineral carbonation reaction pathway is shown in Fig. 44.1. The
goals of the current work were to design an ash–water suspension carbonation
process in a continuous mode laboratory-scale plant and to search for potential
means of intensifying the water neutralization process (Davis 2004; Seifritz 1990;
Kojima et al. 1997; Gunter et al. 1993; Lackner et al. 1995). The carbonation
process was optimized by cascading columns in which the pH progressed from
Fig. 44.1 General chemical
mineralization path
44 Flue Gas CO2 Sequestration by Turkish Coal Fly Ashes. . . 607
alkaline to almost neutral. The amount of CO2 captured from flue gases can reach
0,01–0,12 kg/l at the 500 �C temperature and 10 bar pressure level (O’Connor 1998). Laboratory-scale neutralization experiments were carried out to compare the
reactor designs. Sedimentation of carbonate particles was observed and their main
characteristics were determined.
Mineral carbonation reactions are known to geologists and occur spontaneously
on geological time scales. For example, the reaction of CO2 with common mineral
silicates to form carbonates like calcite and magnesite or calcite is exothermic
and thermodynamically favored (O’Connor 1998; Butt et al. 1997; Drägulescu et al. 1972).
The family of reactions represented by Reaction 44.1 has the potential to convert
naturally occurring silicate minerals to geologically stable carbonate minerals and
silica (Goldberg et al. 2000). This process follows natural chemical transformations
such as weathering of rocks to form carbonates over geologic time periods. Reac-
tion 44.2 illustrates the transformation of the common silicate mineral serpentine
(Goff et al. 1997), Mg3Si2O5(OH)4, and CO2 into magnesite, MgCO3, silica and
water. Using this ideal case, 1 ton of serpentine can dispose of approximately
one-half ton of CO2. Reaction 44.3 illustrates the transformation of forsterite,
which is the end member of the common silicate mineral olivine. One ton of olivine
can dispose of approximately two-thirds of a ton of CO2. Again, the reaction is
exothermic and releases 90 kJ/mole of CO2.
Mg;Cað ÞxSiyOx þ 2yþ zH2z þ xCO2 ! x Mg;Cað ÞCO3 þ ySiO2 þ zH2O ð44:1Þ
1=3 Mg3Si2O5 OHð Þ4 þ CO2 ! MgCO3 þ 2=3 SiO2 þ 2=3 H2O þ 64 kJ=mole:
ð44:2Þ
1=2 Mg2SiO4 þ CO2 ! MgCO3 þ 1=2 SiO2 þ 90 kJ=mole ð44:3Þ
A conceptual illustration of the projected Fly ash mineralization process is
presented in Fig. 44.2. As illustrated, CO2 from one or more power plants is
transported to a carbonation reactor, combined with fly ash slurry tank and held
at the appropriate reaction conditions until the desired degree of carbonation is
Fig. 44.2 Chemical reaction process of fly ashes for sequestration in the diagram
608 Y.İ. Tosun
reached. Careful control of solution chemistry yielded olivine conversions of 90%
in 24 h and 83% within 6 h. The most recent results show further modifications of
the same basic reaction can achieve 65% conversion in 1 h and 83% conversion in
3 h. A recent literature review indicated that weak carbonic acid treatments had also
been suggested for Mg extraction in the prior literature (O’Connor 1998). Carbon- ation tests performed at ARC employing heat pretreated serpentine have resulted in
up to 83% conversion in 30 min lower than 115 bars (O’Connor 1998). Indeed, by increasing sodium bicarbonate concentration the carbonation reaction of serpentine
can reach 62% completion under 50 bars. Waters contains various natural ele-
ments. Substantial fractions of these elements in springs could be lost during clay
rock pores leak. 50–60% of arsenic, lead, manganese, mercury and selenium could
be removed by salt transforming in cooling.
Then products of the reaction, which might be slurry of carbonated minerals and
residues and lean gas CO2 in aqueous, are separated. The residual CO2 is recycled.
Useful materials are collected for construction works or the carbonated materials
and residue are returned to the mine site. Almost calcium and magnesium oxide
(MgO) content in the magnesium silicate ore mineral of 40% and 60–70% chem-
ical efficiency of the carbonation reaction; mass balance of equation 44.1.
A 100 MW power plant in Sırnak-Silopi, generating approximately 200 tons/day
of CO2, would require just over 140 tons/day of calcium and magnesium containing
fly ash. Several fly ash types in Turkey containing sufficient calcium and magne-
sium oxide quantity in silicate mineral to provide raw materials for the mineral
carbonation.
Experimental Work
In this research, representative specimens the different types of Turkish geothermal
hot water sources Sirnak, were classified to calcium content and bicarbonate by
chemical analysis. Gas samples of 10–20 kg tubes from each different coal power
stations were used. Screen analysis of Turkish lignite samples were made by
standard Tyler Screens and particle size distributions and normal distributions of
Turkish fly ash samples are respectively illustrated from Fig. 44.3.
Number citations consecutively in alkali waters were reacted by waste gas in the
process reactor (Fig. 44.2) and solution distributions were investigated at each stage
of sequestration. Specific surface area of fly ash minerals was about 4.76–6.2 m2/g
determined by BET surface analyzer and highly sufficient in order to react with
gaseous CO2. 80% of weights of fly ash were reacted in 10 bar alkali solution. Main
reactive salt structure is widely distributed and pores structures are associated with
clay minerals. Coarse alkali oxides are also seen (Table 44.1).
From these results, we designed and developed laboratory scale process unit
consisting a three consecutive autoclave reactors (1 m Φ� 0.7 m) to capture and carbonize flue gas CO2. Flue gas was filtered and withdrawn from the gas tube and
was fed to the autoclave with fly ash slurry at about 7 l/s. The cyclone and decanter
44 Flue Gas CO2 Sequestration by Turkish Coal Fly Ashes. . . 609
Fig. 44.3 Particle size distribution and normal size distribution of the fly ash used in carbonation process
Table 44.1 Chemical analysis of Turkish fly ash used in the experiment
Chemical composition
Soma fly
ash F
Yatagan fly
ash F
Silopi fly
ash F
Afşin Elbistan
fly ash F
SiO2 (S) 42.14 52.05 40.4 20.4
Al2O3 (A) 17.12 23.69 4.1 7.1
Fe2O3(F) 4.34 5.94 15.96 4.96
CS+CAF 63.26 81.68 81 88
CaO 29.6 19.60 24.7 64.7
MgO 1.53 2.38 2.1 3.1
K2O 1.15 2.51 1.55 0.55
Na2O 1.29 2.56 1.25 0.250
Loss of ignition 0.34 0.90 5.22 4.22
SO3 3.43 1.45 2.2 2.4
Density (g/cm3) 2.22 2.12 1.9 2.0
Loose unit weight (g/cm3) 0.72 0.88 0.71 0.69
610 Y.İ. Tosun
unit separates ash and aqueous water. The salt particles were fluidized by flow of
slurry through a slurry tank and pump. The laboratory scale studies were conducted
at a controlled pressure (115.1 kPa) by controlling the flue gas content. The flue gas
was continuously monitored to measure flue gas CO2, SO2 and NOx concentrations
by an industrial grade gas analyzer, while the fresh and spent ash were analyzed for
calcium carbonate (CaCO3), sulfur (S), and mercury (Hg) content.
Results and Discussion
The major technical challenge now hindering the use of minerals to sequester CO2 is theirs low reaction rate. Weathering of rock is extremely slow. The highest
priority is given to identifying faster reaction pathways. The optimized process
has to be economical. Although many carbonation reactions are exothermic, it is
generally very difficult to recover the low-grade heat while the long reaction time
and demanding reaction conditions.
The environmental impact from mining, mineralization and carbonation pro-
cesses must be considered in sequestration. We succeeded in achieving shortened
carbonation reaction times employing fly ash containing lime and calcium magne-
sium silicates such as gehlenite, mehlenite. Reaction took 4 h to reach 40–50%
completion of carbonation. The reaction required temperatures of 450–550 �C, pressures of 10–20 bar, and mineral particles in the �100 μm size range. Because the high pressure requirement of the carbonation reaction will certainly lead to high
process costs, the team is modifying solution chemistry to allow reaction to proceed
at a lower pressure and temperature. The research showed that the concentration of
HCO3 � in the solution is critical to the reaction rate. The high CO2 pressure will lead
increased CO2 absorption in the solution and thus enhance the HCO3 � concentra-
tion. Adding bicarbonate such as sodium bicarbonate in the solution will signifi-
cantly increase the HCO3 � concentration even at a relatively lower CO2 pressure.
In experiments with 3 h reaction period at reactor temperature of 500 �C and fly ash slurries were kept under changing CO2 pressure ranged 5 bar to 40 bar. Products
were subjected to analysis for carbonate yield determination. Test results of yields
for different Turkish fly ash sources were seen in Fig. 44.4.
That quantity in the carbonation amounts were determined for different source
evaluation and reduce the effect of gas content of waste gas in order to optimize
carbonation rates. As given in Fig. 44.4 gas conversion yield for steam and ash
samples were greatly differed. Yata�gan and Elbistan Fly ash showed high carbon- ation yields reaching 32% and 30% respectively. Because of active lime amounts
were over 20% and even alkali Na and K contents were over totally over 5%, the
higher carbonation yields were sufficiently provided by three consecutive carbon-
ation columns at 20 bar.
In the carbonation experiments with addition alkali, reactor temperature changed
between 200 and 650 �C and ash slurries were mixed with active lime additionally by 10% rate. Products received from carbonation of ash specimens were subjected
44 Flue Gas CO2 Sequestration by Turkish Coal Fly Ashes. . . 611
to analysis for gas hold-up determination. Test results of carbonation by fly ash and
also alkali lime contained over active lime at 10% weight rate were investigated.
In experiments with 3 h reaction period of ash specimens, at reactor temperature
changed between 200 and 600 �C and all ash samples contained over active lime at 10% weight rate. Products were subjected to analysis for carbonate yield determi-
nation. Test results of carbonation yields of Turkish fly ash sources and additional
10% lime were seen in Fig. 44.5.
As given in Fig. 44.5 carbonation yield for steam and ash samples were linearly
changed between 200 and 650 �C. Yata�gan and Elbistan Fly ash showed high carbonation yields reaching 44% and 24% at 650oC, respectively. Because of
low reaction kinetics below 500 �C and even the effect 10% over dosage of active lime content in the reactors were ranged over 3% carbonate yield per hour, the
higher carbonation yields were sufficiently provided over 500 �C at 20 bar. In the carbonation experiments, the experimental conditions were controlled on
the basis of the gas composition in the ambient state. So neither the contained water
vapor nor the others, slurry was taken into account. In order to determine the effect
of reaction period on carbonation yield for Turkish fly ash samples, the tests were
carried out in three consecutive carbonation columns at 500 �C and 20 bar between1min to 6 h. Yata�gan and Elbistan Fly ash showed high carbonation yields reaching 33% and 26% at 500oC at 3 h reaction period, respectively. Because of
low reaction kinetics below 30 min reaction period in the reactors, yield rates were
ranged over 1% carbonate yield per hour, the higher carbonation yields were
sufficiently provided over 2 h reaction period at 20 bar. Carbonation of slurries
and yield products changed to 37% and 29% for Yata�gan and Elbistan Fly ash, respectively, by time increase from 1 to 6 h (Fig. 44.6).
Fig. 44.4 Effect of carbonation time over conversion yield rates in hot 500 �C steam used
612 Y.İ. Tosun
Fig. 44.5 Effect of time of carbonation over conversion yield rates in steam with 10% additional lime used at 20 bar
Fig. 44.6 Effect of time of carbonation over conversion yield rates in hot waters used at 500 �C and 20 bar
44 Flue Gas CO2 Sequestration by Turkish Coal Fly Ashes. . . 613
Conclusion
The qualitative comparison of the carbonation for three different Turkish fly ash
reactants and products revealed a complete MgO, CaO–MgO to MgCO3-CaCO3 conversion. The carbonation efficiency of CaO was dependent on the initial pres-
sure of CO2 of 20 bar. This was significantly affected by reaction temperature
500 �C and by the fly ash dose 100 g/l. The kinetic data demonstrated that the initial rate of CO2 transfer was enhanced by carbonation process for our experiments. The
precipitate calcium carbonate was characterized by isolated micron sized particles
and micron agglomerates of calcite.
This study reveals suitable large scale operating units in order to achieve the
carbonation method as a viable sequestration tool at industrially relevant scales by
using Turkish fly ashes in 500–600 �C waters. Carbonation liquid and gaseous products may change to near 20–40% yield performances by time increase from
1 to 6 h.
While there is a potential to utilize other types of flue ashes in mineralization,
lime or similar alkali can be evaluated to sequester CO2 allowing clearly significant
amounts. Even there are researches succeeded usage of serpentine and olivine.
Consequently, the flue gas should be continuously monitored to measure flue gas
flow at depleted gas outlet in order to reprocess it.
Carbonation of the ash slurries and carbonation yield products changed to 37%,
29%, 25% and 19% for Yata�gan, Elbistan, Silopi and Soma Fly ash, respectively, by time increase from 1 to 6 h.
Other harmful emissions caused by flue gas containing high sulfur (S), and
mercury (Hg) content can be eliminated by this method. In that study, results
suggested that an appreciable amount of flue gas CO2 and significant amounts of
SO2 and Hg can be directly captured and mineralized by the fly ash particles.
Even with progress made so far, to develop an economical method to
sequester CO2 with minerals is still a challenging task, because the process is still
relatively slow, and most reactions require high pressure and moderately elevated
temperature.
Acknowledgment The author would like to thank the Mining Engineering Department of Süleyman Demirel University, Isparta.
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616 Y.İ. Tosun
Chapter 45
Geo.: Gas Production in Offshore Reservoirs in Brazil’s Pre-salt Region
Isabella Vaz Leal da Costa, Pedro Rochedo, Mariana Império,
Alexandre Salem Szklo, and Roberto Schaeffer
Introduction
The expectations regarding the oil sector in Brazil are very promising, both by the
extent of the sedimentary basins of interest for hydrocarbon exploration untapped
(about 7 million square kilometers), but also because of the recent discoveries in the
pre-salt region (BNDES 2010; Wood Mackenzie 2013). Petrobras estimates that
there are between four billion and eight billion recoverable barrels in Lula field and
four billion barrels in Iara field. Besides these, there are the Jubarte field (Campos
Basin) and (the ring-fence) Golfinho in the Espı́rito Santo Basin. The estimates of
the total reserves in the pre-salt region (between 70 billion and 100 billion barrels),
if confirmed, make Brazil a oil exporting country in the next few years (BNDES
2008; ANP 2014; Wood Mackenzie 2013).
However, we must also consider the difficulties linked to the pre-salt, mainly
because of its geographical location. The pre-salt reserves are located at a depth of
over 6000 m, with about 2000 m corresponding to a layer of salt. So there are a lot
of difficulties to extract the hydrocarbons deposited in the pre-salt layer, requiring
special materials and equipment, with technologies that aren’t fully developed yet (Petrobras 2014). Some of these difficulties are showed below:
• Going through a thick layer of salt in deep waters is not a trivial task;
• Plasticity and the solubility of the pre-salt layer will require new technologies to
maintain the well stability;
I.V.L. da Costa (*) • P. Rochedo • M. Império • A.S. Szklo • R. Schaeffer Energy Planning Program, Graduate School of Engineering, Centro de Tecnologia, Federal
University of Rio de Janeiro, Bloco C, sala 211, Cidade Universitária, Ilha do Fund~ao, Rio de Janeiro 21941-972, Brazil
e-mail: [email protected]; [email protected]; [email protected];
[email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_45
617
• Hydrocarbons are located in carbonate rocks, environment that is unknown by
Petrobras activities because their experience is concentrated in other types of
rocks such as sandstones;
And finally, the production occurs in a high temperature and pressure, at the
presence of large CO2 content between 10% and 45 mol% (Formigli 2008; Dino
2014; Credit Suisse 2014), which may be stored in the same underground field.
Petrobras believes that these difficulties can be overcome in the following years
(Petrobras 2011). In addition to the technological difficulties, there is the challenge
of producing hydrocarbons at an average distance of 170 km from the Brazilian
coast, distributing over a range of about 800 km of coastline extension of the states
of Espı́rito Santo and Santa Catarina (BNDES 2010).
According to estimates made by Petrobras (2014), Brazil will become self-
sufficient in oil products in the year 2020. In addition, the domestic supply of
natural gas will increase from 41 million cubic meters per day in 2013 to 86 million
m3/day, in 2020. Imports of Bolivia will remain at 30 million cubic meters/day
(contract expiring in 2019), plus the import via liquefied natural gas (LNG). By
2013, two LNG regasification plants were already in operation phase (27 million m3
/day) and the additional third plant started operation in 2014 (14 million cubic
meters/day) (Petrobras 2014).
The pre-salt oil fields contain large amounts of carbon dioxide (CO2), which
prevents the transportation of natural gas to the coast. CO2, when in contact with
water, forms acids such as carbonic acid, making it very corrosive that can cause
damages to the pipelines and equipment (Nascimento 2012). The presence of CO2 decreases the calorific value of natural gas, and helps the formation of hydrates at
low temperatures and high pressures, which are precisely the flow conditions of the
natural gas present in the pre-salt area (Nascimento 2012).
Thus, the need for separation of CO2 from natural gas produced in the pre-salt
becomes necessary to their production. The process of carbon capture and storage
(carbon capture and storage—CCS) has been used worldwide by large oil and
natural gas companies. In the oil extracting sector, this process is aimed precisely
to separate CO2 from the natural gas extracted. However, a high CO2 content in the
natural gas, reduces the amount of natural gas that can be produced. In the case of
the pre-salt region, the Brazilian natural gas production is related to the amount of
carbon dioxide present in the pre-salt fields.
So, this paper presents an estimate of the natural gas production in the pre-salt
fields, drawn from a model developed in HYSYS software, considering the amount
of CO2 estimated for this region.
618 I.V.L. da Costa et al.
Carbon Capture and Geological Storage Review
Carbon Capture and Geological Storage (CCGS)
CO2 Capture and Geological Storage systems (CCGS) are recognized worldwide
as alternatives to reduce carbon dioxide emissions from stationary sources
(IEA 2008; IPCC 2007; Rochedo 2011; Nogueira et al. 2014; Costa 2009, 2014).
These practices are used in the global oil industry to reduce emissions, for example,
in the offshore fields of exploitation in Norway (Sleipner Field) and onshore fields
in Algeria (Costa 2009, 2014; Roddy 2011; Statoil 2013a).
The first capture demonstration plant that is operating on an industrial scale is
the plant installed at Sleipner, Norway, located in the North Sea and operated by
Statoil since 1996 (Statoil 2014a). This plant is also the main CCGS offshore
project in the world. The Sleipner T platform was built especially for separating
CO2 from natural gas and has being able to separate one million tons of CO2 per
year. These platforms use chemical absorption technology with amine based sol-
vents for the separation of gases, used in post-combustion (Rochedo 2011). It is
worth mentioning that for the pre-salt fields, FPSOs (Floating Production, Storage,
and Offloading) are being used. In the pre-salt area the conditions are more severe
due to the distance from the coast and the depth, so it would be best not to use
chemical absorption technology that has large equipment that can generate insta-
bility on the floating platforms.
The In Salah project in Algeria is another CO2 capture project, conducted by
Statoil, which uses the same separation technology that was already applied in the
Sleipner field, based on the process of amines (Statoil 2014b). The project became
operational in 2004, and contains a storage industrial scale. Several fields with a
carbon dioxide content between 1 and 10 mol%, in order to adapt the natural gas to
the specifications of 0.3 mol% of CO2 present in the composition of the natural gas,
are injecting CO2 into deep saline formations, between 1850 and 1950 feet deep
(Mathieson et al. 2010). By 2010 were injected over three million tons of carbon
dioxide (Mathieson et al. 2010). However, the CO2 injection was discontinued in
2011 as a safety measure, mainly related to reservoir capacity. New data and
seismic results are being studied to create a more appropriate strategy for this
reservoir injection (Statoil 2014b).
CO2 Capture in the Pre-salt Fields
The CO2 capture can be performed before (pre-combustion), or after the use of
natural gas (post-combustion). This study is considering that the capture of CO2 is
directly made of associated gas extracted in the pre-salt fields (pre-combustion). It
is important to mention that the capture of CO2 from gas flaring and from gas
combustion for power generation did not occur. It is, also, worth mentioning that is
45 Geo.: Gas Production in Offshore Reservoirs in Brazil’s Pre-salt Region 619
not possible to capture the total amount of CO2 emitted by oil and gas production
platforms. Here comes to light the concept of "capturable" CO2. The “capturable”
CO2 is the portion of CO2 emitted mainly in the oil and natural gas extraction due to
generation of heat and/or burning fossil fuels, due to the industrial sector and due
to the use of fossil fuels in plants for generation of electricity. In these situations
it is feasible to separate CO2 using at least one of the technological routes
available. Technological routes includes pre-combustion, post-combustion and
oxy-combustion. In addition, it is only captured about 85% mol of “capturable”
CO2 due to technical limitations of existing methods of gas separation (Costa 2014;
Roddy 2011; Rochedo 2011; Kuramochi et al. 2012).
The capture method most suitable for the new pre-salt platforms (FPSOs) would
be the membranes (Dino 2014). Membranes are structures that act as selective
barriers for molecules that are able to cross from one side to another. In the gas
separation, membrane technology is based on chemical or physical interaction of
the gas with the membrane which allows certain gases to go through the membrane
at higher speeds than others.
Membrane performance was determined by the permeability and selectivity of
the materials, which the membranes are made of. The permeability is defined by the
ability to be penetrated with a certain driving force at once. Permeability is
generally indicated by units such as barrer or flux and, selectivity by the ratio of
the permeability of the gas components. The membrane separation takes place
through different mechanisms, which have important influence on the selectivity
and permeability.
Membranes are industrially applied in the form of flat sheets or hollow fibers. In
the case of hollow fibers, the fibers are joined into a tubular beam. Membranes in
flat form are usually produced as a sheet of spiral modules, where two membrane
sheets are placed back-to-back, in the middle of a material which, ensures the
minimum space required to keep the gas flow.
These models have extremely high surface-volume ratios and offer advantages
related to costs and footprint (Schendel 1984).
Therefore, in the case of the platforms to be used in the exploitation of the
pre-salt fields, the use of membranes is justified mainly due to its footprint, which is
significantly smaller than the footprint of conventional absorption technology. A
membrane module has a smaller footprint than a capture plant using, for example,
the chemical absorption method. The space required to accommodate all the
equipment used to capture by chemical absorption is not usually available on a
FPSO. The layouts of the FPSO are well defined and restrict. Furthermore, this kind
of platform is not able to deal with the structure instability by installing equipment
for chemical absorption (Rochedo 2011; Dino 2014; Castelo Branco 2008).
After the capture method selection (membranes), the UOP Separex™ system, was chosen as a standard module for the separation of CO2 in the pre-salt
FPSOs (UOP 2013; Petrobras 2014; Echt and Meister 2009). According to UOP
(2013), these modules were bought by PETROBRAS to separate CO2 from seven
million m3 of natural gas per day in the pre-salt fields. In addition, eight modules
will be installed on production platforms (FPSO) in the Santos Basin. It is
620 I.V.L. da Costa et al.
estimated that a UOP Separex™ system (membraneþ skid) module occupies an area of approximately 347 m2 and weigh about 582 tons (Harness and Sharma
2012). This is a compact module suitable for oil and gas production platforms
because it can reduce the occupied area for gas separation equipment in a platform
(footprint) by 70% (Harness and Sharma 2012).
According to Petrobras (2014) and UOP (2013), will be used the same type of
membrane module in all FPSOs exploiting the pre-salt region. So, according to this
information, in this study, we made the assumption that all membrane modules
would be the same. Moreover, it is worth mentioning that the number of modules
should vary depending on the daily production capacity of each FPSO.
Methodology
Oil and natural gas exploration and production in Brazil occurs mostly offshore and
in deep waters. For the accomplishment of upstream sector analysis in Brazil, in this
study, information about typical marine installations of oil and natural gas produc-
tion located in Campos basin were used. These installations have electric power
system, using their own produced natural gas as an input. Using typical installations
was an assumption taken in this study due to the difficulty in the acquisition of
process data about all marine installations in all Brazilians basins. Campos Basin
represents more than 75% of Brazilian production.
The methodology used to estimate pre-salt natural gas production was divided in
three phases. Initially, it was adopted that pre-salt natural gas derives only from the
associated gas. Thereby, natural gas production is linked to pre-salt oil production.
Hence, the first phase was estimating oil production and number of platforms
required in pre-salt. For this, the oil curve developed by Saraiva (2013), where a
Multi-Hubbert modeling was made, was adopted. This modeling considers the total
volume of ultimately recoverable resources (URR), according to different proba-
bilities of adding reserves, to accomplish the oil production projection. Base year of
2010 has been updated with real oil production data (ANP et al. 2013a; Credit
Suisse 2014) and then an interpolation was made to reach oil production projection
made by Saraiva (2013) for 2015.
This Saraiva’s (2013) result, with a production of 3.8 million bpd, is clearly above numbers that will be achieved in 2015, which probably will be around 2.8
million bpd (Petrobras 2014). However, the aim of this study is building a long-term
scenario, where the current adversities undergone by Brazilian oil industry should,
by hypothesis, be overcome. This evaluation is even reported by Goldemberg
et al. (2014) projection, which clearly distinguishes the role of production arising
out the oil under the onerous assignment tax regime, for which Petrobras has
expended considerable resources.
In this sense, it’s worth noting that Petrobras has been focusing its investments for pre-salt region (Petrobras 2013). Therefore, even with large production
increases in pre-salt region, total production in 2012 and 2013 showed a decline,
45 Geo.: Gas Production in Offshore Reservoirs in Brazil’s Pre-salt Region 621
returning to 2010 levels (BDEP-ANP 2014; Reuters Brasil 2014). In 2012, for
example, Roncador field showed a 27% decrease in its production. In 2014,
Brazilian production increased again (BDEP-ANP 2014), but it was still far
below the post-salt region forecast developed by Saraiva (2013), which was used
in this work.
As a result of oil production, an estimate for pre-salt platforms was also made,
considering that new offshore facilities will be FPSO due to exploitation in deep
and ultra-deep waters. All platforms implemented in the same year will have the
same average capacity. This average capacity increases over time, due to increased
production resulting from pre-salt, which requires larger platforms to process the
estimated oil volumes for this region. Therefore, three different capacities platforms
had been used, with a daily production of 100, 150 and 200 thousand barrels of oil.
Based on pre-salt oil production, the second phase was accomplishing the
estimated natural gas gross production. According to IEA (2014), the extracted
gas amount from the processing of a pre-salt barrel of oil is around 40 m3. Total gas
extracted comes from the multiplication of 40 m3 of natural gas by the estimated
number of platforms, considering the average capacity of each platform. Bypass is
subtracted from extracted gas, resulting in natural gas gross production. Therefore,
each platform will have its respective gross gas production average capacity. Since
there is still much uncertainty about the precise amount of CO2 present in pre-salt
natural gas, a wide range was used, between 10%mol of CO2 and 45%mol of CO2,
as proposed by the available scientific literature (Echt and Meister 2009; IEA 2014;
Credit Suisse 2014). Thus, three classifications have been proposed for estimated
natural gas quantities associated with pre-salt resources: (1) total amount of
extracted gas; (2) natural gas gross production (extracted gas minus bypass); and
(3) natural gas net production (gross production minus platform auto-consumption
and energy penalty from membrane system used in CO2 capture). Equations (45.1)
and (45.2) refer to the amounts of natural gas represented by aforementioned
classifications.
NG GROSS PROD ¼ EXTRACTED GAS � BYPASS ð45:1Þ NG NET PROD ¼ GROSS NG PROD � AC þ EPð Þ ð45:2Þ
Note: NG Gross Prod¼Natural gas gross production (m3); NG Net Prod¼Natural gas net production (m3);
AC ¼ Auto� consumption on platforms m3� �; EP ¼ energy penalty m3� �: Regarding the gross natural gas produced and bypass, they were calculated from
a modeling made in HYSYS software, which took into account the membranes’ properties used in UOP Separex™ membrane module and CO2 content range considered in this study. Reinjection volumes and gas production for a single
module were also obtained through HYSYS model, as well as the composition of
each of these gases. These data are different for different CO2 contents considered.
622 I.V.L. da Costa et al.
According to platform capacity, a gross extracted gas volume from the field may
exceed membrane capacity. This volume does not pass by the membrane (bypass),
and it is directly injected into the reservoir along with the gas rich in CO2 captured
in the membrane, as shown schematically in Fig. 45.1.
The third phase consists in estimating natural gas net production, which is the
amount that actually can be transported to the coast and be available to natural gas
processing units (NGPU). Energy penalty considered by using membranes was the
electrical energy used by compressors for CO2 reinjection in reservoirs. This energy
was estimated based on compressor power, dimensioned by HYSYS® model, to process gross natural gas volumes on membranes for each platform capacity.
Compressors powers are shown in Table 45.1.
Then, considering compressors operating 24 h a day throughout the year, energy
that would be used by compressors is given in GWh and m3 of natural gas. These
values are calculated according to platforms estimates, their capacities and com-
pressors powers. They are presented in Table 45.2.
Platform auto-consumption, refers to energy consumption in platform, which
includes activities such as gas reinjection for oil recovery, transportation to pipe-
lines, power generation for operational activities and accommodations in offshore
platforms, heat and steam production, among others. Auto-consumption used in this
study was 3.2 m3/bbl, derived from oil and gas ratio and auto-consumption per-
centage (Maia 2007; ANP 2013b).
Fig. 45.1 Membrane functioning scheme
45 Geo.: Gas Production in Offshore Reservoirs in Brazil’s Pre-salt Region 623
Then, with natural gas gross production and number of platform for each average
capacity in operation, oil and gas ratio was calculated for each year, weighted by
number of platforms in operation. Therefore, annual natural gas production was
reached. To arrive at platform net production, energy auto-consumption and energy
penalty related to membrane system were discounted from gross production. Auto-
consumption was considered constant over time and equal for all average platform
capacities.
Thus, for each CO2 content and for each platform capacity considered, the
required modules number, volumes captured in membrane, reinjected volumes
(i.e., CO2 captured and bypass) and pre-salt natural gas volumes produced, were
possible to be calculated.
Results
Pre-salt Natural Gas Production
Natural gas gross production projections by typology of platform are presented in
Tables 45.2 and 45.3, separated by respective CO2 content in gross natural gas. CO2 Content: 10% mol of CO2 (Table 45.4).
Table 45.1 Estimated compressor’s powers on the membrane capture
Compressor power (MW)
CO2 content: 10% CO2 content: 45%
100 kbpd 150 kbpd 200 kbpd 100 kbpd 150 kbpd 200 kbpd
4.62 9.24 9.24 11.14 22.28 22.28
Table 45.2 Consumption/energy penalty of membranes (compressors)
Year
CO2 content: 10% CO2 content: 45%
Electric consumption (GWh)
Gas consumption (Mm3)
Electric consumption (GWh)
Gas consumption (Mm3)
2010 40.47 12.38 97.59 29.85
2015 323.77 99.02 780.69 238.77
2020 526.13 160.91 1268.62 388.00
2025 849.90 259.93 2049.31 626.76
2030 1254.61 383.71 3025.18 925.22
2035 1659.32 507.49 4001.04 1223.68
2040 1861.68 569.37 4488.97 1372.91
2045 1821.20 557.00 4391.39 1343.06
2050 1618.85 495.11 3903.46 1193.83
624 I.V.L. da Costa et al.
Thus, auto-consumption and energy penalty were deducted from natural
gas gross production, resulting in a new projection curve of natural gas net
production. A CO2 content range mentioned above—10% mol of CO2 and 45%
mol of CO2—for pre-salt was considered, so, a natural gas net production range was
estimated.
Membrane area calculated by HYSYS model was 32,000 m2. Below, Table 45.5
presents extracted gas estimates, gross and net natural gas production for pre-salt
contents of 10 and 45% mol of CO2. Figure 45.2 shows the same results.
Table 45.3 Production and reinjection volumes of natural gas with content of 10% mol of CO2
Average capacity platform (k bpd)
Extracted gas (M m3/ day)
Membrane modules
Bypass (M m3/ day)
Natural gas gross production (M m3/day)
100 4.0 1 1 2.73
150 6.0 2 0 5.46
200 8.0 2 2 5.46
Average capacity platform (k bpd)
Reinjection (M m3/day)
CO2 content in reinjected gas
CO2 capture on membrane (kt/day)
Capture tax
% (tCO2/ bbl)
100 1.37 26% 0.66 89% 0.0066
150 0.74 70% 0.95 86% 0.0064
200 2.74 26% 1.31 89% 0.0066
CO2 content: 45% mol of CO2
Table 45.4 Production and reinjection volumes of natural gas with content of 45% mol of CO2
Average capacity platform (k bpd)
Extracted gas (M m3/ day)
Membrane modules Bypass (Mm3/day)
Natural gas gross production (M m3/day)
100 4.0 1 1 1.82
150 6.0 2 0 3.64
200 8.0 2 2 3.64
Average capacity platform (k bpd)
Reinjection (M m3/day)
CO2 content on reinjected gas
CO2 Capture on membrane (kt/day)
Capture tax
% (tCO2/ bbl)
100 2.28 75% 3.15 96% 0.0315
150 2.56 95% 4.48 91% 0.0299
200 4.56 75% 6.30 96% 0.0315
45 Geo.: Gas Production in Offshore Reservoirs in Brazil’s Pre-salt Region 625
Concluding Remarks
CO2 content in reinjected gas is higher for 150 thousand bpd platforms. Its
production volume coincides with capacity from two membrane modules, so it
became possible to treat all extracted gas. In other words, there is no bypass, which
would dilute CO2 in reinjected gas and reduce hydrocarbon production. For 100 and
200 thousand bpd platforms there is a gas quantity, which is rich in natural gas that
cannot be treated by membranes. Therefore, it is reinjected back into the reservoir.
This wasted natural gas decreases the reinjected gas CO2 content. For 45% mol of
CO2 gas, 95% CO2 content in reinjected gas has been reached, which is configured
as a very pure gas, justifying the membrane area calculated.
Regarding the capture taxes, when they are compared, it can be seen that
150 thousand bpd platform has a lower tax than the 100 and 200 thousand bpd.
Table 45.5 Pre-salt natural gas production (10 and 45% mol of CO2)
Year
10% mol CO2 45% mol CO2
Extracted gas (Mm3)
Gross production (M m3)
Net production (M m3)
Extracted gas (Mm3)
Gross production (M m3)
Net production (M m3)
2010 1460 428 283 1460 286 123
2015 11,680 6994 4724 11,680 4663 2252
2020 18,250 11,569 7914 18,250 7713 3830
2025 27,010 19,117 13,481 27,010 12,744 6,742
2030 37,960 28,790 20,692 37,960 19,194 10,554
2035 48,910 38,534 27,992 48,910 25,689 14,431
2040 56,210 43,654 31,585 56,210 29,103 16,230
2045 54,750 44,409 32,441 54,750 29,606 16,852
2050 48,180 38,980 28,672 48,180 25,987 14,980
Fig. 45.2 Pre-salt natural gas production (10 and 45% mol of CO2)
626 I.V.L. da Costa et al.
This difference can be explained due to the passage through the membrane of all
extracted gas from the well. Once in gas separation process there is a small CO2 loss, capture tax of 150 thousand bpd platform is penalized. At the same time,
because the other platforms have a volume of bypass, they directly reinjected the
CO2 volume from bypass, without any loss, which increases the capture tax.
As regards the capture, it occurs more efficiently in 45% mol of CO2 gross
natural gas, naturally because of the increased presence of CO2 in extracted gas.
Therefore, there is both a greater CO2 capture in membrane system, as a larger
amount of carbon dioxide in gross natural gas that does not pass through the
membrane, but is directly reinjected. So, for an extracted gas from pre-salt with
higher CO2 content, natural gas production that would be available for the market
decreases, which can be seen from natural gas production curves estimates. Natural
gas gross production is 50% higher for gas with 10%mol of CO2 content, while net
production (discounting energy penalty and auto-consumption) is approximately
twice as large.
CCS implementation is a way to enable pre-salt exploration, as the associated
natural gas contains large CO2 amounts, estimated here between 10 and 45% mol
of CO2, but can reach higher values. When in contact with water, CO2 can produce
acids that may cause wear on pipes and equipment. It can also reduce natural gas
calorific value and it can favor the formation of hydrates at low temperatures and
high pressures. Thus, if there is no separation of CO2, it impedes natural gas
transportation, and therefore, their commercialization. From CCS implementation
and from separation of the largest portion of CO2 contained in natural gas, natural
gas production becomes technically feasible.
Analysis presented in this study is unprecedented and, therefore, in the absence
of public data, lack of relevant historical pre-salt oil and natural gas production and
complexity of the problem portrayed, many assumptions and hypotheses were
adopted to make the presented simulations. The high degree of uncertainty that
was considered here is clear and, thus, these simulations and their results could be
improved in the future, with new available data.
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45 Geo.: Gas Production in Offshore Reservoirs in Brazil’s Pre-salt Region 629
Part XII
Environmental Technologies Related to Global Warming
Water Resources and Management Issues
Water management issues reflected on specific test cases
Chapter 46
Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara Reservoir in Algeria
Belkheir DJELITA, Souaad Bouzid-Lagha, and Kheira Camellia NEHAR
Introduction
Algeria is one of the countries where water availability is limited while the needs
are growing strongly. This growth is due to the population explosion, the industrial
and agricultural development as well as drought. To address this shortage, dam
construction seems to be the most suitable solution to meet different needs. If these
structures constitute a necessity to ensure, in any season, the water supply essential
for our country, it should control and protect the quality of water dams against
various sources of pollution, particularly those due to human activities, namely
agricultural practices, industrial and urban waste. Note that these discharges loaded
pollutants often lead to the natural environment without any treatment. Added to
this, the soil erosion natural processes are likely to bring different elements that
may be the cause of the deterioration of the water quality. One consequence of this
is the enrichment of water by nutrients, especially phosphorus and nitrogen, indi-
cators of an advanced eutrophication of water status (El-Ghachtoul et al. 2005).
Eutrophication is an increase in the fertilization of the lake water by a contribu-
tion of nutrients favoring their proliferation of phytoplankton and aquatic plants.
Gradually, this process accelerates sedimentation: the lake is shrinking, is closing
and finally disappears (Ramade 1982). This phenomenon was classified in 1997 by
B. DJELITA (*) • S. Bouzid-Lagha Laboratory of Environment, Water, of Geomechanics and Structures (LEEGO),
Faculty of Civil Engeniering (FCE), University of Science and Technology Houari
Boumediene (USTHB), BP 32 El-Allia, Bab-Ezzouar, Algiers 16111, Algeria
e-mail: [email protected]; [email protected]
K.C. NEHAR
University of Zian Achour, Djelfa BP 3117, Algeria
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_46
635
the International Lake Environment Committee (ILEC), the fourth of the six major
risks that may affect the lakes and reservoirs of the planet.
The present study focuses on the dam Hammam Boughrara and aims to establish
a diagnosis of the current trophic state of the lake to contribute to the knowledge of
the evolution of this ecosystem. The first aim of this study is to assess the trophic
status of the dam, including eutrophication seems to be an evolutionary process,
natural, nutrient salts and therefore more and more rich in living organisms and
organic matter. Indeed, the lakes are pitfalls to nutritive substances they are
simultaneously victims. The Second is to determine the influence of water quality,
by its physico-chemical properties, chemical and biological aquatic populations. As
The third, it aims both to establish a better understanding of the quantitative
relationship between the intake of nutrient materials and trophic response of our
dam, the other to determine the impact of morphology, hydrology and physico-
chemical characteristics on the latter.
Materials and Methods
Presentation of the Study Site
Hammam Boughrara Dam, located in the extreme northwest of the Wilaya of
Tlemcen (West Algeria), belongs to the watershed area of river Mouillah, whose
area (largely shared with Morocco) is 2000 km2. This basin is bounded by a
perimeter of 241 km and composed in its majority by Angad Plains (located in
Oujda Moroccan territory) and that of Zrigua (located in Maghnia Algerian terri-
tory). The length of its main trough is 104.4 km (Fig. 46.1).
The study area is characterized by a semi-arid climate with mild winter, where
the average annual rainfall is 325 mm, the average annual temperature is 18.5 �C and potential evapotranspiration of 1167 mm. Monthly liquid intake is highly
variable with maximum averages in November (6.29 hm3) and lowest in June
(0.88 hm3). Solid contributions are also variable, the highest values are observed
in March with 0.15 MT and the lowest in July with 0.003 MT. From a geomorpho-
logical point of view, the catchment area of the river Mouillah is characterized by
an elongated shape (k¼ 1.5), an index of overall slope Ig¼ 7.5% and a concentra- tion time Tc¼ 12 h, which means speeds low, favoring the settling of solids in streams. Therefore, the runoff reaches the watershed outlet, low in suspended
solids.
On the geological basin, a terrain succession from Paleozoic to Quaternary has
been identified. The ancient land, dominated by carbonate formations (limestones
and dolomites very cracked and karstified) and sandstone are the reliefs. The
depressions are covered with soft terrain represented by clays, gypsum marl,
alluvium and silt.
636 B. DJELITA et al.
Built at the confluence of oueds Tafna and Mouillah the dam Hammam
Boughrara is intended mainly to meet the drinking water supply needs (AEP) of
cities of Oran (33 hm3) and Maghnia (17 hm3) ; 09 hm3 are provided for irrigation.
It is characterized by a total capacity of 177 hm3, volume 59 hm3 regularized and a
dead volume of 23.30 hm3. The area of the lake is 984 ha. Liquid intake of Wadi
Mouillah to the barrier Hammam Boughrara, as measured by the National Agency
for Water Resources (ANRH) during the 1999–2008 period an average of 79% of
the total intake. The rest is provided by its tributaries. As for the operation of the
dam, monitoring was conducted during the 1999–2008 period. The main results are
shown in the following table (Table 46.1).
They testify to a renewal rates (or dilution) Water (D¼Q/V) relatively small, rarely exceeding unity. Using the formula (D¼ 1/Ts) largely confirmed these results by order of values 0.39<D< 1.14 y�1. With Q: flow in m3/y; V: lake volume in m3. Ts values: mean residence time of the water in the dam (yr), are
shown in Table 46.2.
Fig. 46.1 Situation of the watershed of Oued Mouilah
46 Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara. . . 637
T a b le
4 6 .1
S it u at io n o f D am
H am
m am
B o u g h ra ra
in o p er at io n (1 9 9 9 – 2 0 0 8 )
Y ea rs
P lu v io m et ry
(m m )
T ri b u ta ry
(h m
3 )
C o n so m m at io n -A
E P (h m
3 )
Ir ri g at io n
(h m
3 )
L ac h er
V .F O N D
L ea k
(h m
3 )
E v ap o ra ti o n
(h m
3 )
D ef fl u en t
(h m
3 )
O ra n
M ag h n ia
O ra n
M ag h n ia
1 9 9 9 – 2 0 0 0
2 1 5 .0
1 1 .5 9 3
– –
8 .9 5 8
– 0 .0 1 0
3 .6 6 3
1 2 .6 1 2
2 0 0 0 – 2 0 0 1
2 3 8 .6
3 6 .6 5 1
8 .8 8 8
– 9 .6 2 6
– 0 .0 1 4
4 .6 8 1
2 3 .2 0 8
2 0 0 1 – 2 0 0 2
3 0 8 .6
4 3 .9 1 7
3 9 .7 5
– 9 .2 7 3
0 .3 2 4
0 .0 3 0
4 .5 6 9
5 3 .9 4 6
2 0 0 2 – 2 0 0 3
2 9 3 .6
3 8 .1 5
3 1 .9 8
– 1 .9 1 6
0 .0 2 7
0 .0 3 6
4 .1 7 3
3 8 .1 3 2
2 0 0 3 – 2 0 0 4
3 4 6 .6
4 8 .3 7 1
3 9 .3 7 8
– 4 .4 0 9
0 .3 6 0
0 .0 3 6
3 .8 6 3
4 8 .0 1 1
2 0 0 4 – 2 0 0 5
2 2 9 .3
1 5 .2 0 2
6 .0 4 4
0 .3 4 2
– 1 .0 2 3
0 .0 3 6
3 .4 4 1
1 2 .1 9 6
2 0 0 5 – 2 0 0 6
1 8 9 .6
3 8 .4 4 9
6 .9 0 9
7 .0 0 8
– 0 .5 4 0
0 .0 3 6
5 .0 9 3
1 9 .6 4 3
2 0 0 6 – 2 0 0 7
2 5 3 .0
3 2 .3 2 5
1 .9 9 2
6 .4 9 0
– 0 .3 4 3
0 .0 4 5
6 .2 5 2
1 5 .1 2 2
2 0 0 7 – 2 0 0 8
2 0 3 .0
3 0 .1 2
4 .4 6 5
3 .2 1 0
– 0 .0 8 7
0 .0 2 6
3 .8 3 4
1 6 .4 2 2
S o u rc e:
N at io n al
A g en cy
fo r D am
s an d T ra n sf er s (A
N B T )
638 B. DJELITA et al.
Sources of Pollution
Domestic pollution
Generally, this pollution is from discharges domestic waste water of all cities and
towns, located in the algerian part of the basin, namely the communes of Maghnia,
Bougherara Hammam, Sidi Medjahed and Bouhlou. A wastewater treatment plant,
with a total capacity of 150,000 population equivalents, was performed to treat
wastewater from the city of Maghnia. after several tests conducted from June 1999
to January 2000, the station has gradually achieved acceptable results.
Industrial pollution
Industrial effluents comes from four companies:
The ENOF: Company nonferrous minerals and useful substances. It produces
bleaching earth and bentonite foundry and used as raw materials: clay, and calcium
carbonate (CaCO3), and as secondary material: 98% sulfuric acid (H2SO4) and
sodium carbonate (Na2CO3). It rejects 500 m 3/day of water containing suspended
particles of clay, metal and heavy metals. All of these releases are in the wadi
Ouerdifou.
The ENCG: fatty substances Complex. It produces oil, soap and glycerin. It uses
as raw material: crude oil, animal and vegetable fats, and as secondary materials:
sodium hydroxide (NaOH), phosphoric acid (H3PO4), sodium chloride (NaCl) and
ferric chloride (FeCl3). The ENCG rejects 528 m 3/day of water containing crude
oils, tallow and glycerin. Releases are in the wadi Abbes (tributary of the wadi
Ouerdifou).
The ERIAD: Company food and derivatives industries. The unit produces
products derived from corn. It uses as raw materials corn, and secondary materials
Table 46.2 Results of the application of Eqs. (46.1) and (46.2) of dam Hammam Boughrara
N� (1) (2) (3) (4) (5) (6) Years Z (m) A0 (m
2) TS (yr) Lt(P) (t yr �1) Ld(P) (t yr�1) L. entré (t yr�1)
1999 10.6 2,538,983 2.32 0.37 0.49 6.34
2000 14.0 3,803,621 1.45 0.75 1.11 33.05
2001 15.3 4,097,382 1.52 0.82 1.23 14.21
2002 13.5 3,645,454 2.48 0.56 0.76 6.85
2003 12.6 3,397,891 1.18 0.70 1.06 21.73
2004 12.0 3,137,695 0.87 0.75 1.18 32.62
2005 11.0 2,813,500 1.19 0.54 0.80 35.89
2006 14.5 3,893,022 1.52 0.76 1.13 43.94
2007 18.8 4,790,995 2.57 0.83 1.18 31.42
Source of parameters Z, A0, Ts: ANRH & ANBT
46 Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara. . . 639
such as: sulfur water at 0.2% (SO2), hydrochloric acid (HCl), sodium carbonate and
sodium bisulfite. It rejects 600 m3/day of water containing gluten in Wadi Abbes.
TheECVO: ceramic tableware company. It uses as rawmaterials: clay, kaolin, sand,
water, calcite, dolomite, gypsum, mineral dyes and feldspars. It rejects 130 m3/day
of highly contaminated water with minerals in the wadi Abbes.
Agricultural pollution
Agricultural activities in the studied watershed are located mainly in the irrigated
area of Maghnia and especially in the plain of Angad.
The major sources of pollution from these activities are: fertilizer application,
soil treatment and plant well as livestock, especially poultry. Added to this, a
potential source of pollution that can cause serious damage to health and the
environment, in this case, storage of obsolete pesticides and maintenance of
agricultural machinery (drain) well as fuel and lubricants
Pollution from the Moroccan side
This pollution is caused by urban and industrial wastewater from the Moroccan
town of Oujda, discharged directly into the Oued Bounaim, the main tributary of the
Oued Mouillah, without any treatment.
Data and Methods
Faced with the problem of eutrophication, assessment of water quality requires
knowledge, as complete as possible, physicochemical and biological water. To this
end, nineteen (19) parameters (temperature, pH, conductivity, Ca, Mg, Na, K, Cl,
SO4, HCO3, NO2, NO3, PO4, Ptot, O2dissous, NH4, TSS, BOD5, COD) and biotic
parameters (chlorophyll a, phytoplankton) were selected.
Monthly samples were taken at the surface, at a station located in the tower
measures water intake dam over a period from 1999 to 2008. The samples used for
assays of chemical parameters and chlorophyll (a) have been achieved through a
bottle of overturning 2 L capacity. Various methods of analysis were used (Rodier
et al. 2005). Thus, the temperature, the salinity and the pH were measured by a
standard field probe WTW Multiline P3 PH/LF-SET. Dissolved oxygen was mea-
sured by the chemical method of Winkler. Chemical parameters, Ca, Mg, Na, K, Cl,
HCO3, NO3, NO2, NH4, PO4, and Ptot were analyzed by colorimetric methods using
a spectrophotometer. The gravimetric method was used for the determination of
SO4. Chlorophyll (a) was measured by the fluorimetric method described by
Neveux (1976). The analyzes were performed in the laboratories of the ANRH.
The results were the fundamental database for this study.
640 B. DJELITA et al.
Results and Interpretations
Study of Physicochemical and Biotic Parameters
The graphical representation of different results and reading of changes in physical
and chemical parameters (temperature, conductivity, Ph, Ca, Mg, Na, K, Cl, SO4,
HCO3, NO2, NO3, NH4, PO4, Ptot, O2dissous, TSS, BOD5, COD) imposes the
following comments:
– the monthly temperatures range between 10 and 12.5 �C in winter and between 25 and 31 �C in summer. The annual average is around 18.5 �C.
– the electrical conductivity fluctuates between 977 and 2750 μs/cm and indicates a highly mineralized water. This high mineralization would be due, firstly, to
leaching of the crossed fields and, secondly, to the pollution of waters from
industrial, domestic and agricultural.
– the pH measured varying between 7.5 and 9.1, indicating low to moderately
alkaline water. the value of 9.1 recorded in September 2004 coincided with high
photosynthetic activity.
Graphical representations and interpretations of concentrations of dissolved
oxygen (O2), suspended solids (TSS) and biochemical and chemical oxygen
demand (BOD5, COD), are as follows (Fig. 46.2):
– The Summer dissolved oxygen levels, ranging from 1.3 to 23 mg/L and is
abnormally proportional to temperature. This could be due, firstly, to the intense
photosynthetic activity, on the other hand, to the exchange of oxygen between
air and water, as our sampling station is located on the surface.
– The values of TSS, below 75 mg/L, show that the dam water is of acceptable
quality, with the exception of those of June 2002 and April 2004 (200 and
175 mg/L) due to major floods.
– The BOD5 is generally greater than 15 mg/L. These high values correspond to
high organic load mainly from the food industry. As to the DCO concentrations
vary between 19 and 110 mg/L. High values are associated with an increase in
Fig. 46.2 Monthly evolution of dissolved oxygen, TSS, BOD5 and COD (1999–2008)
46 Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara. . . 641
the amount of organic material and the oxidizable substances. The BOD5/COD
ratio of between 0.2 and 0.6 indicates the possibility of a biological treatment.
– Total phosphorus contents (Ptot), much higher than 0.5 mg/L (Standard ANRH)
indicate mediocre water quality at extremely polluted. They are due on the one
hand, for industrial discharges including those containing detergents, secondly,
to the phosphate fertilizers used in agriculture. It should be noted that the values
of phosphate (PO4) are consistent with those of total phosphorus and are always
less, with an average value of 2.37 mg/L. This confirms the excessive pollution
of water studied (Fig. 46.3).
– The concentrations of ammoniacal nitrogen (NH4) are the highest recorded in
January 2004, February 2005, April 2005, May 2005 and February 2006. They
are 12.2, respectively; 13.3; 14.8; 11.35 and 11.9 mg/L.
Concentrations of nitrite (NO2) vary between 0.01 and 4.5 mg/L.
These high values are due to industrial waste (ERIAD, corn mill and ENCG).
The values of nitrate (NO3) fluctuate between 1 and 15 mg/L (Fig. 46.4).
As to major cations and anions, we can see that:
– Values of chloride (Cl) showed a significant difference between the month and
vary between 213 and 510 mg/L. which ranks our water in Class 6 characterized
Fig. 46.3 Monthly variation in concentrations of total phosphorus and phosphates (1999–2008)
Fig. 46.4 Monthly variation in concentrations of ammonia Nitrogen, Nitrites and Nitrates (1999–2008)
642 B. DJELITA et al.
by specific water more or less polluted. Their presence is exclusively related to
discharges of ENCG (soap Workshop) dominated by sodium chloride (NaCl),
used to activate saponification.
– The average concentrations of sulphates (SO4) recorded is 155 mg/L and proves
that these waters are heavily polluted or very selenitic. This is due to the increase
in sulfur waste urban waste and especially industrial (ENOF unit with sulfuric
acid rejection of 98%).
– Bicarbonates range from 127 to 487 mg/L. They are due to the predominance of
limestone in the watershed.
– The calcium contents (Ca) sometimes exceed 100 mg/L, which may be related to
discharges of ENOF and the predominance of limestone in our site.
– Sodium values (Na) fluctuate between 113 and 416 mg/L. High levels recorded
in the summer, would be mainly due to the scarcity of precipitation combined
with increased evaporation.
– The potassium concentration (K) generally vary between 10 and 21 mg/L with
peaks of up to 32 mg/L. They result from the contributions of groundwater and
runoff. The concentration of magnesium (Mg) vary between 35 and 109 mg/L.
– The Values of chlorophyll “a” vary between 0.5 and 23.8 mg/L. The lowest
recorded concentrations may be due to the decrease of the water temperature and
the reduction of the light intensity. Those recorded in the summer would likely
due to high levels of suspended solids that increase the turbidity of the medium
and reduce, thus the photosynthetic activity. It should be noted, however, that
these values are unusually low for the season. The peak values recorded are due
to the elevation of the algal activity stimulated by environmental enrichment in
nutrients including phosphorus and nitrogen.
Modelisation of Water Plane
In studies of eutrophication, a multitude of models have been developed and
applied to various problems. We will concentrate on models of reservoir lakes.
This is justified by the fact that these models are used for two distinct purposes, but
closely related. They can, on one hand, help in the understanding of the processes
that further determine the overall behavior of the lake and on the other hand, used to
predict the response of the lake at a given change, such as a change in the burden of
nutrients or liquids contributions. Thus, they are a very useful tool for the evalua-
tion of eutrophication and planning and water resources management.
We considered the two main approaches to modeling (Riley 1946):
• The empirical approach: In empirical models (development of an equation from
statistical correlations of data), system variables are related to the input variables
without the detailed mechanisms that cause their relationships are known. The
relationship between trophic status, average depth of the lake and phosphorus
load, developed by Vollenweider (1968), is an example of this type of model.
46 Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara. . . 643
• Conceptual approach: conceptual models (development of an expression on
theoretical grounds and its subsequent combination with constants derived
data) attempt to explain the interactions between different components of the
system. As an example of simple models in this category include nutrient
balance models, such as phosphorus, also developed by Vollenweider (1975,
1976a, b). The model gives a differential equation for the average concentrations
of nutrients, based on a number of input parameters and the lake. In practice, the
two approaches, empirical and conceptual, are usually combined.
Based on these considerations and in order to proceed to the modeling of the
water dam Hammam Boughrara, we followed the following steps:
Estimate of Tolerable and Dangerous Loads of Phosphorus
Concentration in the Dam Hammam Boughrara According
Vollenweider
The equation of Vollenweider (1976b) permits to determine if phosphorus loading
constitutes a risk of eutrophication, since the charges “tolerable” and “dangerous” a
water body are set at 10 and 20 μg P/L, these loads are represented by the following equations:
Lt Pð Þ ¼ A0 100þ 10Z TS
� � ð46:1Þ
Ld Pð Þ ¼ A0 100þ 20Z TS
� � ð46:2Þ
Where: Lt(P)¼ tolerable loads; Ld(P)¼ dangerous loads; A0: the area of the tank (m2); TS: the mean residence time of the water in the tank (year); The entered. :
Estimated annual phosphorus load into our dam (t/year); Z: the average depth of the
container (m).
It should be noted that:
A0: was determined from the curve “height- capacity -surface” of the dam,
established by ANBT collaboration with the research department FUGRO GEOID
SAS-LEM (Laboratory for Maritime Studies), Algiers.
TS¼V/Q¼ lake volume (m3)/flow at the outlet (m3 an�1) The results of the application of these equations waters Boughrara dam are
shown in the following table (Table 46.2).
The values of tolerable and dangerous loads calculated using the equation
Vollenweider (1976b) (Table 2) show that the quantity of phosphorus in the dam
is 9–45 times greater than the load “dangerous” set by this equation when these
values were recorded in 2002 and 2005 respectively. The dam would therefore have
the characteristics of a hyper-eutrophic lake.
644 B. DJELITA et al.
It is emphasized that the application of these equations is not very reliable,
knowing they have been established according to water bodies located in temperate
zones at different trophic states; and that the dam studied (Hammam Boughrara) is
located in a Mediterranean climate zone and receives too loaded water nutrient
urban and industrial original features.
Simple Model of the Phosphorus Cycle (Vollenweider Model)
Vollenweider (1975, 1976a) has developed its models on the conceptual basis that
the concentration of phosphorus in lakes, although largely determined by the rate of
contributions is modified by losses to the sediments and in the flow of lake. Hence
the new formula Vollenweider (1976a):
P ¼ Lp qs
1þ ffiffiffiffiffiTspð Þ ð46:3Þ
Where Ts¼ l/Γw, is the average residence time of water (yr). Γw : annual frequency of renewal (yr�1).
The OCDE Model, 1982
This model represents the equation (3) after being perfected on the base of the
results of the international OCDE study (1982) and is expressed as follows:
P½ �λ ¼ 1:55 P½ �j
1þ ffiffiffiffiffiTspð Þ � �0:82
ð46:4Þ
Where: P½ �λ: average annual concentration of total phosphorus in the lake (μg/L); P½ �j ¼ Lpqs : average concentration of phosphorus in annual water intake (μg/L).
Application of Models in the Dam of Hammam Boughrara
The data are based on the results of analyzes made during the period from 1999 to
2007 by the services of the ANRH (Table 46.3).
The results of the application of Eqs. (46.3) and (46.4) obtained from the data of
Table 46.3 are summarized in Table 46.4.
The application of models, Vollenweider and OCDE, for the various annual
loads gave values close and near each other, but below the actual measured
concentrations.
46 Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara. . . 645
T a b le
4 6 .3
R ec ap it u la ti o n o f d at a (1 9 9 9 – 2 0 0 7 )
1 9 9 9
2 0 0 0
2 0 0 1
2 0 0 2
2 0 0 3
2 0 0 4
2 0 0 5
2 0 0 6
2 0 0 7
L : to ta l an n u al
in ta k e o f p h o sp h o ru s (t o n n es )
6 .3 4
3 3 .0 5
1 4 .2 1
6 .8 5
2 1 .7 3
3 2 .6 2
3 5 .8 9
4 3 .9 4
3 1 .4 2
A v er ag e v o lu m e o f th e re se rv e (h m
3 )
2 3 .3 3
4 0 .5 5
4 5 .3 2
3 8 .1 6
3 5 .1 2
3 1 .4 9
2 7 .2 4
4 2 .0 1
2 3 .3 3
S u rf ac e w at er
(1 0 6 m
2 )
2 .5 4
3 .8 0
4 .1 0
3 .6 5
3 .4 0
3 .1 4
2 .8 1
3 .8 9
2 .5 4
L iq u id
an n u al
in ta k e (h m
3 )
1 1 .5 9
3 6 .6 5
4 1 .2 5
1 9 .8 5
3 6 .1 4
4 3 .2 8
2 5 .9 7
3 7 .0 8
3 5 .1 1
Z : av er ag e d ep th
o f th e d am
(m )
1 0 .6 0
1 4 .0 0
1 5 .3 0
1 3 .5 0
1 2 .6 0
1 2 .0 0
1 1 .0 0
1 4 .5 0
1 8 .8 0
T s: R es id en ce
ti m e
2 .3 2
1 .4 5
1 .5 2
2 .4 8
1 .1 8
0 .8 7
1 .1 9
1 .5 2
2 .5 7
q s: A n n u al
w at er
lo ad
p er
u n it ar ea
4 .5 7
9 .6 4
1 0 .0 7
5 .4 4
1 0 .6 3
1 3 .7 9
9 .2 3
9 .5 3
7 .3 3
L p : an n u al
ch ar g e o f P p er
u n it ar ea
2 4 9 5 .7
8 6 8 8 .3
3 4 6 9 .2
1 8 7 9 .3
6 3 9 6 .4
1 0 3 ,9 6 .9
1 2 7 ,5 5 .4
1 1 2 ,8 5 .7
6 5 5 7 .1
C o as t in
m N G A
(N at io n al
G eo sp at ia l- In te ll ig en ce
A g en cy )
2 7 7 .7 5
2 8 3 .2 6
2 8 4 .4 7
2 8 2 .6 2
2 8 1 .7 6
2 8 0 .6 4
2 7 9 .2 1
2 8 3 .6 4
2 8 7 .9 5
S o u rc e:
A N R H &
A N B T
646 B. DJELITA et al.
The difference between the values calculated by these models and the measured
values could be several explanations for namely:
– the hypotheses of the models suggest that the lake is a homogeneous reactor,
there are no differences in concentrations in the water column. However,
differences exist of concentration in the same column of water especially at
the bottom. This is due to release of phosphorus at the sediment-water interface.
These hypotheses therefore become difficult to apply to the dam studied.
– One of the conditions for the application of the two models assume constant
inputs of phosphorus during the year. The observed irregular contributions do
not verify this hypothesis.
– The difference in high phosphorus concentration would be anthropogenic. Urban
and industrial waste undergoes primary treatment that degrades the organic
materials and leave the water containing phosphorus.
Adaptation of the OCDE Model for Estimating Phosphorus
Concentrations Dam Hammam Boughrara
The differences in phosphorus concentrations observed between the calculated and
measured values can’t be just a consequence of regional climate character (Medi- terranean), it is appropriate to add the effect of human activity. Thus has established
itself the adaptation of the model in question the reality of the waters of the dam
studied. For this purpose we used a non-linear estimation method Rosenbrock and
Quasi Newton, resolvable by “STATISTICA 6.1” software.
Remember that the OCDE equation is of the form:
Y ¼ a*Xb ð46:5Þ
knowing that: Y ¼ P½ �y; X ¼ P½ �J1þ ffiffiffiffiTSpð Þ � �
Table 46.4 Results of models application of Vollenweider (1976a) and of OCDE (1982)
Year Y ¼ P½ �y (μg/L) P ¼
Lp qsð Þ
1 þ√ T sð Þ (μg/L)
P½ �λ ¼ 1, 55 P½ �j
1 þ√ T sð Þ � �0,82
(μg/L) 1999 2186.3 216.59 127.51
2000 3606.6 408.85 214.69
2001 1378.3 154.33 96.57
2002 1380.8 134.08 86.05
2003 2405.8 287.99 161.07
2004 3015.0 389.97 206.53
2005 5528.3 660.70 318.22
2006 4739.1 530.40 265.77
2007 3579.1 343.93 186.31
46 Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara. . . 647
We will try to find again the coefficients a and b, based on the measured values.
The derived equation is of the form:
P½ �λ ¼ 1, 48*X1,28 ð46:6Þ
This equation permits to determine the values of concentration, average annual
total phosphorus in the dam, from the average total phosphorus loads.
The results obtained are shown in column (3) of the following table (Table 46.5).
The majority of the points are within the confidence interval of 95% with a
correlation coefficient R2¼ 0.87, which shows that the model fits correctly (Fig. 46.5).
Table 46.5 Results of the application of Eq. (46.6) Dam
Hammam Boughrara
N� (1) (2) (3)
Years
Y ¼ P½ �y (μg/L)
X ¼ P½ �J 1þ ffiffiffiffiTSpð Þ
� � P½ �λ ¼ 1, 48*X1,28
1999 2186.36 216.59 1489.75
2000 3606.67 408.85 3371.86
2001 1378.33 154.33 963.58
2002 1380.83 134.08 804.14
2003 2405.83 287.99 2148.84
2004 3015.00 389.97 3172.96
2005 5528.33 660.70 6249.58
2006 4739.17 530.40 4711.90
2007 3579.17 343.93 2699.69
Fig. 46.5 Relationship between the intake and the Phosphorus [from Eq. (46.6)] at the dam Hammam Boughrara
648 B. DJELITA et al.
The regression line, indicating the relationship of observed values based on
theoretical values calculated by the equation (7) shows good linear fit as most
points fall within the confidence interval of 95% (Fig. 46.6).
Qualitative Predictions
The management of dam requires the mastery of water quality forecasting system.
The open simple classification system is based on the probabilistic method, it
allows to define five categories namely: ultra-oligotrophic, oligotrophic, mesotro-
phic, eutrophic and hyper-eutrophic.
This classification was developed from a large database of more than a hundred
of water qualities and different trophic states (OCDE 1982). This system allows to
state a prediction closer to the reality that facilitates the evaluation and management
of eutrophication.
Figures 46.7, 46.8 and 46.9 illustrate the classification system and the recovery
of values to different thresholds obtained by projection, concentration values of the
different curves of trophic states then the probabilistic condition, in order to have
the percentage of each trophic state.
The parameters presented in the following table (Table 46.6) characterize the
probabilistic trophic status of the dam Hammam Boughrara. They are based on the
figures of distribution of trophic states.
Fig. 46.6 The regression line Eq. (46.6), indicating the relationship between the observed and predicted values of the mean concentration phosphorus water dam Hammam Boughrara
46 Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara. . . 649
From the open classification system based on the charts of the OECD (1982) and
according to the results of the models Vollenweider and OECD applied to our lake,
the probabilistic trophic status usually varies from eutrophic to hyper eutrophic.
Otherwise, the results of appropriate equations show a state 100% hyper eutrophic.
0
0,5
1,0
1 10 100 1000
Oligotrophie Méstrophie Eutrophie HypereutrophieUlta- oligotrophie
Phosphore total
[P] μg/l
Fig. 46.7 Trophic state distribution function of the total average concentration of phosphorus dam Hammam Boughrara (according Vollenweider 1976a)
0
0,5
1,0
1 10 100 1000
Oligotrophie Méstrophie Eutrophie Hypereutrophie Ulta- oligotrophie
Phosphore total
[P] μg/l
Fig. 46.8 Distribution of trophic states based on the total average concentration of phosphorus dam Hammam Boughrara (based on OCDE 1982)
650 B. DJELITA et al.
Conclusion
The study of physico-chemical and biological characteristics of water collected in
the dam Hammam Boughrara reveals high concentrations of certain parameters
such as Cl, SO4, NH4, NO2, Na, P, BOD5 and COD, which characterize water
highly mineralized and selenitic with conductivities ranging from 977 to 2750 μs/ cm. These waters are rich in nutrients, such as phosphorus, and with a slightly
alkaline pH (between 7.5 and 9.1) favor the proliferation of phytoplankton. This
proliferation causes a decrease in transparency and dissolved oxygen are also signs
of eutrophication. However, the BOD5/COD ratio, ranging between 0.2 and 0.6,
indicating the possibility of a biological treatment. The observed concentrations
of K, Mg, HCO3 result of a contribution by groundwater and leaching of carbonate
terrains. The knowledge of the trophic status of a dam is not enough. To protect it,
we must be able to predict the one hand, changing its state department overlooked
time changes in phosphorus concentrations and their impacts on the ecosystem, on
the other hand, better manage discards based on water use.
Thus, the application of models Vollenweider and OCDE annual loads to
different phosphorus, gave close but lower than actual concentrations estimates.
These models cannot be applied as such to our site, especially as climate and
anthropogenic conditions on which these models are not verified in our case.
Therefore, we adapted the parameters a and b of equation : Y ¼ a∗Xb (OCDE 1982) and in our case, by using the non-linear estimation method Rosenbrock and
Quasi Newton. The regression line obtained using the above mentioned equation,
equipped with the new parameters a and b, shows good fit all the points with
0
0,5
1,0
1 10 100 1000
Oligotrophie Méstrophie Eutrophie Hypereutrophie Ulta- oligotrophie
Phosphore total
[P] μg/l
Fig. 46.9 Distribution of trophic states based on the total average concentration of phosphorus dam Hammam Boughrara (from Eq. 46.6)
46 Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara. . . 651
T a b le
4 6 .6
P ro b ab il is ti c tr o p h ic
st at es
d am
H am
m am
B o u g h ra ra
w it h in
th e p ar am
et er s o f si m p le
cl as si fi ca ti o n sy st em
Y ea rs
1 9 9 9
2 0 0 0
2 0 0 1
2 0 0 2
2 0 0 3
2 0 0 4
2 0 0 5
2 0 0 6
2 0 0 7
P t (μ g /L ) (V
o ll en w ei d er
1 9 7 6 a)
E q . (4 6 .3 )
% 0 o li g o .
1 m és o .
3 0 eu
6 9 h y p er
0 o li g o
0 m és o
0 9 eu
9 1 h y p er
0 o li g o
4 m és o
5 0 eu
4 6
h y p er
0 o li g o
6 m és o
5 6 eu
3 8
h y p er
0 o li g o
0 m és o
1 8 eu
8 2 h y p er
0 o li g o
0 m és o
1 0 eu
9 0 h y p er
0 o li g o
0 m és o
3 eu
9 7 h y p er
0 o li g o
0 m és o
5 eu
9 5 h y p er
0 o li g o
0 m és o
2 5 eu
7 5 h y p er
P t (μ g /L ) (O
C D E 1 9 8 2 ) E q . (4 6 .4 )
% 0 o li g o
7 m és o
5 8 eu
3 5 h y p er
0 o li g o
1 m és o
3 1 eu
6 8 h y p er
0 o li g o
1 3 m és o
6 4 eu
2 3
h y p er
0 o li g o
1 6 m és o
6 5 eu
1 8
h y p er
0 o li g o
4 m és o
4 8 eu
4 8 h y p er
0 o li g o
1 m és o
3 2 eu
6 7 h y p er
0 o li g o
0 m és o
1 5 eu
8 5 h y p er
0 o li g o
0 m és o
2 2 eu
7 8 h y p er
0 o li g o
2 m és o
3 9 eu
5 9 h y p er
P t (μ g /L ) E q . (4 6 .6 )
% 0 o li g o
0 m és o
0 eu
1 0 0
h y p er
0 o li g o
0 m és o
0 eu
1 0 0
h y p er
0 o li g o
0 m és o
1 eu 9 9
h y p er
0 o li g o
0 m és o
2 eu 9 8
h y p er
0 o li g o
0 m és o
0 eu
1 0 0
h y p er
0 o li g o
0 m és o
0 eu
1 0 0
h y p er
0 o li g o
0 m és o
0 eu
1 0 0
h y p er
0 o li g o
0 m és o
0 eu
1 0 0
h y p er
0 o li g o
0 m és o
0 eu
1 0 0
h y p er
O li go
o li g o tr o p h ic , m és o m es o tr o p h ic , eu
eu tr o p h ic , hy pe r h y p er -e u tr o p h ic
652 B. DJELITA et al.
correlation coefficient R2 equal to 0.87. The model thus obtained gives concentra-
tions near the measured values. However, it would be interesting to test it on a
longer observation period. The trophic status of the studied waters varies from
eutrophic to hyper-eutrophic according to the models of Vollenweider and OECD.
While the classification according to the adapted models is 100% hyper eutrophic
for phosphorus.
The probabilistic model obtained will contribute to better management of water
quality in terms of trophic response. It allows to set specific goals for reducing
phosphorus inputs depending on the intended use of the waters. Thus, it can be used
in the context of sustainable development and decision support.
References
Agence Nationale des Ressources Hydriques (ANRH). (2008). Bulletins mensuels de la qualité des eaux superficielles. Algérie: Oran.
El Ghachtoul, Y., Alaoui Mhamidi, M., & Gabi, H. (2005) Eutrophisation des eaux des retenues
des barrages Smir et Sehla (Maroc): Causes, conséquences et consignes de gestion. Revue des sciences de l’eau/Journal of Water Science, 18, 75–89.
ILEC. (1997). Water issue and Global Warming, International Lake Environment Committee
Foundation. http://www.ilec.or.jp/database/Gl.html.
Neveux, J. (1976). Dosage de la chlorophylle a et de la phéophytine a par fluorimétrie. In Annales
Institut Océanographique 52, pp. 165–174. OCDE (Organization for Economic Cooperation and Development). (1982). Eutrophication of
Waters. Monitoring assessment and Control, Final Report. OCDE, Cooperative Programme on
Monitoring of Inland Waters (Eutrophication control), Environment Directorate, OCDE, Paris, France.
Ramade, F. (1982). Elément d’écologie: Ecologie Appliquée. Action de l’homme sur la biosphère. Paris, France: Macgraw-Hill.
Riley, G. A. (1946). Factor controlling phytoplankton populations on Georges Bank. Journal of Marine Research, 6, 54–73.
Rodier, J., et al. (2005). L’analyse de l’eau: eaux naturelles, eaux résiduaires et eau de mer (8th ed.). Paris, France: Dunod.
Vollenweider, R. A. (1968). Scientific fundamentals of the eutrophication of lakes and flowing
waters with particular reference to nitrogen and phosphorus as factors in eutrophication.OECD Technical Report DAS, CSI, 68, 27–54.
Vollenweider, R. A. (1975). Input-output models with special reference to the phosphorus loading
concept in limnology. Schweiz Journal of Hydrology, 3, 53–84. Vollenweider, R. A. (1976a). Advances in defining critical loading levels for phosphorus in
eutrophication. Memorie della Societa Entomologica Italiana, 33, 53–83. Vollenweider, R. A. (1976b). Rotsee, a source, not a sink for phosphorus? A comment to and a plea
for nutrient balance studies. Journal of Hydrology, 38, 29–34.
46 Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara. . . 653
Chapter 47
Natural Tracers for Identifying Causes of the Quality Reduction in Groundwater Emerging Along the Aegean Volcanic Arc (Greece)
E. Dotsika and P. Chantzi
Introduction
The Santorini and Nisyros volcano in Greece located along the Aegean volcanic
arc, which developed during the Quaternary time as a result of a lithosphere
subduction process (Le Pichon and Angelier 1979). The Aegean volcanic arc
comprises, from west to east, Loutraki, Egina, Milos, Santorini, Kos and Nisyros.
In the Aegean Sea, this arc (Fig. 47.1) represents the youngest example of volca-
nism and the only one that can be related to the zone of subduction. The morpho-
logical situation of such a geodynamic setting is found in the south (200 km) of the
arc where the African and Eurasian plate’s collision is in progress (Mckenzie 1970; Lort et al. 1974). The collision takes place from the Pliocene along the south
Aegean island arc and is responsible of volcanism and seism city (Makris 1978).
All the volcanic centers of the south Aegean islands are situated across the Benioff
zone at depth from 130 to 150 km, suggesting that subduction controls magma
generation. Several studies (Papazachos et al. 1995; Jolivet et al. 2013; Chatzipetros
et al. 2013) have shown that tectonic activity is very vigorous in the Aegean region
and all these areas and islands were affected by numerous tectonic events that are
still active.
E. Dotsika (*) Institute of Geosciences and Earth Resources, Via G. Moruzzi 1, 56124 Pisa, Italy
Laboratories of Stable Isotopes and Radiocarbon, Institute of Nanoscience and
Nanotechnology, National Centre for Scientific Research “Demokritos”, 15310 Agia
Paraskevi, Attica, Greece
e-mail: [email protected]
P. Chantzi
Laboratories of Stable Isotopes and Radiocarbon, Institute of Nanoscience and
Nanotechnology, National Centre for Scientific Research “Demokritos”, 15310 Agia
Paraskevi, Attica, Greece
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_47
655
A significant number of thermal water springs emerge in the areas and islands of
the Aegean arc. The temperature of these waters springs ranges from 30 to 53 �C. Also an important number of fresh water springs, with degrading quality, emerge in
the vicinity of hot waters of these islands. These fresh water resources frequently
suffer from severe salinisation problems that put in danger present and future
Fig. 47.1 Study areas of Egina, Milos, Santorini, Kos and Nisyros of the Aegean Volcanic arc
656 E. Dotsika and P. Chantzi
utilization as well economic and social development of the concerned islands. The
origin of this salinisation is very often attributed to the sea water intrusion. In the
islands, marine water might enter the aquifer systems through different pathways
e.g., atmospheric transport of marine aerosols, direct seawater ingression, particu-
larly near the coastal zones, by seawater and modified seawater. However the
vicinity of cold springs with the thermal fields suggests that part of the salinisation
is due to the deep thermal water, coming from geothermal aquifers that intrude in
the fresh aquifers.
The mobile constituent, chloride, is one of the most important geochemical tools
used in the hydro geochemical investigations. The high chloride concentration, in
most groundwater aquifers, in potable and irrigation waters is attributed to evapo-
rative concentration, intrusion of seawater, dissolution of evaporates and human
pollution. Although chloride can be added to deep aquifers by different sources the
mixing processes could be identifiable. Additionally the correlation δ18O-δ2H and mobile specie are particularly useful to investigate the mixing, because they
provide information about the water sources and the different mixing processes
that can operate between the sources. Especially, the δ18O-δ2H isotope composition of groundwater is mainly affected by recharge altitude, water-rock interaction and
mixing of different fluids. Additionally, the use of isotopes of sulphate δ34S, δ18O, consents to identify the origin of the dissolved sulphates and the mixing between
sulphates of different origin. The 13C values of bicarbonates ions in thermal and
fresh waters are used to identify modification processes of equilibration between
water and CO2. The combined use of δ34S, δ18O(SO4), δ18O, δ2H, 13C and Cl� serves as tracers for identifying mixing processes in groundwater system and is used as an
important tool for recognizing the causes of the quality reduction of coastal water
systems.
In this study we used Cl�, HCO3 � and SO4
2� with isotopes of water, carbonate and sulphate to identify the spatial distribution of pollution and its possible origin.
Sampling and Analysis
Seventy-six samples were collected for chemical (Cl�, HCO3 �, SO4
2�) and isoto- pic analyses of water (2H, 18O), carbonate (13C) and sulfate (34S, 18O). The isotopic
composition of water was determined in all collected waters samples while the
isotopic composition of carbonate and sulfate was determined in selected waters
samples. δ13C were also determined in two samples of carbonate rocks and 34S were also measured in three samples of native sulfur from Santorini. Seventy one
samples of water were collected for this study: 3 from Loutraki, 7 from Egina,
21 from Santorini, 19 from Kos, 15 from Milos, 7 from Nisyros and one from sea
water. Temperature and HCO3 � were measured directly in situ. Untreated samples
were collected for analyses of Cl� and SO4 2�. The temperatures of water samples
varied between 16 and 53 �C. Emissions of gases from these waters are abundant in Santorini, Nisyros, Kos and Milos. The major chemical constituents were analyzed
47 Natural Tracers for Identifying Causes of the Quality Reduction. . . 657
with standard methods described in Apha (1989). The anions of the water samples
were analyzed with ion chromatography. The δ18O compositions of water in the samples were determined from CO2 equilibrated with the water (Epstein and May-
eda 1953). The δ2H compositions of water were determined from the H2 generated by the Zn-reduction method (Coleman et al. 1982). The dissolved SO4
2� in the water samples was precipitated as BaSO4 for the analysis of S isotopic composi-
tions (Rafter 1957). The dissolved HCO3 � in the water, for the analysis of 13C, is
collected as BaCO3 precipitates. Determination of the different isotope ratios
carried out in Laboratories of Stable Isotopes and Radiocarbon of Nanoscience
and Nanotechnology Institute in N.C.S.R. in Demokritos with the following preci-
sion: δ2H� 1‰; δ18O� 0.2‰; δ34S� 1‰; δ18O(SO42�)� 0.3‰; δ13C� 0.5‰.
Results and Discussion
The Origin of the Waters and the Sources of the Quality Reduction in Ground Water
The stable isotope contents show quite large variations of δ18O ranging from –7.3‰ to 1.4‰ and δD from –47.4‰ to 6.5‰. The limits of maximum and minimum values were drawn by Nisyros and Loutraki respectively. In general, the water
samples from thermal springs show an isotopic enrichment in relation to the fresh
waters.
The stable isotopic composition (δ2H versus δ18O) of all sampled waters from areas and islands of the Aegean Volcanic arc is shown in Fig. 47.2. At the same
diagram, the global meteoric water line (GMWL) (Craig 1961) is also marked.
Generally, an isotope relationship between δ2H and δ18O with a slope of about 8 is normal for fresh precipitation of all types (Craig 1961), as well as for surface waters
not subjected to excessive evaporation relative to input. In Greece the correlation
function for rainwater (IAEA 1981) is: δD¼ 7.2 * δ18O + 9.3. A regression equation similar to the above and slightly greater (7 and 7.5 respectively) is reported for the
northern part of Eastern Macedonia and for the Eastern Peloponnesus (Leontiadis
et al. 1984). A slope inferior to 7 is reported for Central Macedonia (Christodoulou
et al. 1993), the southern part of Eastern Macedonia and Thrace (Leontiadis
et al. 1996), as well as the northern part of Epirus (Leontiadis and Nikolaou
1999). The local meteoric line that correspond to Greece (LMWL) has a correlation
equation δ2H¼ 8.7δ18O + 19.5 (Dotsika et al. 2009). In Fig. 47.2, two linear correlations appear, apart from the water of mainly
meteoric origin (Loutraki, Egina, Poros), between δ2H and δ18O suggesting a different origin for both elements. Line A, which expresses all the water samples
coming from the islands, is an ideal line mixing between seawater and fresh water,
suggesting that the isotopic data of waters are the result of a mixing at different
degree of meteoric and seawater. This is the case mainly of Santorini Island. The
658 E. Dotsika and P. Chantzi
second line (B) groundwater, from Milos Island, presents an enrichment of δ18O in relation to the δ18O of meteoric waters of the area, while the δ2H remains about stable. This change could suggest the intervention of modification processes. So, for
better identification of the causes of the quality reduction in ground water we study
separately the areas of Santorini, Kos and Nisyros islands, Loutraki-Egina and
Milos Island.
The Case of Santorini, Kos and Nisyros Islands
Figure 47.3 shows the relationship δ2H and δ18O of all the sampled waters from Santorini, Kos and Nisyros islands. The waters from Santorini are distributed along
a line joining local seawater with local fresh water, suggesting that the hot and cold
waters result from a mixing at different degree of meteoric and seawater. These
isotopic data confirm the sea intrusion in fresh aquifers of Santorini Island. In fact in
Santorini a significant number of water boreholes was found, which presented high
Cl� and SO4 2� values. Nevertheless, such brackish waters, with relatively high
temperature, Cl� and SO4 2� contents, are used, in summer for irrigation and
drinking purposes, and could therefore have an antagonistic effect on crop yield
and health.
In the δ18O versus Cl� content (Fig. 47.3) diagram the samples from Santorini located along a straight line, which intercepts the x-axis at the δ18O content of�5.2 ‰. This value corresponds to the mean content of the local meteoric waters as the
Fig. 47.2 The stable isotopic composition (δ2H‰ vs V-SMOW versus δ18O‰ vs V-SMOW) of all sampled waters from Egina, Milos, Santorini, Kos and Nisyros of the Aegean Volcanic arc.
Closed square: Loutraki; : Egina; open triangle: Santorini; open parallelogram: Kos; open diamond: Milos; open square: Nisiros; cross: sea water
47 Natural Tracers for Identifying Causes of the Quality Reduction. . . 659
rainwater samples collected from the area have been found to have similar value for
the δ18O. The position of sample N-Avlaki from Nisyros in the diagram δ2H versus δ18O
(Fig. 47.2) is very close to that of mean seawater, confirming its purely marine
origin. Other samples from Nisyros show very strong meteoric contributions.
Similar positions, in the diagram δ2H versus δ18O, to the one of the N-Avlaki sample show also the water from Kos (Aghios Fokas) suggesting its marine origin
as well. In reverse the δ18O and δ2H contents of the other samples from Kos Island show a meteoric origin for these waters. However the dispersion of some data
suggests intervention of modification processes. Figures 47.4 and 47.5 show the
relationship between δ18O versus SiO2 (Fig. 47.4) and δ2H versus SO42�
(Fig. 47.5). Despite the small number of samples the positive correlation between δ 18O and SiO2 (Fig. 47.4) is of major importance as concerns mainly the samples
which present the major dispersion of δ18O and δ2H. This correlation, δ18O-SiO2, could be explained from the equilibration between water-rock or/and water-CO2 of
deep origin. The augmentation of SiO2 (and probably of HCO3 �) could show the
“aggressiveness” of the water correlated to the partial pressure of CO2. In the
diagram δ2H versus SO42� (Fig. 47.5) the enrichment of δ2H content is accompa- nied by an increase of SO4
2� content. This correlation could be attributed to the equilibration between water and H2S of volcanic origin. Figure 47.2, which sum-
marizes these modification processes, indicates the isotopic change of the fresh
waters due to the modification processes of the equilibration between water and
gases—CO2 and H2S—of deep origin. The isotopic values of the Kos meteoric
water are �6.5‰ and �37‰ for the 18O and 2H respectively. So these two hypotheses, equilibration between H2O-CO2 and H2O-H2S could explain the δ18O and δ2H of all waters sampled in Kos Island (Fig. 47.2). In Fig. 47.2 the lines A and
Fig. 47.3 The relationship between δ18O ‰ vs V-SMOW and Cl� (mg/L) content of Egina, Milos, Santorini, Kos and Nisyros of the Aegean Volcanic arc. Symbols as Fig. 47.2
660 E. Dotsika and P. Chantzi
B show the exchange with H2S and CO2. The intermediate area illustrates the
exchange with both gases, H2S and CO2, of deep origin. The two-δ13C values from the bicarbonate ions in the waters from Kos are �8.4‰ (Aghios Fokas) and 11.9‰ (Fouskis). The very positive δ13C values of bicarbonates ions from Kos (Fouskis) confirm the equilibration between water and CO2 of deep origin.
The negative δ13C data, similarly as data from the Santorini samples (range from �13.7‰ to �8.6‰) probably suggest that the main part of dissolved CO2 is of biogenic origin; even a small contribution of deep CO2 cannot be excluded.
Fig. 47.4 Relationship between δ18O ‰ vs V-SMOW versus SiO2 (mg/L) of Santorini samples. Symbols as Fig. 47.2
Fig. 47.5 Relationship between δ18O ‰ vs V-SMOW versus SO42� (mg/L) of Egina, Milos, Santorini, Kos and Nisyros of the Aegean Volcanic arc. Symbols as Fig. 47.2
47 Natural Tracers for Identifying Causes of the Quality Reduction. . . 661
In Fig. 47.6 the 34S and 18O (SO4) contents of the samples, from Santorini,
Nisyros and Kos, are compared with those of marine sulphate, which are very
constant over the world [δ34S¼ 20‰ CD, δ18Ο¼ 9.5‰ SMOW (Longinelli 1989; Loyd 1968; Rafter and Mizutani 1967, Mizutani and Rafter 1969)]. In the same
diagram, it is also reported the S-bearing sublimate of the Santorini Volcano (Nea
Kameni). In total, ten water samples were analyzed from Santorini and three
samples of native sulfur (δ34S of native sulfur 7.9‰, 5.7‰ and 8.8‰) of the Santorini Volcano, three water samples from Kos, one from Nisyros and one
seawater sample. It appears, in general, that the isotope contents of the samples
are different from those of the marine sulphates. Only one sample from Kos and one
from Nisyros do not differ significantly from those of seawater, suggesting that the
dissolved sulphates of these waters are of purely marine origin. All the Santorini
samples contain sulphate that is depleted in heavy isotopes relative to marine
sulphate. The isotopic data suggest that these sulphates could come from the mixing
between sulphates of marine origin and sulphates, probably, contained in the
volcanic rocks of the island, which have been formed by the oxidation of the
primary sulfur of deep origin. Michaud et al. 2000 has reported the presence of
sulfur in various volcanic products of Santorini. In fact this δ34S depletion was attributed to a mixing of marine sulphate with ‘light’ sulphate (Michelot et al. 1993), deriving from the oxidation of sulphur minerals. This contribution of
sulphur oxidation is confirmed by the decrease of 34S concentration and the increase
of the sulphate contents in the water (Fig. 47.6). The very low δ34S content of the Kos waters is also attributed to oxidation of primary sulfur of deep origin and
defends the condition of existence of strong pressure of H2S of volcanic origin.
Fig. 47.6 Relationship between δ34S ‰ vs CDD versus δ18O (SO4) vs SMOW of Egina, Milos, Santorini, Kos and Nisyros of the Aegean Volcanic arc. Symbols as Fig. 47.2
662 E. Dotsika and P. Chantzi
The Case of Loutraki and Egina Waters
Figure 47.2 shows the relationship between δ2H and δ18O contents of the water of Loutraki and Egina and the range of local meteoric water. The δ2H and δ18O values of Loutraki and Egina waters indicate a negligible contribution of seawater. The
position of these samples in the diagram δ2H versus δ18O confirms their mainly meteoric origin. However in Fig. 47.6 the 34S and 18O(SO4) contents of the Loutraki
samples are compared to those of marine sulphate. It appears that the isotope
contents of the samples do not differ significantly from those of seawater,
suggesting that the dissolved sulphates of these waters are of purely marine origin.
This marine participation is the cause for the augmentation of salinization.
The Case of Milos Waters
The δ2H and δ18O values of Milos’s waters (Fig. 47.2) are shifted to the right of the local meteoric water line.
The isotopic data of Milos’s water show an 18O enrichment with respect to those observed for the local fresh water. In opposite strong meteoric contributions appear
in the 2H contents. These changes could suggest that the stable isotope contents of
Milos’s water are controlled by geothermal exchange. However an exchange between water-rock increases the δ18O, conserving “firm” the Cl� contents. In Fig. 47.3 it is observed a modest enrichment in chloride, probably by mixing with a
solution rich in heavy isotope. So the position of the samples in Fig. 47.3 could be
attributed to the mixing between fresh water and deep thermal waters modified
jointly by water-rock interaction and evaporation. Regardless of the origin of deep
water the modification processes results the quality degradation of waters. The
temperature increase and the salinisation of waters contribute to the unacceptable
values of these waters according to the European standards.
In Fig. 47.6 the 34S and 18O(SO4) contents of Milos’s samples are compared to those of marine sulphate. It appears that the isotope contents of the samples,
especially the Milos samples, differ significantly to those of seawater, suggesting
that the dissolved sulphates of these waters come from oxidation of sulphur
minerals. In fact the contribution of sulphur oxidation is confirmed by the decrease
of 34S concentration and the increase of the sulphate contents in the water.
Conclusions
Interpretation of groundwater geochemical data, including isotopic data of water,
carbonate and sulphates, in terms of mixing and origin of solutes, and therefore
origin of pollution, is often complicated by the non-conservative nature of dissolved
47 Natural Tracers for Identifying Causes of the Quality Reduction. . . 663
components resulting from the mixing with gases, different type of fluid and from
interactions with the aquifer matrix. These fluids are of different origin and, in
particular, in groundwater emerging along the Aegean volcanic arc; result from
actual seawater and water that vary by interactions with the aquifer matrix, by the
exchange with the gases and the geothermal exchange. In the water emerging along
the Aegean volcanic arc, salinisation enrichment is a problem to the quality of the
intensely exploited groundwater, especially during the summer on account of
tourist increase. In general, this salinisation enrichment in coastal areas conjoins
with seawater intrusion. In fact the results of this study indicate that the waters
examined from Loutraki, Egina are essentially of meteoric origin, but some of them
are affected by a slight mixing with seawater. The seawater intrusion is the main
cause for the quality reduction of Nisyros and Santorini Island.
However, the enrichment in HCO3 � and SO4
2� concentrations in groundwater with the parallel increase of water isotopes indicates that the salinisation enrich-
ment in Kos Island is due to the intrusion of gases in the Island aquifers. Therefore
the salinisation enrichment in coastal areas in Kos Island is due to the modifications
processes of equilibration water- gases, CO2 and H2S, of deep origin.
The salinisation enrichment in groundwater in Milos, does not derive from a
contamination source, but is due to mixing between local fresh water and deep
water. In Milos Island the salinisation is controlled probably by mixing of fresh
water with a solution rich in heavy isotope and geothermal exchange. In both cases
the deuterium isotopes are applied in investigations on the origin of the salinisation
in groundwater and the use of δ2H is proved to be an effective approach for understanding the origin of quality reduction in geothermal areas.
In summary, for the water emerging along the Aegean volcanic arc, the
salinisation enrichment is due to sea intrusion, exchange with gas, geothermal
exchange and mixing of fresh water with a deep solution rich in heavy isotope.
References
Apha. (1989). Standard methods for the examination of water and wastewater (19th ed.). Washington, DC: American Public Health Association.
Christodoulou, T., Leontiadis, I. L., Morfis, A., Payne, B. R., & Tzimourtas, S. (1993). Isotope
hydrology study of Axios River plain in northern Greece. Journal of Hydrology, 146, 391–404. Chatzipetros, A., Kiratzi, A., Sboras, S., Zouros, N., & Pavlides, S. (2013). Active faulting in the
north-eastern Aegean Sea Islands. Tectonophysics, 597–598(19), 106–122. Coleman, M. L., Shepard, T. J., Durham, J. J., Rouse, J. E., & Moore, G. R. (1982). Reduction of
water with zinc for hydrogen analysis. Analytical Chemistry, 54, 993–995. Craig, H. (1961). Isotopic variations in meteoric waters. Science, 133, 1702–1703. Dotsika, E., Lykoudis, S., & Poutoukis, D. (2009). Spatial distribution of the isotopic composition
of precipitation and spring water in Greece. Global and Planetary Change, 71, 141–149. Epstein, S., & Mayeda, T. (1953). Variation of 18O content of waters from natural sources.
Geochimica et Cosmochimica Acta, 4(5), 213–224. International Atomic Energy Agency (IAEA). (1981). Statistical treatment of environmental
isotope data in precipitation. IAEA Tech. Rep. Ser. No. 206. Vienna: IAEA.
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Jolivet, L., Faccenna, C., Huet, B., Labrousse, L., Pourhiet, L., Lacombe, O., et al. (2013). Aegean
tectonics: Strain localisation, slab tearing and trench retreat. Tectonophysics, 597–598(19), 1–33.
Leontiadis, I., Payne, B. R., Letsios, A., Papagianni, N., Kakarelis, D., & Chadjiagonakis,
D. (1984). Isotope hydrology study of Kato Nevrokopi of drama. In Proc. of the symposium on isotope hydrology 1983 (pp. 193–206). Vienna: International Atomic Energy Agency.
Leontiadis, I. L., Vergis, S., & Christodoulou, T. (1996). Isotope hydrology study of areas in
Eastern Macedonia and Trace, Northern Greece. Journal of Hydrology, 182, 1–17. Leontiadis, I. L., & Nikolaou, E. (1999). Environmental isotopes in determining groundwater flow
systems, northern part of Epirus, Greece. Hydrogeology Journal, 7, 219–226. Le Pichon, X., & Angelier, J. (1979). The hellenic arc and trench systems a key to the neotectonic
evolution of the eastern Mediterranean area. Tectonophysics, 60, 1–42. Longinelli, A. (1989). Oxygen-18 and Sulphur-34 in dissolved oceanic sulphate and phosphate. In
P. Fritz & J. C. Fontes (Eds.), Handbook of environmental isotope geochemistry (Vol. 3, pp. 219–255). Amsterdam: Elsevier. Chapter 7.
Loyd, R. M. (1968). Oxygen isotope behaviour in the sulfate-water system. Journal of Geophys- ical Research, 73, 6099–6110.
Lort, J. M., Limond, W. Q., & Gray, F. (1974). Preliminary seismic studies in the eastern
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Tectonophysics, 46, 269–284. McKenzie, D. (1970). Plate tectonics of the Mediterranean region. Nature, 226, 269–284. Michaud, V., Clocchiatti, R., & Sbrana, S. (2000). The Minoan and post-Minoan eruptions,
Santorini (Greece), in the light of melt inclusions: Chlorine and sulphur behaviour. Journal of Volcanology and Geothermal Research, 99(1–4), 195–214.
Michelot, J. L., Dotsika, E., & Fytikas, M. (1993). A hydro chemical and isotopic study of thermal
waters on Lesbos Island (Greece). Geothermics, 22(2), 91–99. Mizutani, H., & Rafter, T. A. (1969). Oxygen isotopic composition of sulfates: 3. Oxygen isotopic
fractionation in the disulfate-water system. New Zealand Journal of Science, 12, 54–59. Papazachos, C., Hatzidimitriou, P., Panagiotopoulos, D., & Tsokas, G. (1995). Tomography of the
crust and upper mantle in southeast Europe. Journal of Geophysical Research, 100, 12405–12422.
Rafter, T. A. (1957). Sulphur isotopic variations in nature: Part 1. The preparation of sulphur
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Rafter, T. A., & Mizutani, H. (1967). Oxygen isotopic composition of sulfates: 2. Preliminary
results on oxygen isotopic variation in sulphates and relationship of the environment and to
their δ34S values. New Zealand Journal of Science, 10, 816.
47 Natural Tracers for Identifying Causes of the Quality Reduction. . . 665
Chapter 48
Experimental Study of Longitudinal Dispersion on Trapezoidal Open Channel
Ali Mansour Lagoun and Salim Benziada
Introduction
Water demand does not cease to increase, especially with demography growth,
industry and agricultural development. Global warming and climate changing has
affected directly water resources, rains becomes rare and several areas
becomes arid.
Water, this vital source, that it becomes today very precious, is affected by
pollution, and providing water with quantity and quality is becoming very difficult
and expensive. Governments have to make all procedures to preserve this source
of life.
Pollution in shallow water resources and river is often punctual (Gerhard et al.
2005), when pollutants discharged in streams, is subjected to several processes of
mixing and transportation, a lot of scientists are interesting today to grow knowl-
edge of its mechanisms and to develop models for studying phenomenon of
pollutants transport and predicting its evolution in space and time, to develop
helpful decision tools.
A.M. Lagoun (*) Research Laboratory of Water Sciences, Polytechnic National School of Algiers, Algiers,
Algeria
Laboratory of Environment, Water, Geomechanics and Structures, Faculty of Civil
Engineering (FGC), University of Sciences & Technology Houari Boumediene (USTHB),
Bab Ezzouar, Algiers, Algeria
Scientific and Technical Research Center on Physical and Chemical Analyses, Bou-Ismail,
Tipaza, Algeria
e-mail: [email protected]
S. Benziada
Research Laboratory of Water Sciences, Polytechnic National School of Algiers, Algiers,
Algeria
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_48
667
Researches at this field are in situ (at rivers and streams), at reduced physical
models or mathematical and numerical developments, at this manuscript, we have
conceived an experimental device with trapezoidal open channel, that is the most
responded, usual and similar at rivers, a lot of experimentation was applied by
changing hydrodynamical parameters of flow to determine its effects and under-
standing the phenomenon of contaminations dispersion.
Phenomenon of Transport in Rivers
When any substance is injected in flow, a cloud with high concentration forms, this
cloud occupies a wide area at moving and concentrations become lower. Moving of
substance injected in flow and decreasing in concentration are effected by several
processes such as: diffusion, advection, dispersion (Fischer 1966; Shen et al. 1995;
Gharbi 1998; Hibbs et al. 1999; Czernuszenko et al. 2005; Steve et al. 2005).
Experimental Setup
Experimental setup consists essentially of feed tank, a trapezoidal channel, an
injection device and sampling and collecting systems.
Installation was conceived, and experiments were performed at Research Lab-
oratory of water Sciences (LRS eau) in Polytechnic National School of Algiers with
the aim to measure concentration profiles of contaminant (phenol) at downstream
stations resulting due different injections scenario of phenol in the upstream of
channel.
Figures 48.1 and 48.2 shows equipment of experimental setup, characteristics of
flume are presented in Table 48.1.
Measurement Tools
Discharge Measurement: Discharge measurement was made with V notch weir, after weir calibration, Discharge is given as function of head flow with:
Q ¼ 1, 35:hd5=2 ð48:1Þ
Concentration Measurement: Phenol concentration was measured by Spectropho- tometer, after calibration of phenol, concentration is given as function of optical
densities by:
C ¼ 80 D0 ð48:2Þ
668 A.M. Lagoun and S. Benziada
Feed tank
Support
V Notch Weir
Channel support
Injection system
Flow Stabilizer
Fig. 48.1 3D schema of experimental setup
Fig. 48.2 Photography of experimental setup (LRS. Eau, ENP)
Table 48.1 Summary of flume characteristics
Designation Parameters Values
Channel Form Trapezoidal
Bed slope [%] 5
Lench [m] 10,4
Bottom Width [m] 0,4
Side Slope [�] 60 Slope head [cm] 50
Weir Form Triangular (V notch)
Notch angle [�] 90 Crest elevation [cm] 10
48 Experimental Study of Longitudinal Dispersion on Trapezoidal Open Channel 669
Experimental Procedure
Discharge flow is regulated at upstream by valve and controlled and measured at
downstream by triangular weir.
The water was supplied to the flume through overhead tank with constant water
level in order to have a constant discharge of flow; Flume was market at every 1 m
length.
Once flow is stabilized by passing of water through a flow stabilizer at upstream,
injections of phenol for 30 s with three values of concentration (C0¼ 500, C0¼ 1000 and C0¼ 1500 mg/l) were applied at upstream.
Experimental measurements of water head was made, and samples from every
1 m length of flume was taken at surface of water for different scenario of injection
and a several flow values (Q¼ 0.52; Q¼ 0.78, Q¼ 1.6, Q¼ 1.75 and Q¼ 1.95 l/s). Samples were immediately analyzed at laboratory and concentrations were
determined.
Hydraulic Study of Fume Flow
Reynolds number: is given as: (Lencastre 2005).
Re ¼ UDh ν
ð48:3Þ
Flow regimes are classified according Reynolds number as follows: Re < 2000: laminar flow, 2000<Re< 4000: transient flow, Re > 4000 : turbulent flow (Lencastre 2005).
Froude Number: is given by:
Fr ¼ Uffiffiffiffiffiffiffiffiffiffiffi g� hp ð48:4Þ
Flow regimes are classified according Froude number as follows: Fr > 1 : super- critical flow, Fr < 1 : subcritical flow, Fr ¼ 1 : critical flow (Lencastre 2005) (Table 48.2).
Table 48.2 Flow regimes
Q [l/s] U [m/s] Re Fr Flow regimes
0.52 0.008 2848.03 0.006 Subcritical and transient
0.79 0.011 4220.03 0.009 Subcritical and turbulent
1.60 0.019 8144.88 0.015 Subcritical and turbulent
1.75 0.021 8830.58 0.016 Subcritical and turbulent
1.95 0.023 9754.51 0.017 Subcritical and turbulent
670 A.M. Lagoun and S. Benziada
Results and Discussion
Concentration Profiles of Longitudinal Dispersion
Concentration profiles of phenol for every 1 m of flume length at the surface of
water are shown at Figs. 48.3 and 48.4 (for Q¼ 0.79 l/s and Q¼ 1.75 l/s). (Instantaneous injection of phenol for 30 s):
Discussion
• Concentration peaks obtained (Figs. 48.3 and 48.4) are very smaller than initial
concentrations injected, this considerable decrease is mainly due to dilution phenomenon that occurs just after discharging pollutant at water flow.
16 14 12 10
8 6 4 2 0C
o n
ce n
tr at
io n
(m g
/l )
Time (s)
0 100 200 300 400 500
x=1m x=2m x=3m x=4m x=5m x=6m x=7m x=8m
Fig. 48.3 Concentration profiles of phenol for Q¼ 0.79 l/s and C0¼ 500 mg/l
16 14 12 10
8 6 4 2 0C
o n
ce n
tr at
io n
(m g
/l )
Time (s) 0 100 200 300 400
x=1m x=2m x=3m x=4m x=5m x=6m x=7m x=8m
Fig. 48.4 Concentration profiles of phenol for Q¼ 1.75 l/s et C0¼ 1000 mg/l
48 Experimental Study of Longitudinal Dispersion on Trapezoidal Open Channel 671
• In the Vicinity of injection area, concentrations profiles are pointed and sharp. At
the downstream direction, profiles bearing are becoming much more important
and profiles takes the Gaussian form with decrease in concentrations.
This is explained by the predominance of advection in the vicinity of the injection area, away from the pollutant discharge point, the transportation becomes diffusive.
Flow Discharge Influence
Figures 48.5 and 48.6 show a comparison of phenol concentration profiles for
different discharge flow. We note that for all initial phenol concentration injected
(C0):
• Concentrations obtained are much more important for low flow rates.
• Stays time of pollutant is more important for low flow rates.
Fig. 48.5 Concentration profiles of phenol for
different flow discharges at
x¼ 2 m C0¼ 1000 mg/l
Fig. 48.6 Concentration profiles of phenol for
different flow discharges at
x¼ 1 m, C0¼ 500 mg/l
672 A.M. Lagoun and S. Benziada
For determination of flow rates and stays times of pollutants on dispersion
longitudinal phenomenon, we analyze concentration peaks according discharge
flows and distances length at downstream.
Concentration Peaks According Discharge Flow
Concentration peaks as a function of discharge flow are presented in Figs. 48.7 and
48.8.
Peaks obtained are lower for important flow; this is due to the dilution rate that increases with flow discharge.
Longitudinal evolution of concentration peaks for different flow:
Discussion
By analyzing Figs. 48.9 and 48.10, we observe that decreasing of concentration peaks
is much more important for flow rate Q¼ 0.52 l/s, this is effect of stays time that it is
Fig. 48.7 Concentration peaks as function of
discharge flow for
C0¼ 500 mg/l for different distances x
Fig. 48.8 Concentration peaks as function of
discharge flow for
C0¼ 500 mg/l for different distances x
48 Experimental Study of Longitudinal Dispersion on Trapezoidal Open Channel 673
more important for this flow discharge, dispersion have had more time to
manifest, contrary to the case of flow with Q¼ 1.95 l/s when predominance was for advection.
Conclusion
Qualitative study of concentration profiles obtained experimentally, allowed to the
good understanding of dispersion longitudinal phenomenon, and to identify mech-
anisms that govern it.
For instantaneous injection of pollutant case, the analysis of the spatiotemporal
evolution of concentration of phenol at flume has identified two areas:
• An advection area, near the injection where profiles obtained are pointed; the pollutant transport is convective.
• A diffusive area, in the far field, where the concentration profiles bearing become important and the pollutant transport begin to be increasingly diffusive.
Fig. 48.9 Evolution of concentration peaks at
flume for different flows.
C0¼ 1500 mg/l
Fig. 48.10 Evolution of concentration peaks at
flume for different flows.
C0¼ 500 mg/l
674 A.M. Lagoun and S. Benziada
The quantitative study and the comparison between the results for different
injection scenarios shows that the transport phenomenon is related to the flow
rate, since its influence on the properties of the flow that transports the pollutant:
• The average velocity of flow, therefore the advection processes. Increased
discharge results in higher velocity and pollutant transport becomes more
convective.
• The residence (stays) time is more important for low flows (low velocity), so the
decreasing rate of longitudinal dispersion concentration will be higher.
• Dilution rate, which it is function as flow rate.
Nomenclature
C Pollutant Concentration, mg/l
Dh Hydraulic diameter, m Do Optical density
g Gravity, m/s2
h Hydraulic depth, m
hd Head, m
Q Flow discharge (m3/s)
U Flow velocity (m/s)
Dimensionless Numbers
Fr Froude number
Re Reynolds number
Greek Letters
ν Cinematic viscosity of water, m2/s
References
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in open channels . InWater quality hazards and dispersion of pollutants (pp. 35–54). Library of Congress Cataloging-in-Publication Data. New York: Springer.
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Shen, H. T., Yapa, P. D., & Zhang, B. Z. (1995). A simulation model for chemical spills in the
upper St Lawrence River. Journal of Great Lakes Research, 21(10), 652–664. Steve, W., & Russell, M. (2005). On the theoretical prediction of longitudinal dispersion coeffi-
cients in a compound channel. In Water quality hazards and dispersion of pollutants (pp. 69–84). Library of Congress Cataloging-in-Publication Data. New York: Springer.
676 A.M. Lagoun and S. Benziada
Chapter 49
Mygdonia Basin (N. Greece) in the View of Isotope Geochemistry
P. Chantzi and E. Dotsika
Introduction
Mygdonia basin located 10 km N-E to Thessaloniki in northern Greece and it is
consisted by two sub-basins: Koroneia and Volvi lakes. Both lakes constitute an
important wetland which is being protected by International Ramsar Convention.
Mygdonia basin constitutes an elongated EW tectonic depression which combined
with adjusted minor basins (Zagliveri, Marathousa, Doubia) are the remains of an
initial basin called Promygdonia (Koufos et al. 1993). The initial basin was formed
by tectonic activity probably in the late Paleogene to early Neogene. In late
Neogene and early Pleistocene a set of river and lake surface sediments deposited
in this basin. A new tectonic activity at the end of the period “early-Pleistocene”
resulted to many faults of Promygdonia basin were several smaller basins formed
(Mygdonia, Zagliveri, Marathousa, Doubia). Among them the largest was
Mygdonia basin forming the Mygdonia Lake which gradually drained during the
medium-Pleistocene. Sedimentation continued in this basin mainly by lacustrine
deposits (Psilovikos 1977; Sotiriadis et al. 1983). Koronia and Volvi lakes are the remnants of the initial Mygdonia Lake.
P. Chantzi (*) Laboratories of Stable Isotopes and Radiocarbon, Institute of Nanoscience and
Nanotechnology, National Centre for Scientific Research “Demokritos”, 15310 Agia
Paraskevi, Attica, Greece
e-mail: [email protected]
E. Dotsika
Laboratories of Stable Isotopes and Radiocarbon, Institute of Nanoscience and
Nanotechnology, National Centre for Scientific Research “Demokritos”, 15310 Agia
Paraskevi, Attica, Greece
Institute of Geosciences and Earth Resources, Via G. Moruzzi 1, 56124 Pisa, Italy
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_49
677
Mygdonia basin is bended in metamorphic layers from Serbomacedonian massif
(paleozoic gneisses, amphibolites, schists, marbles and granitic intrusions) with
groundwater circulating in metamorphic rocks and discharging in loose formations
in basin. Moreover it covers a basin about 2026 km2 where the terrestrial part covers
about 656 km2 and particularly extends west of Koronia Lake. The basin is defined
by the mountains of Volvi (627 m) and the lower vertices of Vertiskos mountain
(1103 m) in the north, in the east by the mountains of Psili Rachi (341 m) and
Soulgianodiou (746 m) which are interposed between the mountains Kerdylion and
Stratoniko and through the Strait of Rendina communicates with Strymoniko Bay
and in the south side by Chortiatis mountain (1206 m) the lower vertices of
Cholomontas (1165 m) and Stratoniko (918 m) with S-E direction. West boundaries
of basin are not well defined as there are a set of low hills and depressions except
Camila Mountain (569 m). The annual precipitation in the basin ranges
283–721 mm in the last 30 years. The climate varies from Mediterranean and
continental. For the entire basin the average annual temperature is estimated
about 13.55 �C and an average annual precipitation about 584.9 mm (Vatseris 1992).
Both Koroneia and Volvi subcatchments have been undergone sever environ-
mental and human impacts resulting their ecological death (Nimfopulos, M. K.
et al., 2002). An attempt was made in order to fingerprint the isotopic signature of
groundwater in order to strengthen the knowledge on the hydrology regime of
Mygdonia basin. Cold water samples from boreholes were collected from
Mygdonia basin for stable isotope analyses of δ18O, δ2H, δ13C which was performed in Laboratories of Stable Isotopes and Radiocarbon at NCSR
“Demokritos”. The network of boreholes that were sampled corresponded to
shallow (30–60 m) and moderate deep water circulation (60–100 m). The sampling
took place in June 2014 where the boreholes were operated for at least one month
resulting in the water sample to correspond to the actual groundwater body.
Moreover two water samples from lakes Koroneia and Volvi were taken however
that wasn’t possible for fresh spring water as no such springs were detected (Fig. 49.1).
Results and Discussion
Oxygen δ18O and δ2H Isotopes
The values of stable isotopes ranging from �10.3‰ to �7.3‰ and �70.4‰ to �45.7‰ for δ18O and δD. In more detail on the sub-basin of Lake Koronia the isotope values of water molecules vary from �9.0‰ to �7.5‰ (range 1.5‰) and from �59.2‰ to �45.7‰ (range 13.5‰) for δ18O and δD respectively, while on the sub-basin of Lake Volvi values vary from �10.3‰ to �7.3‰ (range 3‰) and from �70.4‰ to �47.2‰ (range 23.2‰) for δ18O and δD respectively. These
678 P. Chantzi and E. Dotsika
values are shown in diagram δ2H‰V-SMOW versus δ18O‰V-SMOW (Fig. 49.2) where global meteoric water line (GMWL, Craig 1961) and local meteoric water
line (LMWL) for Greece as proposed by Dotsika et al. (2010) are pictured as well.
The correlation equation of groundwater for Mygdonia basin is:
δD ¼ 7:8∗δ18Oþ 10:30 ð49:1Þ
Groundwater in Mygdonia basin presents an excellent correlation. Moreover
Koronia is grouped with groundwater in the south part of Volvi sub-basin, sites
where the network of boreholes is strong, supporting the hydraulic communication
(Fig. 49.3).
The correlation equation of groundwater for Koronia and Volvi sub-basins are:
δD ¼ 7:1∗δ18Oþ 4:11 ð49:2Þ δD ¼ 7:8∗δ18Oþ 10:95 ð49:3Þ
The correlation equations of Mygdonia, Koronia and Volvi basins present slopes
«7.8», «7.8» and «7.1» respectively. For Central Macedonia a slope inferior to 7 is
reported (Christodoulou et al., 1993) while for East Macedonia is reported slightly
greater «7.5» (Leontiadis et al., 1984). Generally fresh precipitation of all types and
surface water that have not undergone evaporation exhibit slopes between 7–8
(Craig 1961), while waters that have undergone secondary evaporation exhibit
Fig. 49.1 Study area of Mygdonia basin with Koronia and Volvi sub-basins (Google earth modified picture)
49 Mygdonia Basin (N. Greece) in the View of Isotope Geochemistry 679
Fig. 49.3 δ2H‰ V-SMOW versus δ18O‰ V-SMOW of cold groundwater in Koronia and Volvi sub-basins
Fig. 49.2 δ2H‰ V-SMOW versus δ18O‰ V-SMOW of cold groundwater in Mygdonia basin
680 P. Chantzi and E. Dotsika
lower slopes about «6» (Gat 1980). Therefore it is concluded that groundwater of
Mygdonia basin doesn’t present any evaporation or mixing episodes with different isotopic water.
Both oxygen and deuterium isotopic values are characterized by homogeneity
without significant fluctuations implying that no isotopic exchange with the geo-
logical environment takes place. This conclusion is in agreement with geological
regime of the basin where groundwaters circulate in metamorphic rocks and
discharge in loose formations in basin without presenting long retention time in
groundwater aquifers.
The correlation between sub-basins and surface water of the corresponding lake
is pictured in Fig. 49.4 with the following equations:
δD ¼ 5:9∗δ18O� 5:2 ð49:4Þ δD ¼ 6:3∗δ18O� 3:9 ð49:5Þ
The slopes of lines (49.4) and (49.5) with values «5.9» and «6.3» for the Koronia
and Volvi respectively reflect evaporation processes occurring in surface reservoirs
with Koronia exhibiting a higher rate. In both sub-basins groundwater and surface
lake water correlates excellent however the linking trend is evident in Volvi
catchment implying their direct hydraulic communication but in Koronia catchment
surface lake water placed slightly away from the corresponding trend-line. Isotopic
Fig. 49.4 δ2H‰ V-SMOW versus δ18O‰ V-SMOW of cold groundwater and surface water in Koronia and Volvi sub-basins
49 Mygdonia Basin (N. Greece) in the View of Isotope Geochemistry 681
values are strongly influenced by temperature and the evaporation processes but
also by the humidity (Fritz and Fontes 1980). Therefore this slightly deviation could
be attributed to the humidity above lake water layers. These observations possible
imply the communication of surface water with groundwater in Koronia basin
through lateral shallow formations as the lacustrine bottom is covered by a clay
layer that makes it impermeable
Carbon Isotopes δ13C
The values of carbon isotopes δ13C can detect the different origins of organic or inorganic carbon. The value of carbon in marine carbonate rocks is around 0‰, the soil CO2 around �25‰ (similar to that of plants) and about �7‰ for atmospheric CO2. However, carbonates evaporation may exhibits higher values about þ10‰. The carbon isotopic ratio of fresh water is strongly affected by carbonate mineral
dissolution in the case of carbonate bicarbonate aquifers: CaCO3þH2CO3!Ca2þ þ 2HCO3� (Dotsika 2015). In temperate climate the contribution of dissolved carbonates (δ13C¼�2‰ to þ1‰, Clark and Fritz, 1997) resulting groundwater δ 13C values about �11‰ (Jin et al. 2009) however in shallow aquifers soil CO2 and atmospheric CO2 (water-rock interaction product) contribute to the values forma-
tion resulting aquifers with δ13C values between �11‰ and �22‰ (Jin et al. 2009). Carbon isotope values δ13C range between �13.6‰ and �10.2‰ for Mygdonia basin. In greater detail range from �13.6‰ to �10.2‰ and from �13.2‰ to �10.4‰ for Koronia and Volvi groundwater respectively, reflecting both the dissolution of carbonate rocks and the participation of organic carbon from
soils.
Conclusions
Stable isotope values of cold water samples ranged from �10.3‰ to �7.3‰, from �70.4‰ to �45.7‰ and from �13.6‰ to �10.2‰ for δ18O, δD and δ13C respectively reflecting the isotopic signature of local precipitation water. In the
entirely basin subsurface water circulation exhibits short retention time influenced
by the strong network of irrigation wells without taking place any isotopic exchange
with the geological environment. Mechanism of neither evaporation nor mixing
with waters of different isotopic origin was detected. Dissolution of carbonate rocks
and the participation of CO2 from soils taking place through the circulation of
groundwater to the shallow and middle shallow aquifers.
682 P. Chantzi and E. Dotsika
References
Christodoulou, Th., Leontiadis, I.L., Morfis, A., Payne, B.R., Tzimourtas, S., 1993: Isotope
hydrology study of Axios River plain in northern Greece. J. Hydrol. 146, 391–404.
Clark, I. D., & Fritz, P. (1997). Environmental isotopes in hydrogeology. Boca Raton, FL: Lewis Publishers.
Craig, H. (1961). Isotopic variations in meteoric waters. Science, 133, 1702–1703. Dotsika, E., Lykoudis, S., & Poutoukis, D. (2010). Spatial distribution of the isotopic composition
of precipitation and spring water in Greece. Global and Planetary Change, 71, 141–149. Dotsika, E. (2015, March). H–O–C–S isotope and geochemical assessment of the geothermal area
of Central Greece. Journal of Geochemical Exploration, 150, 1–15. Fritz, P., & Fontes, J. (1980). Handbook of environmentai lsotope geochemistry. New York:
Elsevier.
Gat, J. R. (1980). Isotope hydrology of very saline lakes. In A. Nissenbaum (Ed.), Developments in sedimentology (Vol. 28, pp. 1–7). New York: Elsevier. Chapter 1.
Jin, L., Ogrinc, N., Hamilton, S., Szramek, K., Kanduc, T., & Walter, L. (2009, June). Inorganic
carbon isotope systematics in soil profiles undergoing silicate and carbonate weathering
(Southern Michigan, USA). Chemical Geology, 264(1–4), 139–153. ISSN: 0009-2541. Koufos, G., Syridis, G., Kostopoulos, D., & Koliadimou, K. (1993). Preliminary results about the
stratigraphy and the palaeoenvironment of Mygdonia Basin, Macedonia, Greece. In Proceed- ings of the 1st congress of paleontological association, Geobios.
Leontiadis, I., Payne, B.R., Letsios, A., Papagianni, N., Kakarelis, D., Chadjiagonakis, D., 1984:
Isotope Hydrology study of Kato Nevrokopi of Drama. Proc. Of the Symposium on Isotope
Hydrology 1983. International Atomic Energy Agency, Vienna, pp. 193–206.
Nimfopulos, M. K., Mylopoulos, N., & Katirtzoglou, K. G. (2002). A qualitative-quantitative
study of water and environmental pollution at the broader area of the Mygdonia Basin,
Thessaloniki, Northern Greece. In Proceedings of the 6th Pan-Hellenical geographical con- ference of the Hellenic geographical society, Thessaloniki, 3–6 October 2002 (Vol. II, pp. 436–444).
Psilovikos, A. (1977). Paleogeographic development of the basin and lake of Mygdonia (Lagada—
Volvi area, Greece). Ph.D. thesis, Department of Geology, Aristotle University of Thessaloniki
(in Greek).
Sotiriadis, L., Psilovikos, A., Vavliakis, E., & Syrides, G. (1983). Some tertiary and quaternary
basins of Macedonia/Greece. Formation and evolution, Clausthaler Geologische Abhandlungen (p. 21).
Vatseris, C. (1992). Hydrogeologie des Mygdonias-Beckens (Nord-Griechenland) under
Berucksichtigung der hydrochemischen und isotopen physikalischen komposition der
thermalwasse. Ph.D. thesis, University of Munster, 171p.
49 Mygdonia Basin (N. Greece) in the View of Isotope Geochemistry 683
Chapter 50
Sustainable Management of Sewage Sludge Conditioning and Valorization
S. Igoud, F. Souahi, and C.-E. Chitour
Introduction
Between 1999 and 2010, the Algerian wastewater treatment data showed that the
wastewater volume has doubled. It increased from 600 million m3 to 1.2 billion m3
corresponding to a ratio of 32.34 m3/inhabitant. This has required the building of
105 new wastewater treatment plant (WWTP) and the increase of the wastewater
collection which passed from 79% to 86% (Hammouche 2011). But, in the same
manner, this performance has increased the electricity consumption, the public
spending and the greenhouse gas emission.
The increase of the electricity consumption has been also recorded because the
wastewater treatment uses mainly the activated sewage sludge and the aerated
lagoon processes applied at 67.7% even if they allowed significant remediation
efficiency (Igoud et al. 2014).
This situation has been maintained particularly between 2010 and 2013 with
increases estimated at 35.2% of wastewater volume, 45.8% of electricity con-
sumption and 58% of electricity budget. During 2013, the volume of wastewater
treated by the most important treatment operator: the National Office of Sanitation
(ONA) was estimated at 161 million m3. Its remediation has consumed 21.68 GWh
of electricity for pumping and 60.28 GWh for treatment. Financially, the electricity
cost has been estimated at 2.6 million €. Also, the electricity consumption has emitted 185.61 tons of CO2-eq (Igoud et al. 2014). At 2015, ONA estimated that the
S. Igoud (*) Unité de Développement des Equipements Solaires, UDES/Centre de Développement des
Energies Renouvelables, CDER, 42415 Bou Ismail, W. Tipasa, Algerie
e-mail: [email protected]
F. Souahi • C.-E. Chitour
Ecole Nationale Polytechniques (ENP), Hacène Badi, 16200 El-Harrach, W. Alger, Algerie
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_50
685
total volume of treated wastewater reached 197 millions m3 and its treatment
consumed 97.73 GWh of electricity (ONA 2015).
The development of the wastewater treatment sector which occurred this last
decade will continuous to increase. That because it is planned the systematic
treatment of all collected wastewater and its reuse to irrigate 1 million hectares.
This trend is also projected at the international level. The International Energy
Agency expects that between 2006 and 2030 the energy needs for the wastewater
treatment will increase by 44% (International Energy Agency 2006). This rate will
reach 60% in developing countries (UNESCO-WWAP 2012).
Contributing to reduce the electricity consumption, the aim of the study is to
suggest a sustainable wastewater treatment approach as it is planned by ONA. This
wastewater management was recommended since 2002 in the Johannesburg world
summit (United Nations 2002) to anticipate the significant energy consumption and
GHG emission.
Currently, in order to reduce the electricity consumption, two trends are
prospected: the generation of renewable energy inside the wastewater treatment
plants (WWTP). This requires the use of renewable resources available at the plants
level especially sewage sludge and solar energy. Also, the use of sustainable
treatment processes.
In the study, three proposal of a sustainable sewage sludge treatment are
investigated: the sludge methanization for the cogeneration of electricity and
thermal energy, the solar sludge dryness and the agricultural valorization by land
application in forest areas.
Also, in order to evaluate the electricity and cost saving the sequestration of the
greenhouse gas (GHG) emission, the yearly electricity consumption has been
conducted in an activated sludge wastewater treatment plant.
Methodology
Sewage Sludge Methanization
The energetic bioconversion of sewage sludge requires two steps: the sludge
methanization applied for the biogas production. Then the biogas cogeneration
used for both of electricity and thermal energy production.
The biogas production has been estimated using theoretical and experimental
approaches. The theoretical step consisted on use of Eq. (50.1) as follows:
BV ¼ SSQ:DM:RVM:CC ð50:1Þ
where:
BV: Biomethane volume
SSQ: Sewage Sludge Quantity¼ 3040 tons DM: Dry Matter¼ 65.1 kg/m3 RVM: Removed Volatile Matter¼ 41.23%
686 S. Igoud et al.
Removal biodegradable pollution rate¼ 30% CC: Conversion Coefficient¼ ranging from 0.5 to 0.7 m3 of biomethane/tons of
removed dry volatile matter (Record 2009; Lagrange 1979, 1995).
The experimental study of the biogas production has also been conducted. It has
been experimented using a test bench (Fig. 50.1) composed of four 2 L flat-bottom
flasks.
During the experiments, each flask has been filled by 1 kg sewage sludge
recovered from Tipasa WWTP. The hermetic closure of the flasks allowed the
maintaining of the anaerobic conditions. To ensure the optimum methanization of
sludge, this last has been diluted at 100% of its weight. Then the flasks were tightly
closed and putted on controlled magnetic stirrer hotplates which allowed 37 �C sludge heat and 800 rpm sludge agitation.
The produced biogas has been quantitatively evaluated using gas meters then
stored in plastic bags for its analyze.
The second step evaluated the use of biogas for the cogeneration of electricity
and thermal energy. This estimation used technical characteristics of a 65-kW
biogas microturbine. Its electric efficiency (EE) is fixed at 29% and its thermal
efficiency (TE) at 50% (Product Catalogue 2010). The calculations were performed
as follows:
EG ¼ BV:LCV:EE ð50:2Þ TEG ¼ BV:LCV:TE ð50:3Þ
Fig. 50.1 Test bench of sewage sludge methanization (Igoud 2015)
50 Sustainable Management of Sewage Sludge Conditioning and Valorization 687
where:
EG: Electricity generation (kWh)
BV: Biogas volume (m3)
LCV: Lower calorific value (kWh/m3)
EE: Electric efficiency (%)
TEG: Thermal energy generation (kWh)
TE: Thermal efficiency (%)
Solar Drying of Sewage Sludge
The experiments were conducted in a test bench (Fig. 50.2) according to a protocol
that allowed a comparative study of a direct solar drying using a “drying bed”
prototype. This process is used in several WWTP in Algeria. The second prototype
used a solar greenhouse prototype; this type of sludge treatment is not applied in
Algeria.
The efficiency evaluation of these two drying processes was undertaken using
two types of sludge recovered from the studied WWTP: (1) biological sludge
recovered from the clarifier and containing 99.5% of humidity, (2) thickened
sludge containing 95.5% of humidity which was recovered from the thickener.
During the experiments, a sludge thickness of 2 cm has been maintained on the
drying bed and a volume of 15 L of sludge has been dried. The dryness kinetic has
been estimated through several daily samples. These last were weighed and then
dried at 105 �C for 24 h to be weighed again; this in order to determine their moisture content.
In the studied WWTP, the sludge conditioning consists firstly, on the gravity
thickening step secondary on the mechanical dehydration step using a belt press to
reach finally 24% of moisture.
Fig. 50.2 Test bench of the sewage sludge solar drying (Igoud 2015)
688 S. Igoud et al.
Sewage Sludge Agricultural Valorization
The essay (Ouanouki and Igoud 1993) has been conducted by the planting of forest
young seedlings: Pinus maritima and Acacia cyanophyla in an area of 3672 m2. This last was split into four plots. The first consisted on the witness. And the
remaining plots were planting after the digested sludge spreading as follows:
2 tons of digested sludge (21.76 tons/ha) in the first plot, 8 tons (87.14 tons/ha) in
the second and 15 tons (163.40 tons/ha) in the third.
For the experimentation, 576 young seedlings were planted with an equidistance
of 3 m� 3 m in a staggered rows distribution.
Results and Discussion
During 2010, the yearly electricity consumed in the activated sludge WWTP has
been estimated at 1.25 GWh. The electricity has been consumed at 89.63% by the
wastewater treatment process, 5.77% by the outdoor lighting and 4.6% by the
management department and laboratory (Fig. 50.3).
The electricity has cost 24,766 € and emitted 757.28 tons of CO2-eq with an average of 607.18 g of CO2-eq/kWh.
Renewable Electricity Generated from Sewage Sludge
The theoretical approach of the sewage sludge methanization estimates that
338,103 m3 of biogas could be produced. And its cogeneration could produce
392.78 MWh of electricity and 667.22 MWht of thermal energy recoverable for
the digesters heating.
Fig. 50.3 Yearly electricity consumption in Tipasa WWTP (Igoud et al. 2014)
50 Sustainable Management of Sewage Sludge Conditioning and Valorization 689
This amount of electricity would have to substitute 31.5% of conventional
electricity consumed by Tipasa WWTP. The experimental results have recorded a
lower biogas production (Fig. 50.4). The sludge methanization lasted 45 days and
cumulated a biogas volume of 20.12 L/kg of sludge. The biogas has been charac-
terized by an average methane content of 48%. This totalized a yearly production
of 61.16 103 m3 of biogas whose combustion could cogenerate 106.42 MWh of
electricity and 183.5 MWht of thermal energy.
The conventional electricity saving has been evaluated at 8.5% of the total
WWTP electricity consumption. This result is lower comparatively to the theoret-
ical. This could be induced by the experimental conditions of the sludge
methanization which require to be optimized. It could be also the result of the use
of mature sludge recovered from the storage area rather than fresh one when
available excess.
Sewage Sludge Dryness Induced by Solar Energy
During the trials, the dryness of the biological sludge characterized by 0.5% of
moisture reached 93%. The drying evolution has showed relatively similar kinetics
drying in the bed drying and under the solar greenhouse until 73 h (Fig. 50.5). This
duration is characterized by the evaporation of free water from sludge. From 73 h
which corresponded to the 3rd day of the experimentation, the speed of dehydration
has increased, especially in the drying bed. This is explained by the reduction of the
thickness of the sludge blade which increased their heating temperature. Indeed,
simulations studies performed for different sludge thicknesses showed that the
energy saving, about 20%, is obtained if the sludge thickness is reduced from
20 cm to 10 cm (Slim 2007).
Compared to the drying beds, the drying rate of the solar greenhouse was slower.
This is due to the low moisture wicking saturated air. The openings in the upper part
of the solar greenhouse were not sufficient for the natural wick moisture. For this,
Fig. 50.4 Total biogas production (Igoud 2015)
690 S. Igoud et al.
the optimization and control of the drying parameters would require the use of a
forced air circulation. Indeed, in industrial plants, the evacuation is carried out
through the air extractors to the ambient environment.
The solar drying of the thickened sludge (Fig. 50.6) containing 4.5% of moisture
also reached 93.6% of dryness. This result approaches that obtained after the
biological sludge treatment but this last was obtained during a longer drying time
(100 h against 72 h).
The solar drying of sludge could allow the substitution of the conventional
electricity estimated at 23,630 kWh (Hammouche 2011) required to achieve dry-
ness from 0.5% to 24%. This result corresponds to a saving of 2.1% of the
electricity consumption in the WWTP, 1.90% of the energy budget and 2.1% of
greenhouse gas emissions.
Fig. 50.5 Dryness kinetic of biologic sludge (Igoud 2015)
Fig. 50.6 Dryness kinetic of thickened sludge (Igoud 2015)
50 Sustainable Management of Sewage Sludge Conditioning and Valorization 691
Biomass Production Induced by Sewage Sludge Spreading
The sludge spreading in the plantation showed a positive correlation between the
height plants growth and the digested sludge spreading.
The best results have been obtained in the plot were the high quantity of sludge
was used. In this plot, the increase of the growth rate has been estimated at 71.87%
for pine, 73% for acacia and 68.38% for the mixed plantation using both pine and
acacia. The influence of acacia on pine growth has not shown a positive result. This
has been induced by the short duration of the experimentation which would not
allow the soil enrichment in nitrogen through the acacia nodules (i.e. root outgrowth
involved in the fixation of atmospheric nitrogen).
Conclusion
The obtained results showed the existence real opportunities for the sustainability
management of sewage sludge which benefit to the fossil energy saving and the
environment preservation.
The theoretical bioconversion of sewage sludge evaluated that 392.78 MWh of
electricity and 667.22 MWht of thermal energy could be generated. This amount of
renewable electricity would have to substitute 31.5% of conventional electricity
consumed in the WWTP. However, the experimental assessment allowed a lower
electricity generation which estimated a saving of 8.5%. This result has been
induced by the uncontrolled parameters of the experimentation which need to be
optimized.
Concerning the sewage sludge conditioning in the WWTP it is restricted at 24%
of dryness. This result has been improved by the use of solar drying process. The
obtained results showed the possibility to reach d up 93% dryness. A part this
improvement, the obtained results could allow saving a saving 2.1% of the elec-
tricity consumption in the WWTP, 1.90% of the energy budget and 2.1% of
greenhouse gas emissions. By the improving the dryness from 24% to 93%, the
savings will be most significant. Also, this sustainable treatment reduces the cost of
sludge storage and transport, increases their stabilization, sanitation and deodori-
zation sludge and facilitates energy recovery by burning.
The spreading of digested sewage sludge also has been beneficial for forest
plants growth. It has allowed an increase of the height plants growth which ranged
from 68.33% to 73%. A part this advantage, this kind of valorization should
particularly successes the reforestation undertaken in Algeria since the seventies’ to fight against desertification which threatening all the African countries. This
reforestation policy should be encouraged for the increase of the afforestation rate
which constitutes carbon sinks in fight against climate change.
692 S. Igoud et al.
Acknowledgement The authors would like to thank colleagues and all people who contributed to this studies especially Mrs. Ahmed and Toufik Medjiah from Tipasa’s wastewater treatment plant, Miss Amina Chalal from the Development Unit of Solar Equipment at Bou-Ismaıı̈l.
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microturbine �a biogaz. Capstone. Record. (2009). Record N�07-0226/1A. Techniques de production d’électricité �a partir de biogaz
et de gaz de synthèse.
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50 Sustainable Management of Sewage Sludge Conditioning and Valorization 693
Chapter 51
Photocatalytic Degradation of Tylosin and Spiramycin in Water by Using TiO2 and ZnO Catalysts Under UV Radiation
D. Tassalit, N. Chekir, O. Benhabiles, F. Bentahar, and N.A. Laoufi
Introduction
Some organic substances are either extremely stable or they have �a very slow rate of natural degradation. Pharmaceuticals for example are widely used by humans and
for food production and may react differently and persist in the environment (Sung-
Suh et al. 2004). During their life cycle, they create a new and emerging problem
and significant effects on the human health and ecological risks. For this reason, it’s important to develop a new efficient processes which can deteriorate these recalci-
trant pollutants (Neelavannan and Ahmed Basha 2010; Assabane et al. 2000). The
use of UV or visible light as a source of energy, especially sunlight, to promote
photocatalytic reactions is of great importance (Campion et al. 1999; Turchi and
Ollis 1989). The intensity of solar radiation reaching earth can be an alternative
source used especially in developing countries. Indeed, this renewable energy is
free and inexhaustible; it is the most abundant energy on Earth, especially in
Algeria (Herrmann et al. 2002; Simon and Dauby 2008).
D. Tassalit (*) • N. Chekir Unité de Développement des Equipements Solaires, UDES/Centre de Développement des
Energies Renouvelables, CDER, 42415 Bou Ismail, W. Tipaza, Algeria
Laboratoire des Phénomènes de Transfert, Faculté de Génie Mécanique et de Génie des
Procédes, Université des Sciences et de la Technologie Houari Boumediene (USTHB), Bab-
Ezzouar, 16111 Algiers, Algeria
e-mail: [email protected]
O. Benhabiles
Unité de Développement des Equipements Solaires, UDES/Centre de Développement des
Energies Renouvelables, CDER, 42415 Bou Ismail, W. Tipaza, Algeria
F. Bentahar • N.A. Laoufi
Laboratoire des Phénomènes de Transfert, Faculté de Génie Mécanique et de Génie des
Procédes, Université des Sciences et de la Technologie Houari Boumediene (USTHB), Bab-
Ezzouar, 16111 Algiers, Algeria
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_51
695
In the environment, pharmaceuticals have been detected in hospital wastewaters
(Jose-Gomez et al. 2006), in surface water such as rivers and lakes (Ternes and Joss
2006), in marine waters as well as in soil matrices (Benner et al. 2009; Santos
et al. 2009). Recent investigations have shown that a number of pharmaceutical
compounds, such as Naproxen, Ibuprofen, Tylosin, spiramycin, Diclofenac,
Naproxen, Amoxicillin and Ibuprofen (Yu et al. 2006; Kemper et al. 2008), are
not completely eliminated in wastewater treatment, they are often toxic and
non-biodegradable, becoming extremely dangerous for the ecosystems (Vıctor
et al. 2011; Westergaardn et al. 2001).
New waste water purification technology leading to the complete mineralization
of organic pollutants is now considered as being the most suitable solution
concerning the decrease of the contamination level in water and wastewater
(Lanao et al. 2012; Magalhaes and Lago 2009). Semiconductor-assisted
photocatalysis has attracted considerable attention because it uses advanced oxida-
tion process as a tool for implementing large-scale purification of waste waters at
low cost. Most studies have focused on large bandgap semiconductors oxides, such
as TiO2 and ZnO, whose photo-excitation by UV light provides electron-hole pairs
capable of initiating the production of hydroxyl radicals in water (Radjenovic
et al. 2009; Gumy et al. 2006; Oyama et al. 2004; Mathews et al. 2009). Although
TiO2 is universally recognized as being the most photoactive catalyst (Farooq
et al. 2009; Shifu and Gengyu 2005), many reports have highlighted the effective-
ness of ZnO in removing organic compounds in water matrices (Bahnemann 2004).
ZnO photocatalysts in most studies are generally applied in the form of aqueous
suspensions (Carlos et al. 2000).
The aim of this work was to investigate the kinetic and efficiency parameters of
the photo-oxidation of mixture of two antibiotics models (tylosine and spiramycin)
in an aqueous solution under UV illumination. The bibliographic research indicated
that assisted photocatalysis degradation of the tylosin and the spiramycin in the
same solution has never been reported. On the other hand, biological methods were
used for the elimination of this pollutant but the elimination ratio is not important.
Biodegradation and biosorption of tetracycline and tylosin were conducted by
Amrane. Tetracycline presented a good adsorbability while tylosin remained
mostly present in the soluble phase. The Langmuir maximum adsorption capacity
was found to be 72 and 7.7 mg g�1 for tetracycline and tylosin respectively (Amrane et al. 2009). Ching-Hua et al. estimated the tylosin concentrations in
animal’s liquid waste to be 496 mg/day-animal. The detection limit of tylosin in waste water is 0.01 mg L�1 (Ching-Hua et al. 2001).
Materials and Methods
All the experiments were carried out under an artificial UV light radiation using
Pyrex glass helical reactor with an illuminated volume of 800 mL. A peristaltic
pump permitted the circulation of water from a glass reservoir to the reactor with a
696 D. Tassalit et al.
flow rate of 3.787 mL s�1. The volume of the solution in the system (1000 mL) is divided into two parts: the 800 mL irradiated volume and the dead volume present
in connecting tubing and in the reservoir. The reactor was illuminated from the axe
with a UV lamp. This lamp has a spectral light that distributes the emitted photons
at wavelengths less than 365 nm.
Chemical and Reagents
Tylosin and spiramycin were obtained from Sinochem Corporation. The semicon-
ductors employed as photocatalysts are TiO2 Dugussa P25 obtained from Merck,
with a BET surface area of 50 m2 g�1 and an average particle size equal to 2 μm and Zinc oxide was purchased from Aldrich Chemical Company of 99% purity, with a
BET surface area of 9 m2 g�1 and an average particle size equal to 1.5 μm. This kind of particles is small enough to be transported by water suspension. Solutions
were prepared by dissolving requisite quantity of Tylosin and/or Spiramycin in
distilled water before each experiment. The pH of the solutions was not adjusted
(free pH of the solution) and the catalyst was introduced in solution of Tylosin or
spiramycin.
The solution was stirred for at least 20 min in the dark to allow the equilibration
of the system, so that the problem of the loss of compound caused by the adsorption
can be solved. The zero time reading was obtained from a blank solution kept in the
dark but otherwise treated similarly to the irradiated solution. Irradiations were
obtained out using a Phillips ATLD 24 W lamp (λmax¼ 365 nm). 2 mL of samples were collected before and after at regular intervals during irradiation from the
reservoir by a plastic syringe then filtered in a Millipore disk. The tylosin concen-
tration was determined by measuring the absorption of pollutants, on a UV–vis
spectroscopy (UV-Visible Lambda 25, commercialized by Perkin Elmer Com-
pany). A correlation curve between tylosin, spiramycin concentrations and the
absorption was set-out.
Results and Discussion
The organic pollutants are never found alone in the environment; wastewater is a
complex mixture of several chemical compounds. To get closer to reality, we
conducted a study of a mixture of two pollutants (spiramycin and tylosin) to
improve the influence of the coexistence of pollutants on the photocatalytic kinetics
degradation.
The presence of a second pollutant may inhibit the conversion of the first one,
which can be explained by a competition and a greater affinity of the second
pollutant for the catalyst than the first one (Jose-Gomez et al. 2006). The study of
the photodegradation of tylosin and spiramycin mixture was carried out with
51 Photocatalytic Degradation of Tylosin and Spiramycin in Water. . . 697
reports of mass concentrations from 0.25 to 2. To achieve this study, the
solutions were prepared with different weight ratios of tylosin/spiramycin
(Table 51.1) keeping the operating conditions of TiO2 and ZnO concentrations of
0.05 mg L�1, flow rate Q equal to 3.787 mL s�1 and a free pH of the solution.
Effect of TiO2 on the Co-degradation
The photocatalytic degradation of an initial concentration of 10 mg L�1 of tylosin with different amounts of spiramycin was performed using the titanium dioxide
suspension as catalyst. The study showed that the adsorption of these two pollutants
on the surface of catalyst was negligible. The kinetics of the two degradation curves
of pollutants during photocatalytic treatment are shown in Figs. 51.1 and 51.2 for
tylosin and spiramycin respectively. The concentration of pollutants decreases
exponentially involving first-order kinetics. Mineralization of spiramycin and
tylosin is complete after 100 and 120 min of the treatment respectively.
In the presence of spiramycin, tylosin degradation is slowed. The idea of a
competition for adsorption sites between tylosin and spiramycin is required. The
results of the degradation kinetics of tylosin are shown in Table 51.2. We observed
that the apparent rate constant of degradation increases with increasing concentra-
tion of spiramycin to a ratio equal to 1, then it remains practically constant for ratios
greater than 1. This can be explained by the competitiveness of the pollutants
adsorption which minimizes the amount of tylosin adsorbed on the catalyst surface.
The results revealed in Fig. 51.2 and in Table 51.2 shows that the presence of an
amount of tylosin affects the degradation kinetics of the spiramycin. The degrada-
tion of tylosin and spiramycin mixture was compared with the photodegradation of
the spiramycin alone in the solution; the results show that the total mineralization
time of the spiramycin alone (40 min) is shorter than in the tylosin/spiramycin
mixture which presents 120 min of radiation. The degradation of spiramycin is
slowed with increasing the concentration of this pollutant but the difference is
insignificant for the various studied reports except for the 0.25, where the reaction
kinetic follow a pseudo Zero order. The degradation kinetic of spiramycin for other
reports follows a pseudo first order (Table 51.3).
To compare between the different calculated rate constants, we plotted in
Fig. 51.3, the k/k0 report based on the concentrations of spiramycin and tylosin
(CSpi/CTyl) with k0, the apparent speed constants of tylosin and spiramycin alone.
Table 51.1 Different solutions considered during
the codegradation
C0Spi (mg L �1) C0tyl (mg L
�1) CSpir/Ctyl 2.5 10 0.25
5 10 0.50
10 10 1.00
15 10 1.50
20 10 2.00
698 D. Tassalit et al.
1.20
1.00
0.80
0.60
0.40
0.20
0.00 0 20 40 60 80 100 120
time (min)
0,25 tylosin alone
Cspi/Ctyl
C/C0
0,5 1 1,5 2
140
Fig. 51.1 Photodegradation of tylosin in the presence of spiramycin with different ratio CSpi/Ctyl,, CTiO2¼ 0.05 g L�1, Q¼ 3.787 mL s�1, free pH
1.2
1.0
0.8
0.6
0.4
0.2
0.0 0 20 40 60 80 100 120 140
time (min)
0,25 Spiram ycin alone
Cspi/Ctyl
0,5 1 1,5 2
C/C0
Fig. 51.2 Photodegradation of the spiramycin for different ratio CSpi/Ctyl, CTiO2¼ 0.05 g L�1, Q¼ 3.787 mL s�1, free pH
Table 51.2 Rate constant, initial rate and the half time of the degradation the tylosin on the presence of TiO2
Cspi/Ctyl (mg/mg) kapp (min �1) r0.10
3 (mmol L�1 min�1) t1/2 (min)
0 0.068� 0.002 0.739� 0.004 10 0.25 0.021� 0.001 0.229� 0.005 33 0.5 0.024� 0.003 0.262� 0.002 29 1 0.035� 0.002 0.382� 0.008 20 1.5 0.031� 0.003 0.338� 0.011 22 2 0.032� 0.001 0.349� 0.010 22
51 Photocatalytic Degradation of Tylosin and Spiramycin in Water. . . 699
When using the 0.25 report, we found that there is degeneration of the order of the
reaction, the rate constant relative to the apparent reaction order equal to the unit
was estimated by dividing it by the initial concentration of the pollutant. The plot
k/k0 based CSpi/CTyl shows that from a concentration ratio equal to 1, the two curves
are superimposed indicating that the degradation kinetics of the two pollutants is
practically the same.
Effect of ZnO on Co-degradation
It is interesting to study the behavior of a solution containing a mixture of tylosin
and spiramycin in competition in the reaction medium in the presence of zinc oxide
(ZnO). Thus, we studied the mineralization of a solution composed of a mixture
of spiramycin and tylosin in optimal conditions previously defined
(CTiO2¼ 0.05 g L�1, Q¼ 3.787 mL s�1, pH and free Cpolluant¼ 10 mg L�1). Concentrations measured during the photodegradation are plotted in Figs. 51.4
and 51.5.
Table 51.3 Rate constant, initial rate and the half time of the degradation of the spiramycin on the presence of TiO2
CSpi/Ctyl kapp (min �1) r0.10
3 (mmol L�1 min�1) t1/2 (min)
Spi. alone 0.078 0.003 min�1 0.908� 0.005 9 0.25 0.254.10�4� 0.001 mol L�1 min�1 0.025� 0.002 57 0.5 0.030� 0.003 min�1 0.175� 0.001 23 1 0.031� 0.001 min�1 0.361� 0.001 22 1.5 0.032� 0.002 min�1 0.559� 0.003 22 2 0.038� 0.005 min�1 0.885� 0.007 18
1.2
1
0.8
0.6
0.4
0.2
0 0 0.5 1 1.5 2
spiramy cin
Tylosin
2.5
k/k0
Cspi/Ctyl
Fig. 51.3 Evolution of the constant rate for different ratios CSpi/Ctyl, Q¼ 3.787mL s�1, CTiO2¼ 0.05 g L�1
700 D. Tassalit et al.
The photodegradation of tylosin is delayed by the coexistence of spiramycin.
Mineralization of tylosin is complete after 120 min for the different ratios studied
except for the 1.5 and tylosin alone. It’s concluded that the photo-oxidation constant rate of tylosin alone is higher than kapp obtained in the case of tylosine mixed with
the spiramycin. However, the decomposition of spiramycin is strong when it is
alone or mixed with equal ratios at 1.5 and 2 where the kinetic curves codégradation
appear very close together and the pseudo-first order. The apparent rate constants
for degradation of tylosin increase with increase in the amount of 1.5 relative to the
spiramycin, and then decreases to a ratio equal to 2 (Table 51.4).
1.20
1.00
0.80
0.60
0.40
0.20
0.00 0 20 40 60 80 100 120
time (min)
0.25 Tylosin alone Cspi/Ctyl
C/C0
0.5 1 1.5 2
140
Fig. 51.4 Degradation of tylosin for different ratios Ctyl/CSpi. CZnO¼ 0.05 g L�1, Q¼ 3.787 mL s�1
1.20
1.00
0.80
0.60
0.40
0.20
0.00 0 20 40 60 80 100 120
time (min)
0.25 Spiram ycin alone
CTyl/CSpi
C/C0
0.5 1 1.5 2
140
Fig. 51.5 Degradation of the spiramycin for different ratios Ctyl/CSpi, CZnO¼ 0.05 g L�1, Q¼ 3.787 mL s�1
51 Photocatalytic Degradation of Tylosin and Spiramycin in Water. . . 701
The curves in Fig. 51.5 correspond to the temporal evolution of the reduced
spiramycin concentration for different ratios of tylosin/spiramycin. From these
curves, the time of degradation of the pollutant is the lowest for the mixtures of
spiramycin and tylosin ratios equal to 1.5 and 2 in the case of the spiramycin. The
curves are almost super-imposable for these other values, while the highest degra-
dation time recorded is when using the tylosin/spiramycin ratio equal to 0.25. The
co-degradation of the spiramycin follows a pseudo zero order for a ratio of 0.25 and
becomes a pseudo-first order kinetics for higher values of CTyl/CSpi ratios
(Table 51.5).
Figure 51.6 present the values of k/k0 versus the ratio of concentrations of
spiramycin and tylosin (CSpi/CTyl) in the case of two pollutants photodegradation
in the presence of zinc oxide as catalyst, k0 is the apparent rate constant for tylosin
and spiramycin alone in the solution. When 0.25 ratio is used, it’s found that there is a degeneration of the reaction order. It’s concluded that the reduced constant k/k0 speed increases with increasing the ratio of these two pollutants in the case of
spiramycin but decreases in the case of tylosin. Furthermore, it’s noted that the values of rate constants for the degradation of tylosin are located below that of
spiramycin.
Table 51.4 Values of the rate constants, initial speed and half-degradation reaction time of tylosin by using ZnO as catalyst
Ctyl/CSpi kapp (min �1) r0.10
3 (mmol L�1 min�1) t1/2 (min)
Tyl. alone 0.056� 0.001 0.611� 0.002 12 0.25 0.017� 0.001 0.185� 0.002 41 0.5 0.022� 0.001 0.240� 0.003 32 1 0.023� 0.001 0.251� 0.001 30 1.5 0.044� 0.002 0.480� 0.004 16 2 0.026� 0.001 0.393� 0.001 19
Table 51.5 Values of the rate constant, initial rate and the half time of the degradation of the spiramycin on the presence of ZnO
Ctyl/CSpi kapp (min �1) r010
�3 (mmol L�1 min�1) t1/2 (min)
Spi alone 0.028� 0.004 0.356� 0.003 25 0.25 0.025� 0.003.10�3 mmol L�1 min�1 0.025� 0.002 57 0.5 0.038� 0.003 min�1 0.064� 0.008 45 1 0.049� 0.004 min�1 0.128� 0.011 45 1.5 0.069� 0.002 min�1 1.204� 0.031 10 2 0.074� 0.005 min�1 1.373� 0.025 12
702 D. Tassalit et al.
Comparison Between ZnO and TiO2 Efficiency on the Photodegradation Process
The tylosin and Spiramycin degradation have been studied by heterogeneous
photocatalysis process with Titanium dioxide (TiO2), Degussa P-25, and zinc
oxide (ZnO). The comparison Between TiO2 and ZnO Photocatalysis rate is reported in Figs. 51.7 and 51.8. In the case of the tylosin, the results show that
the degradation with TiO2 presents a better photocatalytic behavior than the ZnO
for ratios lower than 0.25 and 1.2, for highest ratios the photodegradation rate is
more important when using Zinc oxide.
The titanium dioxide and Zinc oxide are also reported as good photocatalysts for
the degradation of the Spiramycin. The degradation rates obtained by using TiO2 are also important than ZnO values for ratios less than 1.25 and decrease for the
highest ratios. In other hand, two picks are obtained for rates equal to 0.48 and
0.38 10�3 mmol L�1 min�1 when using TiO2 and ZnO respectively.
Conclusion
In this study, ZnO and TiO2 are used as photocatalysts to degrade two pharmaceu-
tical pollutants. It has been shown in the literature review that many of contami-
nants are present in the water to be treated. It would then be appropriate to assess the
effectiveness of the catalysts in the case of mixtures of target molecules. To
investigate this situation, the photodegradation of a mixture of tylosin and
spiramycin was conducted with different mass ratios. The obtained results show a
Fig. 51.6 Evolution of the constant rate of the spiramycin and tylosin for different ratios CSpi/Ctyl, Q¼ 3.787 mL s�1, CZnO¼ 0.05 g L�1
51 Photocatalytic Degradation of Tylosin and Spiramycin in Water. . . 703
decrease of the removal rate when other pollutant is present in the same solution.
The presence of TiO2 photocatalysis is effective for the complete degradation of the
tylosin and the spiramycin pollutants. Photocatalytic degradation by a suspension of
ZnO also showed a good performance for the removal of these pollutants. Degra-
dation ratio of both pollutants in the presence of ZnO is substantially important than
TiO2 for ratios less than 1.25, this ratio increases for the highest ratios of pollutants.
The effectiveness of the reactor is considerable giving the advantage of being used
in real cases upstream or downstream of the biological treatment to a complete
water treatment of urban and industrial waste by using TiO2 and ZnO as catalysts.
1.6
1.4
1.2
0.8
1
0.6
0.4
0.2
0 0 0.5 1 1.5 2
TiO2 ZnO
2.5 3
Fig. 51.7 Tylosin photodegradation rate in the presence of TiO2 and ZnO catalysts
Fig. 51.8 Spiramycin photodegradation rate in the presence of TiO2 and ZnO catalysts
704 D. Tassalit et al.
Nomenclature
C0 Initial concentration of the pollutant, mg/L
C Concentration of the pollutant, mg/L
kapp Kinetic rate constant, min �1
r0 Rate of the degradation of pollutant, mmol/L min
T1/2 Half time of the reaction, min
Q Flowrate of the water solution, mL s�1
UV Ultraviolet light
Tyl. Tylosin
Spi. Spiramycin
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Comparison Between the Photocatalytic Degradation of a Textile Dye Under Sun Light and Artificial Irradiation
N. Sahraoui, N. Chekir, and D. Tassalit
Introduction
Dyes occupy an important place in synthetic organic compounds. They are used
extensively in industries including textiles, ink, plastics, cosmetics, tannery, and are
therefore, automatically found in water as an industrial pollutants (Schwarzenbach
et al. 2006). Their rejection into aquatic systems is causing damage to the environ-
ment due to their toxicity, which requires treatment (Liu et al. 2009).
Some of these pollutants are very stable and therefore difficult to be degraded
naturally or by using classic processes. Others are able to be degraded partially but
producing highly stable intermediate compounds which can have more toxicity than
the first pollutant.
The complexity of these pollutants and their color greatly affect the efficiency of
the classical treatments application, hence the need to develop more efficient
processes than conventional methods which can degrade recalcitrant pollutants.
Among the most recent progress, based on advanced oxidation techniques,
heterogeneous photocatalysis is nowadays, an emerging solution to the problems
of pollution by organic pollutants (Gaya and Abdullah 2008).
The Advanced Oxidation Processes are defined by (McGuigan et al. 1999) as the
very interesting alternative for the degradation of non-biodegradable organic pol-
lutants by biological treatment processes. These POAs are based on the generation
and use of the hydroxyl radical (OH�).
N. Sahraoui (*) Département de Génie des Procédés, Laboratoire des phénomènes de transfert,
USTHB, BP32, El Alia, Bab Ezzouar, 16111 Alger, Algeria
e-mail: [email protected]
N. Chekir • D. Tassalit
Unité de Développement des Equipements Solaires (UDES)/Centre de Développement des
Energies Renouvelables CDER, Bou-Ismail 42415, W. Tipaza, Algeria
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_52
707
Any process requires, in addition to the products for the treatment, a source of
energy. Solar energy available throughout the year with varying intensities can be a
useful alternative source, especially in developing countries. Indeed, this renewable
energy source is free and inexhaustible; it is the most abundant energy on Earth.
Photocatalytic treatment is thus presented as a technology of choice for the
pollution control and the integration of wastewater reuse, because it is an efficient,
simple and economical method. These attractive factors generate a great interest
from researchers for understanding, optimizing the industrial application of this
process (Helali 2012).
The objective of our study is to demonstrate the effectiveness of the
photocatalytic process for treating contaminated water with a Sandocryl Red
(BR46) textile dye. For this purpose, optimization of the operating conditions was
carried out. Photocatalytic degradation experiments were carried out at room
temperature by irradiating Zinc oxide ZnO semiconductor using a batch
photoreactor under ultraviolet (UV) radiation via sunlight or artificially by using
a UV lamp. The temporal evolution of the initial concentration of the contaminant
was studied with different concentrations of catalyst. The light intensity is mea-
sured with a digital UV pyranometre.
Materials and Measurement Method
Chemical Reagents
The used pollutant in this study is the Sandocryl Red (BR46), a pollutant that
belongs to the family of azo dyes. It is a synthetic red dye powder which is very
soluble in water (Table 52.1).
The used photocatalyst in this study is the commercial dioxide Zinc (ZnO), it is a
white powder supplied by Sigma Aldrich. It has a 100% zincite structure with a
specific surface area of 9 m2 g�1 and a particle diameter of 1.5 μm.
Experimental Facility
The photocatalysis treatment of polluted water is conducted by using used batch
photoreactor of 1 L volume capacity. The installation consists essentially of a batch
reactor exposed to either direct sunlight or the Ultraviolet radiation. This last is
UVC radiation of a lamp with a power of 15 W. The experimental setup is shown in
Fig. 52.1.
708 N. Sahraoui et al.
Measurement of the Pollutant Concentration
The temporal evolution of the pollutant concentration of Sandocryl Red is given by
the measurement of absorbance by a UV-visible spectrometer with dual beam of
type Shimadzu UV1800m, coupled to acquisition results software (UV PROB). The
contaminant has a maximum absorbance at a wavelength λ¼ 530 nm. The solar flux is measured at 5-min intervals of time between 9 h am and 15 h, using a
pyranometer coupled to software (Kipp & ZONZN, CMP11) with inclination of
36�. The aim of this work is to perform the parametric study on the photocatalytic
degradation of BR46 in the presence of zinc oxide. The reaction mixture was stirred
to homogenize the solution. Three milliliters of samples are taken every 15 min of
reaction. Before analysis by UV spectrophotometer, the mixture is filtered using a
cellulose acetate filter to remove any traces of ZnO before analysis. At the end of
each experiment, the system is immediately rinsed with distilled water.
Table 52.1 Physical and chemical properties of the BR46
CH3
CH3 CH3OSO3 −
+
H3C
N
N
N
N N
N
Chemical structure of the BR46 dye
Physical properties
Physical State Solid
Appearance Powder
Chemical properties
Molar mass 432 g mol�1
Fig. 52.1 Experimental setup
52 Comparison Between the Photocatalytic Degradation of a Textile Dye Under Sun. . . 709
Results and Discussion
Determination of the Wavelength of the BR46
The absorbance of BR46 is committed to their maximum adsorption. The absorp-
tion spectrum was obtained by scanning the solution of BR46 with concentration of
10 mg L�1 between 300 and 600 nm. Figure 52.2 shows the absorption spectrum of the pollutant for different times of the photodegradation reaction. It is clearly
observed that the BR46 maximum absorption coincide with a wavelength
λ¼ 530 nm.
Direct Photolysis and Photocatalysis
Photolysis of BR46
We conducted a preliminary study to see the degradation of the BR46 under UV
radiation in the absence of ZnO. To study the degradation of the pollutant by direct
photolysis, a solution of this pollutant with a concentration of 10 mg L�1 was exposed to UV irradiation in the photoreactor. The obtained results show that the
dye concentration decreases insignificantly, demonstrating that the irradiation with
1.090
1.000
0.500
0.000
−0.190 400.00 500.00
1 1
1 1
1
600.00 nm.
A b
s.
700.00 800.00
Fig. 52.2 Absorption spectra for different concentrations of BR46
710 N. Sahraoui et al.
UV in the absence of catalyst have no effect on the degradation of the dye. The ratio
of degradation is about 2% after 300 min of irradiation as shown in Fig. 52.3.
Photocatalytic Degradation of BR46 by Sun Radiation and UV
The photodegradation study of BR46 was performed using zinc oxide as catalyst
under solar and UV radiation. In order to optimize the operating conditions of the
photodegradation of BR46, several experiments were conducted by varying the
following parameters:
• Initial concentration of the pollutant;
• Catalyst concentration.
For the better understanding of the phenomenon of photocatalytic degradation of
BR46, knowledge of the degradation reaction order of is essential. For this reason,
we took inspiration from the results found in the literature explaining that the
kinetics of the phenomenon of photodegradation of many organic pollutants fol-
lows a first order reaction whose speed is described by the following equation:
r ¼ dC dt
¼ kapp C ð52:1Þ
with:
r: Photocatalytic degradation rate (mg L�1 min�1) kapp: Apparent degradation constant (min
�1) C: Dye concentration (mg L�1) t: Irradiation time (min)
The solution concentration of the dye when t¼ 0, generates another equation which gives the linearization:
1.20 C/C0
1.00
0.80
0.60
0.40
0.20
0.00 0 100 200 300
time(min)
Fig. 52.3 Photolysis of BR46, CBR46¼ 10 mg L�1, free pH
52 Comparison Between the Photocatalytic Degradation of a Textile Dye Under Sun. . . 711
�ln C C0
¼ kapp t ð52:2Þ
Photocatalytic tests were then carried out in the presence of ZnO assuming that
the reactions are pseudo-first order.
Influence of the Initial Concentration of the Pollutant Under Sunlight
The concentrations of Sandocryl Red (BR46) was varied between 5 and 40 ppm at a
free pH of the solution (between 6, 5 and 7) while maintaining the amount of used
catalyst constant and equal to 1 g L�1. Figure 52.4 shows the temporal evolution of the reduced concentrations of Sandocryl Red (BR46). The results confirm that the
degradation of BR46 is important when the initial concentration of this pollutant
decreases.
The plot of �ln C/C0 versus time in Fig. 52.5 and the values of Kapp reported in Table 52.2 shows that the rate constant (Kapp) decreases as the substrate concen-
tration increases. This is explained by a lower participation of photons when the
color of the solution becomes more intense and therefore a low activation of ZnO
(low production of OH� radicals). The obtained results show that the rate constant for the degradation (Table 52.2)
decreases with increasing of the concentration of BR46, the rate constants of the
values are between 0.143 min�1 for the lower concentration of pollutant (5 ppm) and 0.048 min�1 for the highest concentration (40 ppm).
Fig. 52.4 Evolution of the temporal different reduced pollutant concentrations with free pH and CZnO¼ 1 g L�1
712 N. Sahraoui et al.
Effect of the Initial Concentration of the Pollutant Under UV Radiation
The same experiments with sun light were repeated in the presence of UV radiation
in order to compare the two modes of radiation maintaining the same operating
conditions:
• Free pH of the solution (between 6.5 and 7);
• Initial concentrations of dye range are from 5 to 40 ppm;
• Amount of catalyst used constant are equal to 1 g L�1.
Figure 52.6 shows the evolution of reduced concentrations of Sandocryl Red
(BR46) versus time.
From the curves of Fig. 52.6, the photodegradation is strongly influenced by the
initial concentration of the substrate. The degradation of the BR46 is even more
important when the initial concentration of this pollutant decreases. By using a
concentration of 5 ppm, the degradation is very fast and it reaches an elimination
ratio of 97%.
Fig. 52.5 Temporal evolution of ln (C/C0) for different pollutant concentrations with free pH and CZnO¼ 1 g L�1
Table 52.2 Values of the rate constants for different values of the pollutant concentrations
BR 46 (ppm) Kapp (min �1) r0 (mg L
�1 min�1) t1/2 (min) R 2
5 0.143 0.715 5 0.99
10 0.092 0.920 7.5 0.99
20 0.065 1.300 10 0.99
40 0.048 1.921 14 0.99
52 Comparison Between the Photocatalytic Degradation of a Textile Dye Under Sun. . . 713
The plot of�ln(C/C0) versus time for various initial concentrations of Sandocryl Red (BR46) (Fig. 52.7) show that the kinetics is pseudo first-order, the concentra-
tion satisfactory follows the expression of the first order equation with a slope equal
to the apparent speed constant kapp. The values are shown in Table 52.3.
The obtained results (Fig. 52.7 and Table 52.3) shows that the rate constant of
degradation decreases with increasing the concentration of BR46, the rate constants
are situated between 0.059 min�1 for the lowest concentration of pollutant (5 ppm)
Fig. 52.6 Temporal evolution of different reduced pollutant concentrations with free pH and mass of catalyst¼ 1 g L�1
Fig. 52.7 Temporal evolution of �ln(C/C0) for different pollutant concentrations with free pH and catalyst mass¼ 1 g L�1
714 N. Sahraoui et al.
and 0.015 min�1 for the highest concentration (40 ppm). It can be observed that the rate constant (kapp) decreases as the substrate concentration increases. This is
explained by a lower participation of photons because of the screen effect.
Influence of the Catalyst Concentration Under Sun Radiation
The effect of catalyst concentration (ZnO) on the photo-oxidation of the BR46 was
studied using amounts ranging from 0.125 g L�1 to 1.5 g L�1 under the sun and UV radiation. The experiments were performed with a solution of 10 g L�1 of BR46 and free pH (pH of the solution without adjustment). The obtained results are illustrated
in Fig. 52.8.
The results presented in Fig. 52.9 show that the rate of deterioration of BR46
ZnO for different concentrations are very high and can reach a value of 100% of
removal, like in the case of high concentrations of catalyst (1,5 g L�1). The rate of degradation and the rate constants increase with increasing the amount of ZnO as
Table 52.3 Values of rate constants for the different values of pollutant concentrations
CBR46 (ppm) Kapp (min �1) r0 (mg L
�1 min�1) t ½ (min) R 2
5 0.059 0.295 11.748 0.95
10 0.041 0.410 16.906 0.90
20 0.24 0.480 28.881 0.98
40 0.015 0.600 46.210 0.98
Fig. 52.8 Evolution of the concentration of the pollutant over time with free pH, Cpollutant¼ 10 ppm
52 Comparison Between the Photocatalytic Degradation of a Textile Dye Under Sun. . . 715
shown by the results in Table 52.4 and Fig. 52.10 which present the temporal
evolution of �lnC/C0 at different concentrations in the catalysts.
Influence of the Catalyst Concentration Under UV
It is important to know the optimal catalyst load for the efficient removal of a
pollutant. The effect of catalyst concentration (ZnO) on the photo-oxidation of
BR46 under UV light was also conducted under the same operating conditions as
for the study of solar radiation using catalyst amounts ranging from 0.125 g L�1 to 1.5 g L�1. The experiments were performed with a solution of 10 g L�1 of BR46 and free pH (pH of the solution without adjustment). The results obtained are
illustrated in Fig. 52.11.
The results shown in Fig. 52.11 show that BR46 deterioration rate by ZnO with
different concentrations are very high and can reach a value of 100% removal, in
case of concentrations of catalyst (1.5 g L�1). It is also found that the rate of
Fig. 52.9 Temporal evolution of ln(C/C0) for different concentrations of ZnO, C0BR46¼ 10 mg L�1, free pH
Table 52.4 Values of rate constants, initial speed and time of half-reaction of BR46 degradation for different concentration ZnO
CZnO (g L �1) Kapp (min�1) r0 (mg L
� min�1) t1/2 (min) R 2
0.125 0.029 0.29 23 0.99
0.250 0.078 0.78 9 0.99
0.500 0.129 1.29 5 0.98
1.000 0.139 1.39 5 0.99
1.500 0.179 1.79 4 0.96
716 N. Sahraoui et al.
degradation and the rate constants increase with increasing the amount of ZnO as
shown by the results in Fig. 52.11 and the temporal evolution of �ln C/C0 for different catalysts concentrations and Table 52.5.
The increase in catalyst concentration generally favors the absorption of the
contaminant to the surface, which increases the degradation rate. However too
much affects the light scattering in the solution to treat involving a reduction of
the degradation kinetics
Fig. 52.10 Evolution of different reduced concentrations of the catalyst over time with free pH and Cpollutant¼ 10 ppm
Fig. 52.11 Temporal evolution of ln(C/C0) for different concentrations of ZnO, C0BR46¼ 10 mg L�1, free pH
52 Comparison Between the Photocatalytic Degradation of a Textile Dye Under Sun. . . 717
Conclusion
The carried studies in this work show that the advanced oxidation processes is
effective for the treatment of water polluted by textile dyes. Degradation of the
Sandocryl Red: BR46 is performed by the oxidizing action of the hydroxyl radicals
generated in the medium to be treated. These radicals are capable of degrading
almost all organic pollutants because of their high oxidizing power and their
reactivity and non selectivity against the organic substances. The study of the
influence of different parameters has shown that photodegradation of this pollutant
is favored for low pollutant concentrations and with increasing the concentration of
catalyst.
However, the results of treatment using sun radiation gave better results com-
pared to the treatment by using UV light radiation.
References
Gaya, U. I., & Abdullah, A. H. (2008). Heterogeneous photocatalytic degradation of organic
contaminants over titanium dioxide: A review of fundamentals progress and problems. Journal of Photochemistry and Photobiology C: Photochemistry Reviews, 9(1), 1–12.
Helali, S. (2012). Application de la photocatalyse pour la dégradation des polluants chimiques et bacteriologiques dans l’eau en utilisant des catalyseurs irradies par des photons de lumiere naturelle ou arti_cielle (UV-A/UV-B). France: Université Claude Bernard—Lyon I.
Liu, Z., Kanjo, Y., & Mitzutani, S. (2009). Removal mechanisms for endocrine disrupting
compounds (EDCs) in wastewater treatment—physical means, biodegradation, and chemical
advanced oxidation: A review. Science of the Total Environment, 407, 731–748. McGuigan, K. G., Joyce, T. M., & Conroy, R. M. (1999). Solar disinfection: Use of sunlight to
decontaminate drinking water in developing countries. Journal of Medical Microbiology, 48, 785–787.
Schwarzenbach, R. P., Escher, B. I., Fenner, K., Hofstetter, T. B., Johnson, C. A., Von Gunten, U.,
et al. (2006). The challenge of micropollutants in aquatic systems. Science, 313(5790), 1072–1077.
Table 52.5 Values of rate constants, initial speed and time BR46 degradation half-reaction for different concentration ZnO
CZnO (g L �1) Kapp (min
�1) r0 (mg L �1 min�1) t1/2 R
2
0.125 0.014 0.14 49.51 0.99
0.25 0.024 0.24 28.88 0.98
0.5 0.026 0.26 26.65 0.95
1 0.027 0.27 25.672 0.94
1.5 0.052 0.52 13.330 0.81
718 N. Sahraoui et al.
Chapter 53
Vulnerability and Impact of Climate Change Processes on Water Resource in Semi-Arid Areas: In Essaouira Basin (Morocco)
Salah Ouhamdouch, Mohammed Bahir, Abdellatif Souhel, and Carreira Paula
Introduction
Since the 1950s, the earth’s climate has undergone significant changes represented mainly by the warming due to greenhouse gas emissions, in close relation with
human activity (IPCC, 2013). These changes have a negative influence on the
environment and man. In most semi arid areas, seasonal and long-term climate
variability changes the dynamics of water cycle. Groundwater levels are also falling
at alarming rates. Nowadays, groundwater withdrawal and environmental trends
may bring about serious problems in some parts of the world. The availability of
sufficient fresh waters has become a limiting factor for development. Among the
consequences of these changes, include: (1) the increase of the temperature,
(2) decrease in precipitation as well as the mass of the ice sheets, (3) rise in sea
level and (4) the scarcity of water resources. In addition, the countries of the
Maghreb (Algeria, Morocco and Tunisia) have not been spared the impact of
these changes that negatively affect the most of their natural resources, including
water resources. Locally, the bay of Essaouira also has its share of these effects,
S. Ouhamdouch, Ph.D. (*) Department of Geology, Laboratory 3 GEOLAB, Faculty of Science Semlalia,
Marrakech, Morocco
e-mail: [email protected]
M. Bahir • A. Souhel
Department of Geology, E.N.S. Marrakech, Marrakech, Morocco
e-mail: [email protected]; [email protected]
C. Paula
Centro de Ciências e Tecnologias Nucleares, CTN/IST, Universidade Técnica of Lisboa,
Lisboa, Portugal
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_53
719
which are represented mainly in the scarcity of water resources see also salinity
following the invasion of sea water and the increase in the salinity of the soil,
degradation of groundwater quality and the extermination of a number of water
sources.
Climate Change on a Global Scale
According to its report of September 2013, the Intergovernmental panel on Climate
change (IPCC) states that warming of the climate system of the earth is unequiv-
ocal, adding that the human influence is the primary cause of this warming. Among
the results of this global warming, we note that the three examples below:
– The warming of the atmosphere: The last three decades are successively warmer
at the earth’s surface than all preceding decades since 1850. The average temperature of the globe shows a warming of the order of 0.85 �C during the period 1880-2012 (Fig. 53.1). For precipitation, they have experienced an
Fig. 53.1 Observed Anomalies of average temperatures on the surface of the globe (IPCC, 2013)
720 S. Ouhamdouch et al.
increase since 1901 on the continental regions of the middle latitudes of the
northern hemisphere, as well as eastern South America, and a decrease in the
Sahel; in the Mediterranean; in southern Africa and in parts of south Asia
(Fig. 53.2) (IPCC, 2013).
– The reduction of the surface area of the ice caps and glaciers: everywhere in the
world, there is a reduction of the surface area of the ice caps, and ices. Over the
past three decades, the extent of annual average arctic sea ice has been decreas-
ing at a rate of 3.5–4.1% per decade (Fig. 53.3).
– Sea level: since the early 1970s, the decrease of the glacier masses and the
thermal expansion of the oceans contribute to them only about 75% of the rise
global mean sea level. Between 1901 and 2010, the average level of the sea
shows an increase of 0.19 cm (Fig. 53.4).
Fig. 53.2 Maps of the observed changes in precipitation between 1901 and 2010, and between 1951 and 2010 (IPCC, 2013)
14
12
10
8
6
4 1900 1920 1940 1960 1980 2000
Fig. 53.3 Arctic summer sea ice extent (in million km2) (IPCC, 2013)
53 Vulnerability and Impact of Climate Change Processes on Water Resource. . . 721
Climate Change in North African
As in most world countries, the three countries of the Maghreb (Algeria, Morocco
and Tunisia) have not been spared the impact of climate change, which has affected
and still affects negatively the most of their natural resources. Among these
resources, the resource water. For example, the north-west Algeria has experienced
a reduction of the order of 40% of annual precipitation from the first half of the
1970s (Nouaceur et al. 2013; UNESCO, 2010). This reduction is carried out in a
temperature increase, which corresponds to the signal of global climate change.
This change has affected the river flows of this region. According to the fourth
report of the IPCC (Bates et al., 2008), the blades of waters passed the annual
average of the period 1976–2002 are 28–36% lower than those of the period
1949–1976, and this reduction is due to climate change. According to the national
institute of meteorology Tunisia, the rainfall pattern in the Tunisia during the
twentieth century has been marked by relative stability. In contrast to the rest of
the century was marked by the alternation of dry periods (1940–1950) and wet
periods (1950–1960). However, the temperature tends to increase (1.1 �C) since the sixties. In addition to this increase, Tunisia has suffer amplification erosion pro-
cesses dry up the soil and consequently augment and increase the salinity of the
water tanks. In addition, the elevation of accelerated sea level due to global
warming will have serious impacts on the shoreline such that the contamination
of the aquifers in the coastal waters of freshwater by the marine waters of salt. In
Morocco, the water resources are limited and have a potential water that can be
mobilised estimated at 20 billion m3, giving an average of 700 m3/capita/year,
which is recognized as a relatively high water stress. The number of years of deficit
rainfall everywhere is more important than that of surplus years (Fig. 53.5). This
decline coincides with an increase in the frequency of droughts also visible from the
1980s (Driouech et al., 2013; Sebbar et al., 2011; Driouech, 2010; Sinan et al.,
2009). As found by various previous studies (including that of the minister of
public works, 2007), we distinguish two dry periods: 1980–1985 and 1990–1995.
200
150
100
50
0
−50 1900 1920 1940 1960 1980 2000
Fig. 53.4 Global average sea level evolution (in mm) (IPCC, 2013)
722 S. Ouhamdouch et al.
By contrast, the evolution of the temperature is constant, and tends to increase
(Fig. 53.6), which corresponds to the signal of global climate change, and makes
Morocco among the countries affected by climate change. Among the results of this
change, we quote: (1) Erosion of the soil under the effect of desertification, which
resulted in the silting up of dams. (2) Accentuation of soil salinization and water
resources. (3) Lowering of the piezometric levels of the groundwater on one side
Fig. 53.5 National averages (in %), of relative anomalies of annual rainfall, calculated over the 14 Moroccan meteorological stations. 1961–2008 period (Driouech, 2010)
Fig. 53.6 Trends in seasonal mean temperature calculated for the 1961–2008 period at the 14 meterological stations (in �C / decade). (Driouech, 2010) (Color figure online). Note bene: winter: red bars, spring: green bars, autumn yellow bars
53 Vulnerability and Impact of Climate Change Processes on Water Resource. . . 723
and the increase in the level of the sea on the other side, which creates in coastal
areas, a reversal of current, resulting in the invasion of seawater and the destruction
of the hydraulic potential.
Climate Change and Essaouira Basin
In Morocco, most studies of the impact of climate change on water resources
focused on coastal areas (Bouchaou et al., 2011; Bahir et al., 2003; Hsissou et al.,
2001). These regions that are densely populated and subjected tourism activities are
characterized by a growing demand for water.
Geographic Location
The Essaouira basin is located on the Atlantic coast of Morocco, specifically at the
western end of the high atlas chain, where it occupies an area of 1827 km2. This
basin includes several aquifer systems whose structures and resources are often
poorly known. The most important of these systems belong to two synclinal units:
the unit of Bouabout located in the eastern part of the basin and the unit of Essaouira
synclinal who represents the Western part of the basin. These two units are
separated by the Tidzi diaper (Fig. 53.7).
Fig. 53.7 Location of the study area
724 S. Ouhamdouch et al.
Geological Cadre
At the basin level of Essaouira, the Triassic and the Jurassic have outcrops very
reduced and localized to the anticlines core (jbel Hadid NW, jbel Amstétene to the
SW and Tidzi diaper). While the tertiary formations and the quaternary are found in
the basins syncline. The Triassic is made up of red clay salt, basalt diabase and
pelites sandstone. The Jurassic is represented by an alternation of carbonate
deposits (limestone’s and dolomites) and marls rich in evaporite (gypsum and anhydrites). While the cretaceous formations and quaternary rocks are grouped in
the stratigraphic log synthetic (Duffaud et al., 1966) (Fig. 53.8).
The Essaouira basin is a vast area synclinal open on the Atlantic Ocean, affected
by several folds and accident, which allow for the individualization of many
Fig. 53.8 Log synthetic stratigraphic Cretaceous and Tertiary of Essaouira basin
53 Vulnerability and Impact of Climate Change Processes on Water Resource. . . 725
synclinal basins: (1) the synclinal basin of Bouabout occupying the upstream part of
the basin, crossed by the river Igrounzar. (2) The bowl of Kourimat and (3) the
synclinal basin of Essaouira synclinal (downstream part of the basin), separate from
that of Bouabout by the diaper of Tidzi which shows the outcrop of the subterranean
triassic. These cups give birth to hydrogeological aquifer systems (Fig. 53.9) (Bahir
et al., 2013; Chamchati and Bahir, 2013; Bahir et al., 2008; Jalal et al., 2001).
Climate Cadre
According to the Martonne index (53.1) in which the equation stated below, the
Essaouira basin is located in a semi-arid zone, characterized by ocean, continental
and mountain influences. The aridity is marked in the basin, especially in the
summer; it is relatively increased in going from the Atlantic to the continent.
This aridity growth is the result of the remoteness of the ocean influence, where
the rain decreases and the thermal differences increase.
I ¼ P= Tþ 10ð Þ ð53:1Þ
With P: average annual rainfall in mm and T: average annual temperature in �C. At the level of the Igrounzar’s station, the temperatures show a very significant seasonal variation. In winter, minimum temperatures can reach up to�11 �C, while summer highs are in the order of 40–45 �C (Chamchati and Bahir, 2011). From the Ombrothermic diagram of Igrounzar’s station, the hot season runs fromMarch until
Fig. 53.9 Geological map (1:1,000,000) of study area
726 S. Ouhamdouch et al.
October or even November. While the wet period occurs from November to march
(Fig. 53.10). The rainfall varies from year to year around an average of 306 mm
(Fig. 53.11). For the series of years stripped (1977–1978 to 2010–2011), are found
in wet years, the height of which exceeds the average (1987–1989, 1995–1997,
2005–2006, 2008–2010), therefore, the rush and show an irregular interannual
striking.
Piezometry
To have an idea about the evolution of the piezometric level in the Essaouira basin,
we will treat in a first time the water cenomanian-turonian of Bouabout (upstream)
and in the second time the water plio-quaternary (downstream):
– Cenomanian-turonian water (Bouabout): The companions of measuring the level
piezometric carried out from 2006 to 2010 were used to establish the evolution
Fig. 53.10 Ombrothermic diagram of Igrounzar station
Igrounzar (1977-2010)
P moy(mm)
19 77
-7 8
19 78
-7 9
19 79
-8 0
19 80
-8 1
19 81
-8 2
19 82
-8 3
19 83
-8 4
19 84
-8 5
19 85
-8 6
19 86
-8 7
19 87
-8 8
19 88
-8 9
19 89
-9 0
19 90
-9 1
19 91
-9 2
19 92
-9 3
19 93
-9 4
19 94
-9 5
19 95
-9 6
19 96
-9 7
19 97
-9 8
19 98
-9 9
19 99
-0 0
20 00
-0 1
20 01
-0 2
20 02
-0 3
20 03
-0 4
20 04
-0 5
20 05
-0 6
20 06
-0 7
20 07
-0 8
20 08
-0 9
20 09
-1 0
20 10
-1 1
800.000 700.000 600.000 500.000 400.000 300.000 200.000 100.000
0.000
Fig. 53.11 Evolution of the annual rains in Igrounzar station from 1977 to 2010
53 Vulnerability and Impact of Climate Change Processes on Water Resource. . . 727
curves of the water level of a water points number such as 1126/52 and 1726/52
(Fig. 53.12). La représentation graphique de l’évolution du niveau piézométrique
dans la période 2006–2010 �a ces points, montre une diminution du niveau de l’eau de Juin 2006 �a Octobre 2008. Cette baisse se explique par la sécheresse qui affecte la région au cours des deux années 2007 et 2008 et aussi par la surexploitation de
l’aquifère pour l’irrigation afin de compenser l’impact de la sécheresse. Après
Octobre 2008, le niveau de l’eau commence �a monter pendant une période de huit mois, puis recommence �a baisser.
– Plio-quaternary water: the companions of measurement of the piezometric level
of the Plio-quaternary aquifer, during 1990,1995, 2000, 2004 and 2009 resulted
in the piezometric maps (Fig. 53.13). They show a sense of overall flow of the
South-East to North-West, conditioned by the recovery of its substratum to the Is
a result of the lifting of the Tidzi diaper. A comparison of these piezometric
maps reveals a decrease of the piezometric levels in 1995 (the driest year of the
century in Morocco) within a certain wells have experienced measures of level
30.00
02/2006
01 /2
00 6
03 /2
00 6
05 /2
00 6
07 /2
00 6
09 /2
00 6
11 /2
00 6
01 /2
00 7
03 /2
00 7
05 /2
00 7
07 /2
00 7
09 /2
00 7
11 /2
00 7
01 /2
00 8
03 /2
00 8
05 /2
00 8
07 /2
00 8
09 /2
00 8
11 /2
00 8
01 /2
00 9
03 /2
00 9
05 /2
00 9
07 /2
00 9
09 /2
00 9
11 /2
00 9
01 /2
01 0
06/2006
12/2006
02/2007
04/2007
06/2007
08/2007
10/2007
12/2007
02/2008
04/2008
06/2008
08/2008
10/2008
12/2008
02/2009
04/2009
06/2009
09/2009
22/12/09
35.00
40.00
1726/52
1126/52
45.00
P (M
) P
(M )
50.00
60.00
65.00
70.00
75.00
80.00
Fig. 53.12 Evolution of the piezometric level in the period 2006–2010 at the level of the water points 1126/52 and 1726/52 (2006–2010)
728 S. Ouhamdouch et al.
in the five periods (Table 53.1). After the dry year of 1995, a number of wet
years, the occurrence of 1996–1997, 2002, 2003, 2004, 2006 and 2009 can
restore and go back in the piezometric level in the aquifer. This variation of
the piezometric level can only be explained by the vagaries of the weather and
the over-exploitation for irrigation in order to disguise the impact of the drought.
Fig. 53.13 Maps piezometric groundwater Plio-Quaternary of the synclinal area of Essaouira in 1990, 1995, 2000, 2004 and 2009
53 Vulnerability and Impact of Climate Change Processes on Water Resource. . . 729
Hydrochemistry
The chemistry study of water allows the identification of chemical facies of waters,
their quality and potability, and their irrigation suitability. The Piper diagram shows
the water of plio-quaternary aquifer has a chloride-sodium facies (Fig. 53.14).
Based on electrical conductivity and chlorides of plio-quaternary groundwater,
we can have an idea on water quality and its evolution. In the temporary scale,
the groundwater quality is becoming more and more good by going to the driest
year that knows Morocco (1995) in 2009, through the years modestly dry and rainy.
Spatially, its takes a positive direction from the North to South of the groundwater
table (Fig. 53.15 and Table 53.2). The temporal and spatial evolution of this quality
have closely linked to climatic change.
Table 53.1 Variation in piezometric within the water Plio-Quaternary
N�
IRE X (m) Y (m)
Z
(m)
Sep90
(m)
May95
(m)
Jul00
(m)
March04
(m)
Oct09
(m)
3/51 81400 93400 18 5.4 4.8 5.2 5.5 4
15/51 86000 97970 70 54.2 52.6 54 65 63
93/51 92370 101900 98 66.9 64.7 66.5 67.4 54
138 88275 92825 109 85 81.8 84.1 85.3 104
149/51 85100 105800 40 2 1 1.5 4 2
327/51 88800 88800 130 108.3 98.8 107.2 108.2 106
116/51 100650 96000 200 179 176 178.2 sec sec
117/51 100450 98500 180 137.4 134.5 136.7 sec sec
Fig. 53.14 Chemical facies of plio-quaternary
groundwater
730 S. Ouhamdouch et al.
Fig. 53.15 (a) Temporal and spatial distribution of the Electrical conductivity of the groundwater in the aquifer plio-quaternary (1995, 2004 and 2009). (b) Chlorides (1995 and 2009)
Table 53.2 Simplified grid for groundwater
Quality
parameter
C.E.
(μs/cm) Cl�
(mg/l)
NO3 �
(mg/l)
NH4 þ
(mgNH4 þ/l)
MO
(mgO2/l)
Excellent <400 <200 <5 �0,1 <3 Good 400–1300 200–300 5–25 0,1–0,5 3–5
average 1300–2700 300–750 25–50 0,5–2 5–8
Bad 2700–3000 750–1000 50–100 2–8 >8
Very bad >3000 >1000 >100 >8
53 Vulnerability and Impact of Climate Change Processes on Water Resource. . . 731
Stable Isotopes
In the Essaouira basin, the hydrodynamic is influenced by the structure (folds and
faults) which determines the flow (Bahir, 2007). In the study area, the isotopes of
the water molecule, the oxygen-18 (18O), deuterium (2H), tritium (3H) and carbon-14
(14C), may provide part of the answer in the determination of the areas and
conditions aquifer recharge, as well as their relationship and their age. The isotopic
analyses were carried out in the institute of technology and nuclear Lisbon. The
isotopic content of the water plio-quaternary are between �3.72 and �4.56 δ‰ v-smow. Those of groundwater turonienne are between �4.17 and �4.55 δ‰ v-smow. The results of the analyses of 2H to allow to set on a diagram of
correlation 18O-2H the local meteoric right (LMW) equation 2H¼ 7.72� 18 Oþ 10.53 (r2¼ 0.82), close to the Global meteoric water (GMW) slope 8 with excess 2H close 10 (Craig, 1961). It characterizes the precipitation of oceanic
origin. The equation of this line was calculated without taking into account the
three points 390/51, 27251, and Ksob wadi, identified as evaporated, because they
fall below GMW. The other points are aligned on the LMR, which indicates that the
supply of water aquifers is completed quickly without significant evaporation. The 3
H is a radioactive element in the cycle of water through rainfall, its presence with
concentrations above 2 units tritium (TU) means a charging current (Olive et al.,
1996). By contrast, the water having concentrations of less than 2 UT are confed-
erated without active recharge (Olive, 1999). The results are compiled in Table 53.3.
The levels of 3H varied between a minimum value of 0.2 and a maximum of 4.2 UT.
The water points 272, 327, 65, 386, and 203/51 have a content 3H greater than 2 UT,
which means a charging current. While the other points are levels very low. This
uses the technique of dating by 14C to confirm or affirm the hypothesis. The 14C is
the radioelement the most used to date ancient waters at very low levels of 3H.the
results obtained are grouped in Table 53.3. The analysis makes it possible to
identify that: the waters of the two points 65 and 386/51 have significant assays in 3H and percentages in 14C higher than 85%, which makes them as current. The
drilling M98, which does not, 3H detectable but has a 14C content of 80% shows a
power supply prior to the nuclear tests from 1962 to 1963, and its radiocarbon age
does not exceed a 2000 years. The radiocarbon age of the drilling 390/51 is of the
order of 6500 years ago, and one of 380/51 is greater than 2000 year. These two
boreholes capturing the turonian aquifer, feed, respectively, the Essaouira city and
the village of Si Ahmed Ou Hmad (5000 inhabitants). This reflects that we are in the
presence of an ancient water and that it is in the process of exhausting a strategic
resource, which could be used in extreme cases (Fig. 53.16).
Conclusion
In addition to the demographic pressure, the cultural practices and pastoral, climate
change put the countries of the Maghreb (Algeria, Morocco and Tunisia) in
alarming water situation manifested by: (1) the drought, which accentuates the
732 S. Ouhamdouch et al.
T a b le
5 3 .3
P h y si ca l p ar am
et er s an d an al y si s o f ra d io ac ti v e is o to p es
o f g ro u n d w at er
in th e co as ta l ar ea
o f E ss ao u ir a
N � I R E
N at u re
O ri g in
A lt it u d e
P ro f (m
)
T (� C )
P H
A lc
M éq /l
3 H U T
1 4 C
p cm
1 3 C
� / ��
2 7 2 /5 1
W el l
P li o -Q
1 0 5 .5
3 8 .4
2 0 .6
7 .6 5
3 .3 0
3 .9
2 1 /5 1
W el l
P li o -Q
1 3 5
2 9
2 1 .7
7 .1 3
2 .8 0
2 .0
3 2 7 /5 1
W el l
P li o -Q
1 3 0
2 2 .2
7 .2 3
4 .0 3
3 .2
6 5 /5 1
W el l
T u ro n
1 5
2 0 .3
2 2 .5
7 .4 8
4 .6 4
2 .8
8 8 .9 � 0 .5
�9 .8
3 9 0 /5 1
b o re h o le
T u ro n
9 5
2 0 0
2 6 .7
7 .3 5
4 .9 4
2 3 2 .5 � 0 .4
�9 .4
3 8 6 /5 1
b o re h o le
T u ro n
1 0 5
1 0 0
2 3 .2
7 .5 6
4 .2 6
4 .2
8 4 .8 � 0 .6
�1 0 .3
3 8 0 /5 1
b o re h o le
T u ro n
1 3 5
1 9 4
2 6 .1
7 .5 4
4 .6 7
1 3 .0 � 0 .5
�9 .0
M 9 8
b o re h o le
B ar -A
p t
9 0
1 0 0
2 2 .0
7 .5 9
3 .5 5
1 .1
7 9 .6 � 0 .6
�9 .3
A . A g h b al o u
b o re h o le
B ar -A
p t
8 0
2 3 .1
7 .5 0
3 .5 8
1 7 2 .0 � 0 .4
�1 0 .0
2 1 6 /5 1
S o u rc e
P o r- B er
1 6 0
2 3 .1
7 .2 8
4 .5 3
1
2 1 8 /5 1
S o u rc e
P o r- B er
3 0 8
2 2 .5
7 .2 9
4 .2 4
1 6 8 .5 � 0 .6
�9 .9
3 6 1 /5 1
b o re h o le
L ia s
3 8 2
9 0
2 3 .5
7 .2 2
4 .4 5
2
2 0 3 /5 1
b o re h o le
C al lo w
1 4
5 0
2 2 .7
7 .1 1
4 .2 6
3 .8
3 4 6 /5 1
b o re h o le
T u ro n
1 0 5
1 .5
3 6 3 /5 1
b o re h o le
T u ro n
1 5 0
1 .2
1 4 9 /5 1
b o re h o le
T u ro n
4 0
0 .2
53 Vulnerability and Impact of Climate Change Processes on Water Resource. . . 733
phenomenon of desertification, (2) increased salinity of the soil and the lowering of
the piezometric levels of the groundwater. It encourages the countries of the
Maghreb to develop the strategy of the increased mobilization of
non-conventional, such as the desalination of seawater and brackish water. The
complementarity of the approaches hydrochemical, piezometric and isotopic may
lead to the diagnosis of the state of vulnerability of the aquifers in the basin of
Essaouira in the face of climate change. However, the development of a strategy for
the rational exploitation could thus enable the value of its waters, while preserving
its potential in the long term. As well as the use of non-conventional resources such
as desalinated seawater for the supply of drinking water or treated wastewater for
agriculture must be seen as a priority in order to avoid trigger situations of water
scarcity.
Acknowledgment This research was carried out within the Laboratory 3GEOLAB science faculty Semlalia of Marrakech Cadi Ayyad University, in collaboration with the ENS of Marra-
kech and the Institute of Technology Nuclear Lisbon, Portugal. Our acknowledgments will go to
the agents of the agency of the Basin Hydraulic Tensift that contributed to the realization of this
work. We also thank the research group of Professor Paul�a Carreira at the institute of technological and nuclear Lisbon, who has done isotope analyses.
−5 −30
−25
−20
−15
−10
−4,5
21/51 363/51
390/51
380/51
28/51 93/51
27/51
386/51 346/51
148/51 272/51
Oued Ksob
11/51
15/51
149/51
327/51
M98 M24
−3,5−4
d 18O‰ V-SMOW
LMW
GMW
d 2 H
‰ V
-S M
O W
−3
2H=7.7218O+10.53 R2=0.82
Fig. 53.16 Corrélation 18O-2H dans les eaux souterraines de la zone synclinale d’Essaouira (2006)
734 S. Ouhamdouch et al.
References
Bahir, M. (2007). Isotopes et ressources en eaux en zones-arides et semi-arides: exemple du bassin
d’Es saouira (p. 175). Bahir, M., Mennani, M., Olivreira Da Silva, M., & Blavoux, B. (2003). Impact de la sècheresse sur
la ressource en eau en zone semi-aride : cas de l’aquifère barremien-aptien de la zone côtière d’Essaouira (Maroc). Paı́ses Mediterráneos: Tecnologı́a De La Intrusi�on De Agua De Mar En Acuı́feros Costeros.
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736 S. Ouhamdouch et al.
Part XIII
Environmental Technologies Related to Global Warming
Waste Management
Chapter 54
Experimental Study of Transverse Mixing of Pollutants in Trapezoidal Open Channel
Ali Mansour Lagoun and Salim Benziada
Introduction
Natural streams receive usually domestic, industrial and agricultural wastes. In
some cases, variously incidental discharges find way to rivers, which are generally
punctual and cause different problems for water quality. It is important to know the
capacity of rivers to mix those pollutants, and to determine the of mixing and
dispersing rates of rivers.
When miscible product is injected instantly into a river, it propagates and mixes
in three directions under the effect of several processes such as: diffusion, advection
and dispersion (Fischer 1966; Shen and Yapa 1995; Gharbi 1999; Hibbs et al. 1999;
Czernuszenko and Alexey 2005; Rutherford 1994; Steve and Russell 2005)
A.M. Lagoun (*) Research Laboratory of Water Sciences, Polytechnic National School of Algiers, Algiers,
Algeria
Laboratory of Environment, Water, Geomechanics and Structures, Faculty of Civil
Engineering (FGC), University of Sciences & Technology HouariBoumediene (USTHB), Bab
Ezzouar, Algiers, Algeria
Scientific and Technical Research Center on Physical and Chemical Analyses (CRAPC),
Bou-Ismail, Tipaza, Algeria
e-mail: [email protected]
S. Benziada
Research Laboratory of Water Sciences, Polytechnic National School of Algiers, Algiers,
Algeria
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_54
741
Transverse Mixing
The mixing term is reserved to express the global result of a miscible fluid transportation processes without accounting mechanism sources (Gharbi 1999).
Generally, the term of the transverse mixing refers to the lateral spread of
contaminants (horizontal) caused by turbulence (Fischer and John 1979; Rutherford
1994; Van Prooijen and Uijttewaal 2005) (Fig. 54.1).
Notion of Mixing Zones
Generally, Pollutants transport processes is consisted of three distinct areas (Fischer
1967; Yotsukura et al. 1976; Jobson 1997; Jabour 2006) which are:
Initial Mixing Zone: where the process is effected in the three dimensions of
space, this area is achieved relatively very quickly since the water depth is often less
than the width of the watercourse (Demetracopoulos and Stelan 1983a, b; Ruther-
ford 1994; Sanchez-Cabeza and Pujol 1999).
Complete Mixing Zone: The complete mixing zone begins at the limit of the
initial mixing zone. It ends when the rejected product becomes homogeneous
throughout the section of the river, in the vertical and lateral directions (Jabour
2006; Rutherford 1994).
The Far-Field Zone: It extends from the full mixing zone to the infinity.
Dispersion is one-dimensional in flow direction (Jabour 2006).
Fig. 54.1 Mixing processues in rivers (Chanson 2004)
742 A.M. Lagoun and S. Benziada
Experimental Setup and Procedures
Tests were performed in the Research Laboratory of Water Sciences (LRS water) at
the Polytechnic National School in Algiers, in a trapezoidal channel that was
designed specifically to study the problem of transport of pollutants in rivers,
especially transverse mixing, it consists essentially of:
Feeding System: allows adjusting the flow through block valve, and constant
level tank to maintain the flow invariable.
Trapezoidal Channel: 10 m of length, provided with:
– A triangular weir: to measure and control the flow. After calibration of the weir across flow measurement by the volumetric method according to water head at
weir, discharge is given by:
Q ¼ 1, 35:hd5=2 ð54:1Þ
– A flow stabilizer.
– An injection system of pollutant (phenol): consists of a double tanks with a
constant rate for 30 s. The injection is done at the channel center.
– A sampling system for each 1 m longitudinally and for each 10 cm laterally
(see Figs. 54.2 and 54.3) photography of the experimental setup is shown at Fig.
54.4.
Samples for different injection scenarios have been analyzed and the concentra-
tions were determined by spectrophotometer (Table 54.1).
Feed tank
Injection system
Flow StabilizerSupport
V Notch Weir
Channel support
Fig. 54.2 3D schema of experimental setup
54 Experimental Study of Transverse Mixing of Pollutants in Trapezoidal Open. . . 743
Injection point (0,0)
cross section of channel
y=−10cm
y=−20cm
x
y y=20cm
y=10cm y=0
Fig. 54.3 Injection system and sampling points
Fig. 54.4 Photography of experimental setup (LRS. Eau, ENP)
744 A.M. Lagoun and S. Benziada
Variables Studied
(a) Discharge flow:
The most hydrodynamic variables cited in the literature are the flow dis-
charge and mean flow velocity (Gharbi 1999; Chaudhry 2008). We selected
the first variable to study it; it is a general variable that covers several
hydrodynamic parameters (velocity and Reynolds number Re), and geometric
parameters (water depth, surface width . . .). This variable has a practical advantage, since its value is relatively easy to measure, with V-notch weir at
our case.
The selected flow rates studied are: 0.52, 0.79, 1.6, 1.75 and 1.95 l/s.
(b) Initial concentration of pollutant:
Three initial concentrations C0were studied: 500, 1000 and 1500 mg/l.
Results and Discussion
Flow Regimes
The different flow regimes are determined by the Reynolds number and Froude
number as follows:
Reynolds Number: Is defined as the ratio of inertial forces to viscous forces (Lencastre 2005; Gualtieri and Dragutin 2008):
Re ¼ UDh ν
ð54:2Þ
Flow regimes are classified according Reynolds number as follows: Re < 2000: laminar flow, 2000<Re< 4000: transient flow, Re > 4000: turbulent flow (Ernest and Horace 1996).
Table 54.1 Summary of flume characteristics
Designation Parameters Values
Channel Form Trapezoidal
Bed slope [%] 5
Length [m] 10,4
Bottom width [m] 0,4
Side slope [�] 60 Slope head [cm] 50
Weir Form Triangular (V notch)
Notch angle [�] 90 Crest elevation [cm] 10
54 Experimental Study of Transverse Mixing of Pollutants in Trapezoidal Open. . . 745
Froude Number: Is the ratio between the forces of inertia and forces of gravities:
Fr ¼ Uffiffiffiffiffiffiffiffiffiffiffi g� hp ð54:3Þ
Flow regimes are classified according Froude number as follows: Fr> 1: super- critical flow, Fr< 1: subcritical flow, Fr¼ 1: critical flow (Dingman 2009).
Flow regimes for the different flow rates examined are shown in Table 54.2.
Transverse Concentration Profiles
Lateral (horizontal) concentration evolution of phenol according time, at 2 m of
injection point of phenol with C0¼ 500 mg/l, for different flows, are given at Figs. 54.5 and 54.6.
Remarks and Interpretation
Transverse concentration profiles are identical for the two symmetrical point from
center of flow direction (y¼ 20 cm and y¼�20 cm/ y¼ 10 cm and y¼�10 cm), it shows that the pollutant injected at the center of channel is mixed to both lateral
sides of the channel (symmetric concentration profile); it is the effect of the
Table 54.2 Flow regimes according Reynolds number Re and Froude number Fr
Q [l/s] U [m/s] Re Fr Flow regimes
0.52 0.008 2848.03 0.006 Subcritical and transient
0.79 0.011 4220.03 0.009 Subcritical and turbulent
1.60 0.019 8144.88 0.015 Subcritical and turbulent
1.75 0.021 8830.58 0.016 Subcritical and turbulent
1.95 0.023 9754.51 0.017 Subcritical and turbulent
20
15
10
5
0 0 100 200 300
y=-20cm y=-10cm
y=10cm y=20cm
y=0
Time (s)
C o
n ce
n tr
at io
n (m
g /l
)
Fig. 54.5 Evolution of concentration profiles of
phenol in time for different
transverse distances at
x¼ 2 m—Q¼ 0,52 l/s, C0¼ 500 mg/l— Instantaneous injection
746 A.M. Lagoun and S. Benziada
horizontal velocity profile, which is not yet well defined (Chaudhry 2008; Gharbi
1999; Chanson 2004), but it is maximal at center (y¼ 0) and minimum at both banks of the canal.
Transverse Concentration Profiles Evolution at Downstream in Flow Direction
The concentration profiles obtained experimentally with deferent transverse dis-
tances (y¼�20 cm, y¼�10 cm, y¼ 0, y¼ 10 cm and y¼ 20 cm), at different distances from the injection point in downstream (x-direction) for a flow rate
Q¼ 0.52 l/s, with an injection of phenol with initial concentration C0¼ 500 mg/l, are shown in Figs. 54.7, 54.8, 54.9, and 54.10.
6
5
4
3
2
1
0
C o
n ce
n tr
at io
n (m
g /l
)
0 50 100 150 Time (s)
y=-20cm y=-10cm
y=10cm y=20cm
y=0
Fig. 54.6 Evolution of concentration profiles of
phenol in time for different
transverse distances at
x¼ 2 m—Q¼ 1,95 l/s, C0¼ 500 mg/l— Instantaneous injection
Fig. 54.7 Evolution of concentration profiles of
phenol in time for different
transverse distances at
x¼ 1 m—Q¼ 0,52 l/s, C0¼ 500 mg/l— Instantaneous injection
54 Experimental Study of Transverse Mixing of Pollutants in Trapezoidal Open. . . 747
Fig. 54.8 Evolution of concentration profiles of
phenol in time for different
transverse distances at
x¼ 2 m—Q¼ 0,52 l/s, C0¼ 500 mg/l— Instantaneous injection
Fig. 54.9 Evolution of concentration profiles of
phenol in time for different
transverse distances at
x¼ 5 m—Q¼ 0,52 l/s, C0¼ 500 mg/l— Instantaneous injection
Fig. 54.10 Evolution of concentration profiles of
phenol in time for different
transverse distances at
x¼ 6 m—Q¼ 0,52 l/s, C0¼ 500 mg/l— Instantaneous injection
748 A.M. Lagoun and S. Benziada
Remarks and Interpretation
From Figs. 54.7–54.10, we note that:
(a) There has a cloud movement of the pollutant (phenol) in the flow direction
(x direction) by the flow velocity effect; it is the process of advection. (b) There is a significant gradient of concentration profiles for different horizontal
points, concentrations are maximal at the center of the channel and becomes
less important for both boundaries of the channel (Figs. 54.7 and 54.8). Away
from the injection site at downstream, concentration profiles gradient becomes
less important (Figs. 54.9 and 54.10), and concentration started to be uniform
throughout the section of the channel at transverse direction (Fig. 54.10), this
is explained by the manifestation the transverse mixing of phenol.
Effect of Flow Discharge and Turbulence Phenomena:
Remarks and Interpretation
From Figs. 54.11–54.13 below, at different point in the downstream of injection
point, we note that concentration profiles for different horizontal distances (y) are
more homogeneous for flow with discharge Q¼ 1.95 l/s than for Q¼ 0.52 l/s. this means that the contaminant has been completely mixed at transverse direction,
concentration distribution becomes homogeneous and uniform in the cross section
of flow. This is can be explained by rate of turbulence that increase with flow
discharge, turbulent diffusion will be important that increase transverse mixing rate.
Fig. 54.11 Concentration Profiles for different transverse distances (y) at x¼ 3 m for Q¼ 0,52 l/s and Q¼ 1,95 l/s, C0¼ 500 mg/l
54 Experimental Study of Transverse Mixing of Pollutants in Trapezoidal Open. . . 749
Effect of Pollutant Quantity (Initial Phenol Concentration)
To determine the influence of the initial concentration on the transverse mixing,
making a comparative analysis between the concentration profiles obtained in
(x¼ 6 m, x¼ 7 m and x¼ 8 m) and at several transverse distances (y), for flow Discharge Q¼ 0.52 l/s for two initial concentrations C0¼ 500 mg/l and C0¼ 1500 mg/l:
Fig. 54.12 Concentration Profiles for different transverse distances (y) at x¼ 8 m for Q¼ 0,52 l/s and Q¼ 1,95 l/s, C0¼ 500 mg/l
Fig. 54.13 Concentrations profiles observed for different transverse distances (y) at x¼ 6 m for flow discharge Q¼ 0.52 l/s, for C0¼ 500 mg/l and C0¼ 1500 mg/l
750 A.M. Lagoun and S. Benziada
Remarks and Interpretation
From Figs. 54.14 and 54.15, we remark that the concentration profiles gradient for
different transverse distances is more important for an injection of phenol with
C0¼ 1500 mg/l that for C0¼ 500 mg/l, where the quantity of pollution has been well mixed, and the concentration distribution is more homogeneous and uniform
laterally for phenol injection C0¼ 500 mg/l then C0¼ 1500 mg/l. Mixing favors low amount.
Fig. 54.14 Concentrations Profiles observed for different transverse distances (y) at x¼ 7 m for flow discharge Q¼ 0.52 l/s, for C0¼ 500 mg/l and C0¼ 1500 mg/l
Fig. 54.15 Concentrations Profiles observed for different transverse distances (y) at x¼ 8m for flow discharge Q¼ 0.52 l/s, for C0¼ 500 mg/l and C0¼ 1500 mg/l
54 Experimental Study of Transverse Mixing of Pollutants in Trapezoidal Open. . . 751
Conclusion
Experimental model of flume designed at Research Laboratory of Water Sciences at
National Polytechnical School, and analyses of concentration profiles obtained
from several tests, have allowed to well study transverse mixing and to define the
mechanisms that govern it (advection with flow velocity and propagation with
velocity profile, turbulent diffusion).
Concentration profiles examination for different transverses sections at several
point in downstream allowed to understand the transverse mixing processes, to
distinguish the mixing zones and shows the effect of flow discharge in the
advection rate.
Flow discharge has a great effect on transverse mixing, turbulent diffusion that
becomes predominate away from injection area is accentuated with increasing flow
discharge, with growth the transverse mixing rate.
Pollutants and contamination rejected at flow will be easily mixed when their
amount and concentrations were low.
Nomenclature
C Pollutant Concentration, mg/l
Dh Hydraulic diameter, m
Do Optical density
g Gravity, m/s2
h Hydraulic depth, m
hd Head, m
Q Flow discharge (m3/s)
U Flow velocity (m/s)
Dimensionless Numbers
Fr Froude number
Re Reynolds number
Greek Letters
ν Cinematic viscosity of water, m2/s
752 A.M. Lagoun and S. Benziada
References
Chanson, H. (2004). Environmental hydraulics of open channel flow. Library of Congress Cataloguing in Publication Data, 423p.
Chaudhry, M. H. (2008). Open channel flow (2nd ed., 523p). Library of Congress, Control Number: 2007936602. New York: Springer.
Czernuszenko, W., & Alexey, R. (2005). Three-dimensional model of flow and mixing processes
in open channels. InWater quality hazards and dispersion of pollutants (pp. 35–54). Library of Congress Cataloging-in-Publication Data. New York: Springer.
Demetracopoulos, A. C., & Stelan, H. G. (1983a). Transverse mixing in wide and shallow rivers:
Case study. Journal of Environment Engineering, 109(3), 685–699. Demetracopoulos, A. C., & Stelan, H. G. (1983b). Model of Mississipi river pool: Mass transport.
Journal of Environment Engineering, 109(5), 1006–1019. Dingman, S. L. (2009). Fluvial hydraulics. Oxford: Oxford University Press. 559p. Ernest, F. B., & Horace, W. K. (1996). Handbook of hydraulics (7th ed.). New York: McGraw-
Hill. 611p.
Fischer, H. B. (1966). Longitudinal dispersion in laboratory and natural streams. Report N�. KH-R-12 . Journal of Water Resources Division, 250p.
Fischer, H. B. (1967). The mechanisms of dispersion in natural streams. Journal of Hydraulic Division. ASCE, 93(HY6), 187–215.
Fischer, H. B. & John, E. L. (1979).Mixing in inland and coastal waters. Academic Press. Library of Congress Cataloging in Publication Data, 458p.
Gharbi, S. (1999). Évaluation des coefficients de mélange longitudinal et transversal des polluants
dans les cours d’eau: proposition de nouvelles formules. Thèse Doctorat �a l’université Laval, Québec, 197p.
Gualtieri, C., & Dragutin, T. M. (2008). Fluid mechanics in environmental interfaces, Taylor & Francis e-Library, 332p.
Hibbs, D., Gulliver, J., Voller, V., & Chen, Y. F. (1999). An aqueous concentration model for
riverine spills. Journal of Hazardous Materials, A64, 37–53. Jabour, D. (2006). Etude expérimentale et modélisation de la dispersion en champ lointain suite �a
un rejet accidentel d’un polluant miscible dans un cours d’eau. Application �a la gestion de crise. Thèse Doctorat �a l’Université de Provence, 246p.
Jobson, H. E. (1997). Predicting travel time and dispersion in rivers and streams. Journal of Hydraulics Engineering. ASCE, 123(11), 971–978.
Lencastre, A. (2005). Hydraulique Général. Edition Eyrolles, 633p. Rutherford, J. C. (1994). River mixing. New York: Willey. 347p. Sanchez-Cabeza, J. A., & Pujol, L. (1999). Study on the hydrodynamic of the Ebro River lower
course using tritium as radiotracer. Water Research, 33(10), 2345–2356. Shen, H. T., & Yapa, P. D. (1995). A simulation model for chemical spills in the upper St
Lawarence River. Journal of Great Lakes Research, 21(10), 652–664. Steve, W., & Russell, M. (2005). On the theoretical prediction of longitudinal dispersion coeffi-
cients in a compound channel. In Water quality hazards and dispersion of pollutants (pp. 69–84). Library of Congress Cataloging-in-Publication Data. New York: Springer.
Van Prooijen, B. G., & Uijttewaal, W. S. J. (2005). Horizontal mixing in shallow flows; Physical
aspects and numerical modelling. In Water quality hazards and dispersion of pollutants (pp 55–68). Library of Congress Cataloging-in-Publication Data. New York: Springer.
54 Experimental Study of Transverse Mixing of Pollutants in Trapezoidal Open. . . 753
Chapter 55
Elimination of Micropollutent Lysine Acetylsalicylate by Adsorption on Natural and Synthetical Supports
Amel Djouadi and Fatiha Bentahar
Introduction
The existence of several micropollutents in wastewater has been long identified in
broad categories in persistent organic pollutants that remain active after conven-
tional wastewater treatment. This study conducts a biotechnological strategy, the
adsorption phenomena, using natural supports as algae, black tea, or synthetical
supports as the powered activated carbon or the titan oxide. Its main focus is to
produce water that may be reutilized after treatment (Gupta and Rastogi 2008).
Adsorption phenomena have been identified for its ability to degrade
micropollutents. The pollutant, a common painkiller, acetylsalicylic acid also
goes by the name aspirin. Lysine acetylsalicylate is a slightly different molecule
in structure to the original aspirin molecule, but scientists still use the name aspirin
to refer to it (Aronson 2006).
Aspirin Properties
Lysine acetylsalicylate is an analgesic substance. Its different properties are the
following:
• Formule: C9H8O4 • Poids moléculaire: 180.1574
• Structure Chimique
A. Djouadi (*) • F. Bentahar Laboratoire de phénomènes de transfert, Faculté de Génie des Procèdes et de Génie
Mécanique, USTHB, Bab Ezzouar, BP 32 El Alia, 16111 Alger, Algeria
e-mail: [email protected]; [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_55
755
Method and Procedure
A UV-Vis Absorbance Spectroscopy is used in this experiment in order to deter-
mine the absorbance of the sample and, in turn, determine purity. This is done by
weighing out a carefully measured amount of product and fully dissolving it in a
certain amount of water. If some of this resulting solution is placed in a cuvette and
is analyzed by the UV-Vis machine, it is then possible to determine the concentra-
tion of the dissolved substance from the given absorbance values using Beer’s law. The IR analysis is established to determine the characterization of each utilized
adsorbent giving their own absorbance bands and to identify the experimental
adsorption protocol (Sarat Chandra et al. 2015; Salima et al. 2013). The parametric
study is based on varying the initial concentration of the adsorbate, Lysine acetyl-
salicylate, and the temperature of the aqueous solution, pH and the mass of
adsorbent. The obtained results are summarized giving the adsorption efficiencies
of these adsorbents for the degradation of this adsorbate: The activated carbon is
considered as the best one followed by titan oxide, algae and black tea (Fig. 55.1).
Fig. 55.1 Absorbance versus wavelength
756 A. Djouadi and F. Bentahar
Results and Discussion
The obtained results are summarized giving the adsorption efficiencies of these
adsorbents for the degradation of this adsorbate: The activated carbon is considered
as the best one followed by titan oxide, algae and black tea. The adsorption
isotherms of each couple (adsorbate-adsorbent) resulting from experimental data
show that they describe well the model of Langmuir with the coefficient of
correlation R2 equal to 0.996. The kinetic model pseudo-second order represents
faithfully the experimental results, coefficient of correlation R2¼ 0.996. The ther- modynamic study has revealed that the adsorption of Lysine acetylsalicylate on the
natural supports is an exothermic reaction characterized by an increase of molecular
disorder at interface solid/ adsorbate. Adsorption reaction is endergonic on natural
supports, algae and black tea but spontaneous reaction using synthetical supports,
activated carbon or titan oxide. At the end of this work, we can conclude that the
waste plant studied have an important adsorbing power of this pollutant, Aspirin.
The absorbance values of the three working standard solutions were measured,
the measured values are shown in Table 55.1.
Conclusions
The batch studies conducted in the present study provides significant information
regarding biosorption of the pollutent on green algae Spirogyra species in terms of
optimum pH and biomass dose from the aqueous solution. The studies indicate that
Spirogyra species is an effective biosorbent for Lysine acetylsalicylate removal.
The maximum biosorption capacity has been found of dry weight of biomass at an
algal dose of 0.5 g/L in 150 min of contact time with initial Lysine acetylsalicylate
concentration of 200 mg/L and optimum pH of 5.0. The Langmuir and Freundlich
adsorption model were used for the mathematical description of the biosorption of
Lysine acetylsalicylate onto algal biomass and it was found that the adsorption
equilibrium data fitted well to the Langmuir model. The biosorption of Lysine
acetylsalicylate on the algal biomass follows second-order biosorption kinetics.
With the advantage of high biosorption capacity, the biomass of Spirogyra has the
potential to be used as an efficient and economic biosorbent microorganism for the
removal of Lysine acetylsalicylate from aqueous solutions.
Table 55.1 Absorbance values of aspirin
Equivalent conc. (mg/ml) Absorbance
0.0125 0.232
0.0250 0.466
0.0501 0.942
55 Elimination of Micropollutent Lysine Acetylsalicylate by Adsorption. . . 757
References
Aronson, J. K. (2006). Lysine acetylsalicylate. In J. K. Aronson (Ed.), Meyler’s side effects of drugs: The international encyclopedia of adverse drug reactions and interactions (15 ed., p. 2179). Amsterdam: Elsevier.
Gupta, V. K., & Rastogi, A. (2008). Biosorption of lead from aqueous solutions by green algae
Spirogyra species: Kinetics and equilibrium studies. Journal of Hazardous Materials, 152(1), 407–414.
Salima, A., et al. (2013). Application of Ulva lactuca and Systoceira stricta algae-based activated
carbons to hazardous cationic dyes removal from industrial effluents.Water Research, 47(10), 3375–3388.
Sarat Chandra, T., et al. (2015). Defatted algal biomass as a non-conventional low-cost adsorbent:
Surface characterization and methylene blue adsorption characteristics. Bioresource Technol- ogy, 184, 395–404.
758 A. Djouadi and F. Bentahar
Chapter 56
Integrated System for Optimized Data Collection and processing of End of Life Tires: Case of Greece
Panagiotis Vounatsos, John Vournas, George Mavrias, and Panagiotis Grammelis
Introduction
The tires used from all types of vehicles, like private vehicles, trucks, motorbikes,
bikes, construction and agricultural machinery, turn into waste at the end of their
life cycle. According to European Tyre and Rubber Manufacturers Association
(ETRMA 2011), about 3.3 million tonnes of end of life tyres were gathered in
Europe, of which 2.5 million tonnes were recycled or recovered. In the international
scale, each year about 1 billion tyres reach the end of their life cycle. The treatment
schemes followed in order to utilize the amounts of collected End of Life Tyres
(ELT) vary (ETRA 2013). As presented in Fig. 56.1, the situation in EU is led to a
continuous increase of methods that are more environmental friendly than
landfilling which, as shown, represents less than 10% of the total treatment
methods in 2012. On the contrary, methods such as energy utilization and tyre
recycling grew the past decade to such a degree, that more than 70% of the
collected tyres are treated by one of these methods.
The material recovery applications include among others the recycling of ELTs
as rubber granulated and powder (83%), utilization in civil engineering works
(~12%), and other applications which cover the rest of the percentage. The energy
recovery options include the utilization in cement industry at a devastating per-
centage of 91% and the majority of the rest of the quantities are used for electricity
P. Vounatsos (*) • P. Grammelis Chemical Process and Energy Resources Institute (ISFTA Sector), Centre for Research and
Technology-Hellas, 6th Km, Charilaou-Thermi Road, 57001 Thermi-Thessaloniki, Greece
e-mail: [email protected]
J. Vournas
Motion Hellas Ltd., 8, Philippou Litsa Str., Halandri, 15234 Athens, Greece
G. Mavrias
Εcoelastika SA, 14 Sorou Str., Marousi, 15125 Athens, Greece
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_56
759
generation (ETRMA 2014). Likewise, as presented from the Rubber Manufacturers
Association (Rubber Manufacturers Association 2013) the percentage of end of life
tires that is led to landfill is reduced to around 12,6%, while the percentage of tyres
utilized in energy or recycling sector (as Tyre-Derived Fuel, Ground Rubber and
Civil Engineering) covers more than 70%. The available data are presented in
Table 56.1.
As far as the best treatment methods for ELT is concerned, it has been a case of
study from many different teams around the world in terms of financial and
environmental viability and sustainability. Xingfu et al. (2010) compared four tire
treatment methods in China, were it was found that the most eco-effective ELT
treatment technology is pyrolysis (with product recovery) followed by dynamic
devulcanization and ambient grinding. It is noted that in future, ambient grinding
for crumb rubber may be more advantageous with less energy consumption and less
emissions of pollutants. Moreover, regarding the pyrolysis process, the viability
depends on the variation of the prices that the products will be sold in the future.
The work elaborated from Corti and Lombardi (2004) supports the aforementioned
utilizing life cycle assessment (LCA) tools, they found that the use of ELT as fuel
substitute in cement kilns and in Waste to Energy (WTE) processes allow better
environmental behavior than other alternatives. More specifically cryogenic and
mechanical pulverization of ELT for reuse as filling materials presented the worst
results of environmental impact comparing to all other treatment methods. Pyrol-
ysis was studied and is proposed as an alternative method for waste tyres treatment
(Williams 2013), proving that high added value products can derive from this
treatment method. Sometimes the produced products may require upgrading in
order to fit in specific standards for commercial use.
Fig. 56.1 End of Life Tyres treatment schemes in EU
760 P. Vounatsos et al.
Samolada and Zabaniotou (2012) studied the application of pyrolysis in Greece
and found that it is environmentally and financial a more sound application from
combustion-incineration (which is a destructive one). Specifically, pyrolysis can be
considerably attractive if all of the final products are effectively used. It was also
studied from Zabaniotou et al. (Zabaniotou et al. 2014), the barriers and drivers for
ELT pyrolysis in industrial application, and it was noted that the current EU
legislation prevents the implementation of large scale pyrolysis plants. As another
means for waste ELT utilization, the production of acoustic material from tire fluff
was studied (Jimenez-Espadafor et al. 2011) and it was found that it is a technically
possible and sound approach.
Apart from the studying of the after use treatment methods, there have been
studies for the replacement of metal parts (alumimium) of tires with other rubber or
plastic parts, in order to improve the carbon footprint depending on the final
treatment method that will be used. Specifically, it was found that aluminum
wore is better for landfilling while plastic and rubber parts are far better for thermal
utilization (Simoes et al. 2013). However Arroyo et al. (2011) found that steel
corrosion is the main source of heat production in Tires that have been landfilled or
in tire derived aggregate that is actually ELT that have been reduced in size and
used as lightweight fill alternative solution. This leads to possibilities of occurring
uncontrolled fires in landfills. Shakya et al. (2008) studied the emissions of
uncontrolled open-air burning of waste vehicle tyres, as happens in landfills. It
was found that CO and SO2 emissions were significantly higher than controlled
thermal utilization of tyres. Moreover the emission of other pollutants such as NO2,
CO2, polyaromatic hydrocarbons and smoke were also higher than controlled
utilization in specially designed facilities.
As presented from all of the aforementioned studies, all of the technologies and
treatment schemes present advantages and disadvantages. It was clearly observed
that despite the wide technological study for environmental and financial viability,
Table 56.1 Market trends in U.S.
Product (thousand tons) 2005 2007 2009
Tire-derived fuel 2144.64 2484.36 2084.75
Ground rubber 552.51 789.09 1354.17
Land disposed 590.81 593.98 653.38
Used tires – – 371.25
Civil engineering 639.99 561.56 284.92
Reclamation projects – 132.58 130
Exported 111.99 102.08 102.1
Baled tires/market – – 27.79
Electric arc furnace 18.88 27.14 27.1
Baled/no market 42.22 9.31 15.57
Agricultural 47.59 7.13 7.1
Punched/stamped 10.51 1.85 1.9
Generated 4410.73 4595.72 5170.5
Land disposed/generated 13.39% 12.92% 12.64%
56 Integrated System for Optimized Data Collection and processing. . . 761
there is not a widely accepted scheme or combination of technologies in order to
achieve the optimum treatment of ELTs. There are some studies (Uruburu
et al. 2013; Ene and Ozturk 2015; Subulan et al. 2015) were the product recovery
operations network as well as the final treatment for environmental optimization
has been investigated. As presented in these studies the first step is data collection,
in order to acquire certain parameters for processing.
Scope of the present study is to present a model for optimized data collection and
processing of end of life tires produced in Greece. This will lead to an integrated
system for controlling the fate of ELT, leading the treatment to most environmental
friendly solutions and therefore reducing the emissions and pollution created from
ELT utilization.
Methodology
In Greece the products from ELT treatment can be utilized in new products and
replace in some cases other raw material with equal or better properties. In the
following table (Table 56.2) the tyres categories that are collected in Greece are
presented.
The monitoring of data from the collection, transportation and final utilization of
end of life tyres is organized from ECOELASTIKA S.A. which is the Greek body
responsible for tyres recovery. Afterwards, the data are registered in a designed
database. Each party that collaborates with Ecoelastika, fills in periodically (every
week) an electronic file in which the following parameters are detailed:
• Time of collection
• The collection point
• Tyre category and quantities of used tyres per collection point
• The tyre quantities carried forward to the final users
Table 56.2 Tyres Categories that are collected in Greece
Description
Mean weight of
each tyre
Category
A0 – Passenger car tires (passenger tires and tires 4� 4) – Commercial vehicle tires
– Conventional (diagonal) agricultural tractor tyres for front
wheels
– Tyres for industrial lift trucks
8 kg
Category
B0 – Commercial vehicle tires with nominal (inner) rim diameter
greater than or equal to a certain diameter
– Agricultural tractor tyres for rear drive wheels
– Tires for industrial lift trucks with nominal (inner) rim
diameter greater than a certain diameter
– Tires for earthmoving vehicles
50 kg
Category
C0 – Motorcycle tires 2,5 kg
762 P. Vounatsos et al.
The database can afterwards provide information regarding the following points:
• The collected amounts in pieces or mass per region, for specific periods
• The frequency of transportation from certain collection points
• The collected quantities per collection point for specific periods
• The number of serviced collection points
• The amounts of tyres stored in temporary storages
• The amounts of utilized (recycled, thermal utilization) tyres in final users
The active collection points have been reduced in the latter years. From 3093
active points in 2010 only 2603 remain in operation in 2014.
The final users vary depending on the treatment method and include:
1. Mechanical grinding
2. Recycling
3. Utilization in construction projects, and
4. Thermal utilization
From the above end users 51.55% end in material recovery, 28.21% end in
Energy Recovery, while the rest 20.24% end as Tyre Derived Fuels (TDF). The
main products from the recovered tyres include textiles, wire, shredded and crumb
rubber. The percentages that derive from the mechanical grinding treatment is
presented in Fig. 56.2.
However, the business as usual may present deviations between the real data and
the ones collected. This produces two weaknesses. The first is that the calculations
derived from the database may not fully depict the reality and the second is that it is
not real time and automated. These reasons are the source for delays in processing
of the data and decision making for optimum ELT treatment options.
Therefore the data collection system determines the user requirements, which
include the following:
• Procedures for production and quality
• Integration of the Green WTMS system with other systems
Fig. 56.2 Products from mechanical grinding
process
56 Integrated System for Optimized Data Collection and processing. . . 763
• List the number and types of relevant equipment
• System size including spare capacity e.g., number of workstations
• Requirements for data presentation, records and reports
• Any networking requirements to local/wide area networks LANs/WANs
• Communication links
An automated online system will be installed in the final users, with an auto-
mated weighing system which will continuously communicate with the central
database in order to inform real time about the tyres received and about to be
treated. The online system will be composed of a network of stations installed in the
weight bridges of end users which will directly communicate with the server
located in Ecoelastika S.A. providing detailed information on:
• Mixed, net weight and tare of each ELT load that is input or output of the final
user plants for end of life tyres utilization
• Information on the trucks transporting the ELTs entering/leaving end use plant
areas (e.g. registration number, net truck volume, photos)
• Time and day of each transaction
Moreover photos of the front and the rear of each truck will be taken during the
first and second weighting (mixed weight and tare) of each truck that enters or
leaves the final use plant areas.
Utilizing this type of systems, the capacity is provided in order to:
• Online check the quantities of whole tyres that enter or leave the end use
facilities
• Check the quantities of final or intermediate products that leave from the end use
facilities in order to be sold
• Crosschecking the data that are gathered through the manual system of
weighting the loads and sending the data via a form to the system manager
(Ecoelastika S.A.)
The loads will be registered as following:
1. Input load of whole end of life tyres
2. Output load
(a) Shredded tyres
(b) Tyre crumb
(c) Wire
(d) Textile
Moreover information will be included for the user that will receive the load
exiting the facility, and for the type of final treatment.
764 P. Vounatsos et al.
Results and Discussion
Taking into consideration the requirements of the data collection system designed,
a demonstration was implemented in an already existing tyre recycling plant
located in North Greece. The incoming material (end of life tires) are brought in
the plant through closed trucks. The trucks leaving the plant and carrying the
products are mostly three-axle or four-axle vehicles with open or closed containers
and lifting hook type vehicles with trailers (hook lifts). The plant is divided in six
different modules, which are the following:
1. Shredding module: It is consisted of a tyre shredder and a separator for the shredding product
2. Grinding module: It is consisted of two grinders for the reduction of the mean size of the tyres leaving the shredder
3. Metal separation: It is consisted of two stage magnetic separation 4. Module for tire crumb milling: It is consisted of two mills 5. Textile separation module: it is consisted of a series of aspirators and air filters 6. Sieving and packaging module: It is consisted of machinery were the separation
in different categories of final products takes place, according to particle size of
the product
The designed system was studied in order to include 32 different requirements as
they were set from the users. The more important of them were the following:
1. Potential for a detailed recording of all sensors, metering and measurement
systems in the database
2. Potential for continuous and automatic recording of the measurements for the
existing analogue and digital signals
3. Capability to connect with RFID readers
4. Ability to connect to message boards
5. Ability to connect to cameras for photographing vehicles
6. Capacity to connect with photocells for vehicle presence control
7. Ability to connect to traffic lights for the management of incoming and exiting
vehicles
8. It must be based on internet/intranet architecture, operate in a Windows
environment and be based on a GUI
9. The database in which the data will be saved and inserted will be SQL
10. It must provide the opportunity for continuous monitoring and presentation of
the measurements in a PC, and give the results for all the previous periods
11. Capability to record the following data on input and output vehicles
(a) Vehicle, type, owner
(b) Date, time and system operator
(c) Mix weight, net and tare
(d) Collector
56 Integrated System for Optimized Data Collection and processing. . . 765
In the entrance of the plant, the control room as well as the weight bridge for
weighting the vehicles is located. The weight bridge is electronic industrial type
with reinforced structure, according to European Regulations. It is connected
through an electronic alphanumeric weighting scale which is installed in the control
room. In Fig. 56.3, the weight bridge installed is presented.
The weight bridge was made to communicate with the system that was described
before and gather, store and transmit the gathered information. In Fig. 56.4 the data
acquisition system with the online statistic analysis is presented.
Fig. 56.3 Weight bridge installed in plant in order to
collect and transmit
online data
766 P. Vounatsos et al.
Fig. 56.4 Weight bridge installed in plant in order to collect and transmit online data
56 Integrated System for Optimized Data Collection and processing. . . 767
Conclusions
The installation and operation of a data acquisition and processing system was
found to be critical for the implementation of the first stage of an integrated control
of End of Life Tyres treatment. As presented, the integration of a data recording
system was implemented in a weight bridge located in a ELT treatment plant on the
Northern Greece. Its purpose was to record and transmit data relevant with the type
and quantities of the input stream for treatment, as well as the output stream, led to
the final users. The first demonstration of such a holistic system was successful.
Acknowledgement The support of the Greek National Strategic Reference Framework 2007–2013 is gratefully acknowledged. More specifically the project GreenWTMS (contract
number: 27-BET-2013) in the framework of the Program for Development of Industrial Research
and Technology 2013.
References
Arroyo, M., San Martin, I., Olivella, S., & Saaltink, M. W. (2011). Evaluation of self-combustion
risk in tire derived aggregate fills. Waste Management, 31, 2133–2141. Corti, A., & Lombardi, L. (2004). End life tyres: Alternative final disposal processes compared by
LCA. Energy, 29, 2089–2108. Ene, S., & Ozturk, N. (2015). Network modeling for reverse flows of end-of-life vehicles. Waste
Management, 38, 284–296. European Tyre and Rubber Manufacturers Association. (2011). End of life tyres: A valuable
resource with growing potential (2011 ed.). European Tyre & Rubber Manufacturers’ Association. Annual report 2013/2014. Jimenez-Espadafor, F. J., Villanueva, J. A. B., Garcia, M. T., Trujillo, E. C., & Blanco, A. M.
(2011). Optimal design of acoustic material from tire fluff. Materials and Design, 32, 3608–3616.
Rubber Manufacturers Association. (2013, September). U.S. Scrap Tire Management Summary
2005–2009.
Samolada, M. C., & Zabaniotou, A. A. (2012). Potential application of pyrolysis for the effective
valorisation of the end of life tires in Greece. Environmental Development, 4, 73–87. Shakya, P. R., Shrestha, P., Tamrakar, C. S., & Bhattarai, P. K. (2008). Studies on potential
emission of hazardous gases due to uncontrolled open-air burning of waste vehicle tyres and
their possible impacts on the environment. Atmospheric Environment, 42, 6555–6559. Simoes, C. L., Simoes, R., Carvalho, J., Pontes, A. J., & Bernardo, C. A. (2013). The quest for a
sustainable product: An environmental study of tyre recyclates. Materials and Design, 52, 196–206.
Subulan, K., Tasan, A. S., & Baykasoglu, A. (2015). Designing an environmentally conscious tire
closed-loop supply chain network with multiple recovery options using interactive fuzzy goal
programming. Applied Mathematical Modeling, 39(9), 2661–2702. European Tyre Recycling Association: Introduction to Tyre Recycling: 2013. (2013). Twenty
years of tyre recycling in the EU.
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Uruburu, A., Ponce-Cueto, E., Cobo-Benita, J. R., & Ordieres-Mere, J. (2013). The new challenges
of end-of-life tyres management systems: A Spanish case study. Waste Management, 33, 679–688.
Williams, P. T. (2013). Pyrolysis of waste tyres: A review. Waste Management, 33, 1714–1728. Xingfu, L., Gao, Y., & Yijun, T. (2010). Comparison of end-of-life tire treatment technologies: A
Chinese case study. Waste Management, 30, 2235–2246. Zabaniotou, A., Antoniou, N., & Bruton, G. (2014). Analysis of good practices, barriers and
drivers for ELTs pyrolysis industrial application. Waste Management, 34, 2335–2346.
56 Integrated System for Optimized Data Collection and processing. . . 769
Chapter 57
Smart Recovery of Materials and Upgrade of Organic Compost and RDF in Existing Mechanical Biological Treatment Plants by Using NIR Technology
Dimitrios-Sotirios Kourkoumpas, Georgios Kontopoulos, Ioannis Vournas,
Dimitrios Koulocheris, Panagiotis Grammelis, and Emmanouel Kakaras
Introduction
The first near infra-red (NIR) sorting systems were used to process recyclable
materials in the early 1990s. Until then, hand-sorting for the separation of the
recyclables materials from the MSW had been used. Nowadays modern sorting
systems, where e.g. paper, plastics or other recyclable materials can be sorted,
cannot be run economically without near infra-red technology.
The NIR spectroscopy is applied as a quick and reliable method for the analysis
of sample mixtures during the process analysis. Regarding the working method of
the technology, the infrared radiation generated by halogen lamps is directed on the
sample surface. Specific wavelength ranges are particularly absorbed depending on
the sample material, since this is directly linked with the resonance frequency of the
excited molecules. In what concerns the radiation reflected by the sample, this is
detected as a function of the wavelength. A measurement of the sample in the
relevant wavelength band with a high spectral resolution is required, in order to get
a detailed analysis about the sample composition (Habich 2007).
Sorting systems using NIR technology have applied in the waste processing
sector in the last 15 years. Especially, such of type of automatic sorting systems are
D.-S. Kourkoumpas (*) • P. Grammelis • E. Kakaras Centre for Research & Technology Hellas/Chemical Process and Energy Resources Institute,
52, Egialias Str., Maroussi, 15125 Athens, Greece
e-mail: [email protected]; [email protected]; [email protected]
G. Kontopoulos • I. Vournas
HELECTOR S.A., 25, Ermou Str., N. Kifissia, 14564 Attica, Greece
e-mail: [email protected]
D. Koulocheris
National Technical University of Athens, 9, Heroon Polytechniou, 15780 Athens, Greece
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_57
771
applied for the separation of the different plastic fractions, in order to get high
purity materials, which means higher selling price. In the MBT plant, mechanical
separation is achieved by using several components as optical (NIR) separators,
ballistic separators and magnets. In addition a hand picking step for the removal of
heavy and large objects is found in the most of the existing MBT plants in order to
remove the heavy and large materials. For the largest part these plants operate
automatically. In order to facilitate the separation, waste is usually shredded to the
average size of a few hundred mm. The shredder is usually followed by a drum
screen, creating two waste streams of different sizes, (B€ohm et al. 2010). The aim of this paper is to present the scope of the project “Smart Recovery of
materials and upgrade of organic compost and RDF in existing mechanical biolog-
ical treatment plants by using NIR technology” funded by the GSRT.
Methodology
Scope of the Project
The scope of the project is to design, develop and integrate a Smart System for
Recovery of materials and upgrade of the organic Compost and RDF quality in
existing Mechanical Biological Treatment Plants by using NIR technology, state of
the art technology systems for automation and measurement and algorithms for
waste process and recycling optimization. The main goals for the SmartWasteTech
project are:
• the development and integration of an online monitoring software for the MBT
plant operation based on the continuous information obtained from the modern
online sensor technology
• to increase the valuable plastic fraction (PET, PE/PP, LDPE film) sorted out
from MSW, towards increasing recycling efficiency and overall environmental
performance of the plant
• the process optimization based on the Greek MSW quality
• to increase the compost quality through application of innovative technology for
sorting out inert materials (glass, inert materials) and other unwanted materials
such as heavy metals and the production of a high purity compost
• to perform continuous quality monitoring of the produced Refused Derived Fuel
to investigate the economic, feasibility and environmental benefits of the
proposed technology
• to disseminate the project results to all relevant stakeholders including among
others manufacturers and operators of waste treatment facilities, local authori-
ties, engineering and planning companies in the waste treatment sector, end
users of recycled plastics and compost
772 D.-S. Kourkoumpas et al.
Innovation Activities
Through the latest development of online sensor technology (Near Infrared, laser,
X-Ray etc.) different machines have been developed and are currently applied as
complete solutions for sorting of mixed Municipal Solid Waste. Based on this
development, modern waste treatment plants have the appropriate process technol-
ogy installed to efficiently recover valuable materials from mixed Municipal Solid
Waste (metals, specific plastic fractions like PET), while the remaining high
calorific fraction of MSW is usually led to other energy recovery processes by
producing high quality Solid Recovered Fuels (SRF) or Refused Derived Fuels
(RDF) (Nasrullah et al. 2014; Cimpan et al. 2015). Nevertheless, recently devel-
oped waste sorting techniques cannot be applied in the existing Mechanical Bio-
logical Treatment Plants (MBTs), without additional research work and carefully
planned modifications in the current waste treatment processes. Due to the difficulty
of this task, no integrated concept solution for the enhancement of environmental
performance in existing MBT plants has been developed and demonstrated up to
now. This is exactly the first innovative aspect in the present project.
This conventional type of waste treatment plants usually includes a separation
step for the fine organic fraction, which is usually followed by a biological drying
and a composting step towards the production of a material with characteristics
argued to be similar with these of organic “compost”. However, after a thor-
ough evaluation of the compost composition it can be noticed that the compost
material derived from mixed MSW has usually a high amount of inert materials and
a high concentration in heavy metals. Hence the utilization of this type of material
is rather limited, thus it cannot be promoted as fertilizer. Therefore, the goal of the
project is the upgrade of the compost quality up to a level that will be comparable
with the organic fertilizer. This will be achieved by the development and optimi-
zation of a process for sorting out inert, heavy metals and other unwanted materials,
which will be the second innovative point of the project. The particular process has
been applied for other types of waste in the past (commercial waste) but it has never
been tested for mixed MSW. Therefore, a further development of the process based
on the particular characteristics of compost derived from mixed MSW is required
and will be carried out. The remaining stream with the bigger size particles,
including packaging materials is then utilized for the production of a refused
derived fuel (RDF). Nevertheless, the particular type of RDFs, produced at MBT
plants operating with an aged technology, can hardly meet the high quality criteria
required by today’s incineration or co-incineration plants (cement, brick kilns) in terms of calorific value, chlorine content and heavy metals concentration. For this
reason, their marketability is limited and only a view of them are standardized
according to the recently published European standards (EN 15357, EN 15358, EN
15359). Furthermore, the recovery of paper and plastic fractions is a target of the
project. In specific, this type of recyclables is usually not recovered in mixed waste
treatment plants. An ambitious goal of recovering about 85% of the recyclables still
present in the packaging material stream is set. This will be achieved through the
57 Smart Recovery of Materials and Upgrade of Organic Compost and RDF. . . 773
customization of new sorting equipment and optimization based on the specific
parameters of mixed MSW, which is the third innovative point of the project.
The concept under development was implemented in the Athens Mechanical and
Biological Waste Treatment plant located in the main Athens land fill site of Ano
Liosia and operated by Helector S.A. and to the MBT plant in Larnaca, Cyprus
which was designed, constructed and operated by Helector S.A. since 2010.
The daily input stream of the Athens MBT plant is about 1200 tn of mixed
MSW. The production of RDF and compost rise to 450 t/d and 180 t/d respectively.
The recyclable fraction of the input mixed MSW is about 1.5% PET, 1.5% PE/PP,
8% recyclable paper, 9% glass and 5% metals. The proposed work intends to
provide a complete solution for the quality improvement of MBT plant’s output streams and the increase of its recycling efficiency by the application of modern,
innovative sensor and separation technology.
The technologies that were incorporated in the Integrated System
SmartWasteTech are related with industrial research (IR) and aim at obtaining
expertise by design and install:
• special electromechanical structures
• specific type and measurement sensors
• automation and control systems
• optimization algorithms for measurement and process
• quantitative and qualitative management system and evaluation assessment
models (LCA, feasibility study for environmental, social and economic benefits)
of the collected data.
The Technology
The Titech equipment uses an NIR sensor to detect the characteristic infrared
spectrum of light reflected by an illuminated object. The NIR spectrum of each
material is unique and can be used to identify specific materials and then separate
them (Fig. 57.1). The system has
• Modular design
• Modular build
Fig. 57.1 NIR technology of TITECH (TOMRA)
774 D.-S. Kourkoumpas et al.
• Maximize cost benefit process plant to product recovery
The basic characteristics of the system are:
• High tech sensors are utilized to identify objects on a conveyor belt
• High speed processing of information: material, shape, size, color, defect,
damage and location objects
• Precise sorting by air jets
The system works by scanning the material as it travels along a conveyor belt.
The PolySort UHR uses a fast near infrared analyzer along with a computer-
controlled air jet ejection system. Material is identified across the entire width of
the conveyor belt. The type of material, position and projected area of every single
object on the belt is determined by the machine. A computer then rapidly processes
the information and controls a series of air jets situated at the end of the conveyor
belt. The air jets are activated accordingly to remove the identified material from
the main product stream. The projected area determines which air jets need to be
activated and only those which the object will pass over are used. The duration for
which the air jet is active corresponds to the overall projected length of the object.
Results
NIR’s municipal waste sorting systems identify and sort grain sizes from 10 to 500 mm, separated according to preferred size ranges. These systems provide inert
material elimination of up to 95% in municipal waste, producing material suitable
for biomethanisation. Inert material, such as glass and stones, can cause significant
problems during the treatment process and therefore has to be reduced to a
minimum, while as little organic content as possible is removed. In addition,
materials such as PET, PE/PP, LDPE film etc. can be recovered successfully.
The NIR system is operated entirely by a computer with an LCD screen display
from which the system can be controlled. Most settings and functions can be
changed via the screen such as the belt speed, material selected for ejection. The
SmartWasteTech system communicates directly to the NIR in order to monitor via
a SCADA and MIS system the operating parameters. The integration of the
SmartWasteTech system in the MBT plant leads to the following results:
• Process analysis
• Real time process and material information
• Batch process and reporting
• Real time analysis and process tuning
• Input composition over a period
• Material timetable which shows how much material was detected in a period
• Distribution of the material which shows how much material was detected on
different parts of the conveyor
• Temperature and pressure
57 Smart Recovery of Materials and Upgrade of Organic Compost and RDF. . . 775
• Management
• Database capture of process and material
• Overall equipment effectiveness
The integration of the NIR technology in the MBT plant in Larnaca, operated by
Helector S.A. have increased the recovery of the material and the efficiency of the
technology performance. These results are presented in the following diagrams.
In specific, the purity of the materials are shown in Figs. 57.2 and 57.3. As it is
shown, the purity of the recovered materials are high. This means that the environ-
mental benefit is high, as well as the selling price of the materials to the recycling
industries. In Fig. 57.3, the purity of the materials in Larnaca is compared with the
green Dot system in Germany. The purity of materials is higher than the respective
purity of the German Dot system, thanks to the NIR technology applied in the plant.
The NIR online analysis has been applied successfully for the identification of
the input waste. The results are shown in Fig. 57.4. The results from NIR online
analysis are very closed to the results from the experimental analysis (mass
balancing). In summer months, there is a significant deviation of the results, since
the waste composition is quite different due to the change of the consumer’s behaviour e.g. increase of tourism.
Fig. 57.2 Indicative purity results in MBT plant at Larnaca
776 D.-S. Kourkoumpas et al.
Conclusions
The SmartWasteTech proposal, using NIR technology for recycling, improves the
operation of the existing MBT plants and the SCADA system communicates
directly to the NIR in order to monitor the process and the operating parameters.
The SmartWasteTech system can be applied in existing MBT plant, giving a
Fig. 57.3 Comparison between Larnaca’s MBT plant with a typical plant in Germany
Fig. 57.4 Composition of input waste based on NIR online analysis and experimental analysis
57 Smart Recovery of Materials and Upgrade of Organic Compost and RDF. . . 777
solution to the improvement of the final products (compost, RDF, PET, PP, etc.). In
addition, despite the fact that the input waste corresponds to mixed municipal
waste, the proposed system can recover materials in high purity. The overall
environmental footprint of the plant is improved, as well as its economic feasibility.
The identification of the input waste over a time period is also another outcome of
the proposed system. Based on this identification, appropriate configurations of the
NIR separators can be carried out, in order to maximize the recovery efficiency of
the materials, as well as to improve the final quality of the produced materials
(compost, RDF, PET, PP, etc.).
Acknowledgement The study described in this publication was financially supported by the Greek General Secretariat for Research and Technology (GSRT). The enumerated code of the
Project is 1115-BET-2013.
References
B€ohm, K., Smidt, E., Binner, E., Schwanninger, M., Tintner, J., & Lechner, P. (2010). Determi- nation of Mbt-waste reactivity – An infrared spectroscopic and multivariate statistical
approach to identify and avoid failures of biological tests. Waste Management, 30, 583–90 Cimpan, C., Maul, A., Jansen, M., Pretz, T., &Wenzel, H. (2015). ’Central sorting and recovery of
Msw recyclable materials: A review of technological state-of-the-art, cases, practice and
implications for materials recycling’. Journal of Environmental Management, 156, 181–99 Habich, U. (2007). Sensor-based sorting systems in waste. In Processing international symposium
MBT. Nasrullah, M., Vainikka, P., Hannula, J., Hurme, M., & Kärki, J. (2014). Mass, energy and material
balances of Srf production process. Part 1: SRF produced from commercial and industrial
waste. Waste Management, 34, 1398–407 TOMRA. Brochures and Guidelines for Titech equipment. http://www.tomra.com/en/solutions-
and-products/sorting-solutions/recycling.
778 D.-S. Kourkoumpas et al.
Part XIV
Securing Sustainable Mobility to Mitigate Climate Change
Transport Operation and Resilience Issues
Chapter 58
Road Transport Induced GHG Emissions Calculation for Urban Transportation Networks: The Case of Athens and Thessaloniki in Greece
Christos Samaras, Iraklis Stamos, Leonidas Ntziachristos,
Evangelos Mitsakis, Zissis Samaras, and Georgia Ayfantopoulou
Introduction
The threat of climate change is not only well recognized, but is an important item on
the political agenda of all countries due to the severity and intensity with which the
impacts are already occurring (Graus and Blomen 2008). The world is experiencing
extreme weather conditions, such as lengthy droughts, heat waves, changing rain-
fall patterns, changing seasonal patterns, severe hurricanes, etc. (IPCC 2015).
Climate change is mainly induced by human activity and is primarily caused by
the combustion of fossil fuels (coal, oil and gas). The average global temperature
has already risen by 0.8 �C since the beginning of the Industrial Revolution (NOAA 2005). According to researchers (IPCC 2015; Hare 2003), an average global
warming of 2 �C or above compared to the pre-Industrial Revolution level would result in dangerous and probably irreversible impacts in human ecosystems.
It is evident that GHG emissions are strongly related with climate change.
According to the annual European Union (EU) greenhouse gas inventory, total
GHG emissions, without Land Use, Land-Use Change and Forestry (LULUCF), in
the EU-15 decreased by 15.1% between 1990 and 2012. However, at the same time
frame, GHG emissions produced by road transport increased by 72 million tons of
CO2 equivalent. Furthermore, in 2012, the contribution of road transport alone in
C. Samaras (*) • L. Ntziachristos • Z. Samaras Laboratory of Applied Thermodynamics, Aristotle University of Thessaloniki,
54124 Thessaloniki, Greece
e-mail: [email protected]; [email protected]; [email protected]
I. Stamos • E. Mitsakis • G. Ayfantopoulou
Center for Research and Technology Hellas—Hellenic Institute of Transport,
6th Km Charilaou Thermis Road, 57001 Thessaloniki, Greece
e-mail: [email protected]; [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_58
783
the EU-15 total CO2 emissions—the main greenhouse gas—was about 24% (EEA
2014).
In respect of GHG emissions, the situation in Greece is worse than the average
EU-15; total GHG emissions—without LULUCF—were increased by 5.8%
between 1990 and 2012 (EEA 2014). The peak years were 2005 and 2007, but,
after 2007 there was a substantial decrease, mainly due to the economic crisis
(MEECC 2014). In the annual EU emissions inventory for 2012, GHG emissions in
Greece were calculated equal to 111 million tons of CO2 equivalent (EEA 2014).
The Greek Ministry of Environment, Energy and Climate Change (MEECC)
estimates that in 2010 the contribution of transport in the total national GHG
emissions was about 24.7%, making transport the second most important source
of GHG emissions (MEECC 2012). In the same report, MEECC states that approx-
imately 84% of total GHG emissions of the transport sector were derived from road
transport (83.8% for CO2, 94.5% for CH4 and 57% for N2O emissions).
From the aforementioned statistical data it is evident that road transport is a
major source of GHG emissions in Greece. In an effort to gain a clear and more
detailed understanding of the amount of GHG emitted in Greece, this paper maps
GHG pollutants in the two largest cities of the country, namely Athens and
Thessaloniki. According to the latest national census that was conducted in 2011,
the examined cities accommodate almost half of the country’s population (Hellenic Statistical Authority 2014); therefore, the calculation conducted herein will largely
reflect the national status in respect to GHG emissions.
Compared to national and European inventories, as well as to other studies
(Progiou and Ziomas 2012), this paper focuses solely on road transport. Apart
from daily GHG emissions values, the paper tries to identify the road sections
that produce the majority of emissions (hot-spots). Moreover, emphasis is given to
the hourly variation of GHG emissions, as well as to the contribution of different
vehicle categories on total emissions.
Materials and Methods
In the next section, the methodology for both traffic and emissions modelling is
analyzed. It should be highlighted that due to the lack of available data the study
focuses only on hot emissions.
Traffic Modelling
The transportation model for Athens has been developed with the PTV VISUM
software (Gentile and Noekel 2009), a traffic assignment tool for urban and regional
operational planning analysis that has been used in several studies (Stamos
et al. 2011; Ayfadopoulou et al. 2012; Mitsakis et al. 2013). The network used in
784 C. Samaras et al.
this study consists of a detailed representation of the urban and regional road
network of the metropolitan region of Athens, based on open-source GIS, fused
with traffic related parameters.
The network consists of 81.880 directed links and 36.725 nodes. The links
contain information about the number of lanes, the road type and its hierarchy in
the network, width, length, free flow speed, design and effective capacity, direction
and allowed transport systems. The link delays are calculated with the use of
volume-delay functions, the parameters of which rely on previous studies and
have been updated through travel time measurements for the purposes of the
work presented herein. The nodes contain detailed information about the junction’s geometry, allowed movements and control type of the node.
The network consists of 359 traffic analysis zones (TAZ) connected to physical
nodes of the road network via 3.468 connectors, according to their accessibility
index (Friedrich and Galster 2009), avoiding connections with nodes belonging to
high hierarchy links. The demand side is comprised by 24 hourly Origin-
Destination (OD) matrices and the travel demand for a typical weekday is within
the range of 3.8 million vehicle trips. The obtained OD matrices are corrected using
the hourly volume data measured by inductive loop detectors installed at 557 loca-
tions across the city. The OD matrix correction is performed with a fuzzy-set based
matrix correction procedure (Rosinowski 1994).
Since traffic measurements are available only at a number of locations which is
smaller than the number of trips, then the problem of determining the OD matrix
which reproduces trips that result to traffic volumes equal to the ones measured is
underdetermined. The matrix correction procedure described herein is of bi-level
nature, where at the upper level user equilibrium traffic flows are computed, subject
to the corrected OD matrices at the lower level. The upper level user equilibrium
traffic flow estimation, known as the Traffic Assignment Problem, based on
Wardrop’s user equilibrium principle (Wardrop 1952), is solved with an imple- mentation of the Linear User Cost Equilibrium algorithm (Gentile and Noekel
2009), with an average goodness-of-fit of 0.94.
A similar approach has been followed for modelling traffic in the network of
Thessaloniki. The final output concerns a large-scale model with 137.938 links,
47.838 nodes and 339 TAZ accounting for a daily total of about 1.3 million vehicle
trips. The OD matrix correction is conducted via real-time measurements of
cameras, radars and inductive loop detectors located in 37 signalized junctions of
the road network, measuring volumes at a frequency of 1.5 min. Figure 58.1 depicts
instances of the road transportation network in Athens and Thessaloniki
respectively.
Emissions Modelling
The emission calculations were performed with COPERT Micro (Samaras
et al. 2014), a specially developed version of COPERT 4 (Ntziachristos
et al. 2009) for urban areas. COPERT Micro is an average speed emissions model
58 Road Transport Induced GHG Emissions Calculation for Urban Transportation. . . 785
that is able to calculate fuel consumption, as well as several important pollutants
(CO, NOx, VOC, PM exhaust, GHG emissions and others). It is a bottom-up model,
hence, it can calculate the emissions from a single traffic link up to an entire city.
COPERT Micro was developed focusing primarily on hot exhaust emissions. It
includes 230 different vehicles categories and incorporates several emission factors
that were obtained experimentally as a function of the average vehicle speed.
The equations below summarize the main calculations conducted by COPERT
Micro during hot exhaust emissions calculation. First of all, based on the average
speed of each traffic link the corresponding emission factors are calculated for each
vehicle category and for every pollutant:
EFi, k Vð Þ ¼ f EF, i, k Vj � � ð58:1Þ
where:
EFi(V): hot exhaust emission factor per vehicle category k, for average speed V and for pollutant i [g/km]
i: pollutant of interest (CO2, N2O and CH4) fEF, i, k: polynomial function derived from measured data (as trendline); unique for
every vehicle category k and for each pollutant i
Vj: average speed of the vehicles circulating on the traffic link j [km/h]
After calculating the emission factors for all pollutants, the hot exhaust emis-
sions of the traffic link j are calculated by the formula:
Ehoti, j ¼ Lj � Nj � X
Pj, k � EFi, k Vð Þ � � ð58:2Þ
where:
Ehoti, j: hot emissions of pollutant i produced by Nj vehicles that circulate on the link j [g]
Lj: length of the traffic link j [km] Nj: number of vehicles circulating on link j
Fig. 58.1 Graphical representation of the road network in Athens (left) and Thessaloniki (right)
786 C. Samaras et al.
Pj, k: percentage of vehicles of the specific category k on the overall vehicle fleet that circulate on link j, e.g. passenger cars 0.8–1.4 l gasoline Euro 3¼ 5% etc. This is not constant, but it changes form link to link.
Finally, the total hot exhaust emissions of the pollutant i for the entire area
(Ehoti, area) are calculated by summing the emissions of individual traffic links j:
Ehoti, area ¼ X
Ehoti, j ð58:3Þ
Since the hourly activity data are available from the traffic model, the calculation
is repeated for each hour of the day and the hourly and daily emissions are
calculated for all pollutants and for all traffic links.
Results and Discussion
The results are divided into two sections. In the first one, the emissions at micro/link
level are presented upon the GIS grid, whereas in the second one, the hourly and
daily emissions for both cities are given.
Emissions on Micro Level
In general, the visual representation of emissions on GIS grid is extremely helpful
for identifying the localized hot-spots throughout a road network. This is the reason
why in Fig. 58.2 the daily CO2 hot emissions of both Athens and Thessaloniki are
Daily CO2 emissions - 2014
Daily CO2 emissions - 2014
0.1 - 385.6 0.0 - 770.9 771.0 - 2352.7 2352.8 - 4325.3 4325.4 - 7276.8 7276.9 - 12769.0
385.7 - 1229.7 1229.8 - 2328.2 2328.3 - 4385.3
4385.4 - 9806.1
Fig. 58.2 Daily CO2 hot emissions (kg) on a 100� 100 (500� 500 m2) grid for a typical weekday of October 2010 in Greater Athens Area (left) and for a typical weekday of November 2014 (right) in metropolitan area of Thessaloniki
58 Road Transport Induced GHG Emissions Calculation for Urban Transportation. . . 787
presented. It is evident that in both cities there are specific road sections—marked
with red color—that strongly affect CO2 emissions. In the case of Athens, sections
of large boulevards, such as Attica Road, Kifisou Avenue, Mesogion Avenue,
Athinon Avenue, along with Kifisias Avenue, Vouliagmenis Avenue and
Poseidonos Avenue, are major CO2 emitters. In Thessaloniki the situation is
much clearer; Inner Ring Road constitutes the major source of CO2 emissions in
the city, while large sections of Egnatia Avenue, Tsimiski Avenue and Karamanli
Avenue follow. In both cases the results are not surprising, since the number of
vehicles circulating in these boulevards is quite high, so, as a consequence, the
emissions will be high.
Since transport activity is not constant throughout the day, the local hot-spots
will vary from hour to hour. This is demonstrated in Fig. 58.3, where the off-peak
(3–4 A.M.) and peak (8–9 A.M.) CH4 hot emissions for Athens are shown upon the
GIS grid. During the off-peak hour the highest values of CH4 hot emissions are
found close to city center, mainly in Stadiou, Panepistimiou, Agiou Konstantinou
and P. Tsaldari streets, as well as in a section of Vouliagmenis Avenue near
Argyroupoli. During the rush hour in the morning, there are multiple hot-spots,
including also the off-peak hour hot-spots. Note, that although the colors in both
pictures are the same, the legends have different values.
The variation of N2O hot emissions in Thessaloniki during peak and off-peak
hours is shown in Fig. 58.4. In both cases the Inner Ring Road, again, plays the most
important role. However, late at night, the city center seems to have a significant
contribution too. More precisely, the N2O hot emissions caused by transport
activity in Egnatia and Tsimiski Avenue are quite high during the off-peak hour,
while, contrary to Athens, these hot-spots disappear in the morning (peak hour). It
should be highlighted that the Inner Ring Road is probably one of the country’s busiest highway sections. It is a dual carriageway ring road encircling most of the
urban area of Thessaloniki. It consists of two sections; the Western Ring and the
main Inner Ring. It has three lanes per direction and carries over 100.000 vehicles
per day (Ewen et al. 2009).
Off-peak CH4 emissions - 2014
Peak-hour CH4 emissions - 2014
0.000000000 - 0.001500995 0.000000000 - 0.020380227
0.020380228 - 0.048731997
0.048731998 - 0.083542174
0.083542175 - 0.127850818
0.127850819 - 0.207582387
0.001500996 - 0.004327670
0.004327671 - 0.008450395
0.008450396 - 0.017203846
0.017203847 - 0.041356440
Fig. 58.3 Off-peak—3–4 A.M.—(left) and peak—8–9 A.M.—(right) CH4 hot emissions (kg) on a 100� 100 (500� 500 m2) grid for a typical weekday of October 2010 in the Greater Athens Area
788 C. Samaras et al.
Emissions on Macro Level
Figure 58.5 shows the hourly GHG emissions for both Athens and Thessaloniki. It
is evident that GHG emissions are not constant during the day, but follow propor-
tionally the transport activity. In both cities, GHG emissions attain their highest
values during the rush hour in the morning (8–9 A.M.), when most citizens start
their typical activities (work, school etc.). Emissions decreasing until about noon
(12–1 P.M.), and, then, start rising again during afternoon (2–6 P.M.), when the
majority of people finish their activities and return back to their origin. From the
evening until late at night (6 P.M.–4 A.M.) the traffic activity drops, so do GHG
emissions. Finally, after the off-peak hour (3–4 A.M.), the emissions start increas-
ing again.
The emission patterns for both cities have many similarities. This is expected,
since most residents have similar daily schedules; they usually drive to work
between 7–9 A.M., and, after about 8 h, they drive back to their houses in the
afternoon (3 P.M.–5 P.M.). It’s worth mentioning that due to the increased leisure activities after the midnight in Thessaloniki, there is a small increase of GHG
emissions between 1 A.M. and 3 A.M., when people usually return to their
homes. Furthermore, between 9 A.M. and 1 P.M., GHG emission values in
Thessaloniki vary significantly, indicating that transport activity in the city is
more variable compared to Athens.
In the next three figures, the daily hot GHG emissions are presented both for
Athens and Thessaloniki, as well as the share of those emissions in the main vehicle
categories. Starting with CO2 in Fig. 58.6, it is evident that passenger cars are the
Off-peak N2O emissions - 2014
Peak-hour N2O emissions - 2014
0.00000 - 0.00018 0.00000 - 0.00213
0.00214 - 0.00665
0.00666 - 0.01358
0.01359 - 0.02572
0.02573 - 0.04782
0.00019 - 0.00057
0.00058 - 0.00114
0.00115 - 0.00198
0.00199 - 0.00360
Fig. 58.4 Off-peak—3–4 A.M.—(left) and peak—8–9 A.M.—(right) N2O hot emissions (kg) on a 100� 100 (500� 500 m2) grid for a typical weekday of November 2014 in metropolitan area of Thessaloniki
58 Road Transport Induced GHG Emissions Calculation for Urban Transportation. . . 789
main source of CO2 emissions in both cities. The contribution of light and heavy
duty vehicles in the case of Athens is similar—close to 15%, whereas in
Thessaloniki, light duty vehicles have more impact on CO2 emissions than heavy
140
49
42
35
28
21
14
7
0
525
175
150
125
100
75
50
25
0
450
375
300
225
150
75
0
120
100
80
60
40
20
0 1 2 3 4 5 6 7
N2O CO2CH4
N2O CO2CH4
8 9 10 11 12 13
Hour
Athens GHG Hot Emissions
Thessaloniki GHG Hot Emissions
C O
2 E
m is
si o
n s
[t ]
C O
2 E
m is
si o
n s
[t ]
N 2O
& C
H 4
E m
is si
o n
s [k
g ]
N 2O
& C
H 4
E m
is si
o n
s [k
g ]
14 15 16 17 18 19 20 21 22 23 24
1 2 3 4 5 6 7 8 9 10 11 12 13
Hour
14 15 16 17 18 19 20 21 22 23 24
Fig. 58.5 Hourly CO2, N2O and CH4 hot emissions for a typical weekday of October 2010 in Greater Athens Area (up) and for a typical weekday of November 2014 (down) in metropolitan area of Thessaloniki
790 C. Samaras et al.
duty vehicles (17.2% and 5.5% respectively). Finally, the two cities have almost
the same level of CO2 emissions coming from buses and two-wheel vehicles
(mopeds and motorcycles).
On absolute level, the daily CO2 hot emissions in Athens are three times higher
than the corresponding ones in Thessaloniki. This is in line with the number of
vehicle trips simulated with the traffic software used herein (about 3.8 and 1.3
million vehicle trips for Athens and Thessaloniki respectively). Since the vehicle
trips in the case of Athens are about three times the trips in Thessaloniki, it is
reasonable to expect that CO2 emissions in Athens will be approximately three
times the corresponding ones in Thessaloniki.
Regarding methane, the situation is similar to CO2 in respect to absolute
emission levels (Fig. 58.7). It is noteworthy that the share of two-wheel vehicles
is quite high, almost similar to the share of passenger cars. On the other hand, the
contribution of passenger cars in CH4 hot emissions in both cities has been reduced
substantially compared to CO2—almost 42% relative reduction (from 60.9% for
CO2 to 35.4% for CH4 in the case of Athens and from 68.5% to 39.6% respectively
for Thessaloniki).
8,000
7,000 7,106
Athens
CO2 Daily Hot Emissions C
O 2
E m
is si
o n
s [t
]
C O
2 E
m is
si o
n s
[t ]
CO2 Daily Hot Emissions Per Vehicle Type
Thessaloniki MOT PC LDV HDV BUS
2,385
4.4% 3.9%
68.5%
60.9%
Athens Thessaloniki
14.2% 17.2% 15.8%
5.5% 4.7% 4.8%
6,000
5,000
4,000
3,000
2,000
1,000
0
80%
70%
60%
50%
40%
30%
20%
10%
0%
Fig. 58.6 Daily CO2 hot emissions (left) and contribution of each vehicle category (right) for a typical weekday of October 2010 in Greater Athens Area and for a typical weekday of November
2014 in metropolitan area of Thessaloniki
CH4 Daily Hot Emissions CH4 Daily Hot Emissions Per Vehicle Type 2,000 45%
40%
35%
30%
25%
20%
15%
10%
5%
0%
1,800
1,600 1,400
1,200
1,000
800
600
400
200
0
1,740
33.6% 31.8%
35.4%
39.6%
22.6%
10.6%
3.5% 2.4% 2.6%
18.1%
604
MOT PC LDV HDV BUSAthens Thessaloniki
Athens Thessaloniki
C H
4 E
m is
si o
n s
[k g
]
C H
4 E
m is
si o
n s
[% ]
Fig. 58.7 Daily CH4 hot emissions (left) and contribution of each vehicle category (right) for a typical weekday of October 2010 in Greater Athens Area and for a typical weekday of November
2014 in metropolitan area of Thessaloniki
58 Road Transport Induced GHG Emissions Calculation for Urban Transportation. . . 791
The two-wheel vehicles are responsible for almost one third of CH4 hot emis-
sions in each city. This is due to the fact that two-wheel vehicles have higher CH4 hot emission factors compared with other vehicle types (Ntziachristos and Samaras
2014). Furthermore, another important factor is the relative high share of two-wheel
vehicles on the average fleet composition, which for the case of Athens is about
19.8%, and, for Thessaloniki is 12.3%.
The absolute levels of the last GHG pollutant of interest-N2O-follow the trend of
CO2 and CH4 emissions (Fig. 58.8); N2O hot emissions in Athens are about 2.7
times the respective ones in Thessaloniki. However, when daily N2O hot emissions
are split into the main vehicle categories, the percentages of passenger cars and
light duty vehicles are higher than in the CO2 case. The shares in both cities are
relatively similar except for heavy duty vehicles, which in the case of Athens are
much higher (10.6% compared with 3.3% in Thessaloniki).
The previous charts depict the recent situation in the two largest cities of Greece
in respect to GHG emissions. Since the country is away from its Kyoto targets (EEA
2014), measures should be taken in order to reduce GHG emissions and meet these
targets. In road transport the measures should focus on alleviating the traffic in main
boulevards of the cities, since they constitute the major sources of pollution.
Moreover, the adoption of stricter policies and cleaner technologies in passenger
cars, light duty vehicles (i.e. new Euro 6 regulation), as well as in two-wheel
vehicles will be beneficial for GHG emissions.
Conclusions
Climate change is already perceptible in Greece. There are clear indications of
warming in the country from the early 1990s (Feidas and Lalas 2001); gradually
strengthened and record-breaking hot summers days are an increasingly regular
occurrence. Road transport in Greece constitutes a significant source of GHG
emissions, and it consequently affects the local climate change.
N 2O
E m
is si
o n
s [%
]
N 2O
E m
is si
o n
s [k
g ]
80%
70%
60%
50%
40%
30%
20%
10%
0%
350
300
250
200
150
100
50
0 Athens Thessaloniki
112
307
MOT PC LDV HDV BUS
70.9% 66.8%
2.5% 2.2%
18.3% 21.7%
10.6%
3.3% 1.8%1.9%
Athens Thessaloniki
N2O Daily Hot Emissions Per Vehicle TypeN2O Daily Hot Emissions
Fig. 58.8 Daily N2O hot emissions (left) and contribution of each vehicle category (right) for a typical weekday of October 2010 in Greater Athens Area and for a typical weekday of November
2014 in metropolitan area of Thessaloniki
792 C. Samaras et al.
In this paper, the hourly and daily GHG hot emissions were examined in both
Athens and Thessaloniki, the two more heavily-populated cities in Greece. In both
case studies the results at link level revealed the local pollution hot-spots and the
high-emission links, which usually lie along the main urban highways. These
hot-spots are not constant, but changing throughout the day, proportionally follow-
ing transport activity. During the rush hour in the morning (8–9 A.M.), GHG
emission attain their highest values, while the opposite occurs late at night (3–4
A.M.).
Passenger cars, and, secondarily, light duty vehicles are the vehicle categories
which mainly contribute to GHG in the cities examined. Moreover, two-wheel
vehicles should be also taken into account in respect of CH4 emissions. Thus, apart
from alleviating the traffic in the large arterials, the application of stricter policies
and cleaner technologies in these vehicle categories should be also examined,
considering that the country should meet its Kyoto targets.
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Feidas, H., Lalas, D. (2001). Climatic changes in Mediterranean and Greece: A critical review. In:
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Mitsakis, E., Stamos, I., Salanova Grau, J. M., Chrysochoou, E., Iordanopoulos, P., &
Ayfadopoulou, G. (2013). Urban mobility indicators for Thessaloniki. Journal of Traffic and Logistics Engineering, 1, 148–152.
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Chapter 59
The Effect of Parameter Selection on Fume Formation Rate in SMAW of AH36 Shipbuilding Steel and Analysis with ANOVA Method
Tolga Mert, Levent Bilgili, Kutsi Mert Senoz, U�gur Bu�gra Çelebi, and Serkan Ekinci
Introduction
Shipbuilding consists of various types of production processes such as painting,
blasting, cutting and welding, which cause considerable amount of deleterious
emissions. Shipbuilding includes the characteristics of both manufacturing and
construction processes. Due to the great amount of steel used during shipbuilding,
welding, which is used to join steel sheet metals, is one of the main manufacturing
methods in shipbuilding.
Welding Types
There are more than 80 different types of welding operations, including brazing,
thermal cutting and gauging, in commercial use. In welding and similar operations,
such as brazing, thermal cutting, and gauging, the most frequently used method for
generating heat is obtained either from an electric arc or a gas-oxygen flame (Mener
et al. 2001). Figure 59.1 presents the most common welding and cutting techniques
used in shipbuilding.
Welding provides a powerful manufacturing tool for high quality joining of
metallic components. Essentially, all metals and alloys can be welded; some with
ease, others requiring special precautions. Of these processes, some of more
common types include shielded metal arc welding (SMAW), gas metal arc welding
(GMAW), flux-cored arc welding (FCAW), submerged arc welding (SAW), gas
T. Mert (*) • L. Bilgili • K.M. Senoz • U.B. Çelebi • S. Ekinci Yildiz Technical University, Barbaros Bulvari, Besiktas, Istanbul 34349, Turkey
e-mail: [email protected]; [email protected]; [email protected]; ucelebi@yildiz.
edu.tr; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_59
795
tungsten arc welding (GTAW), and others such as, plasma arc welding, and oxy-gas
welding (NIOSH 2002). Electric arc welding is the most frequently used process.
Although electric arc welding method can be divided into various types, the
welding process is more or less the same. A flow of electricity across the tip of
the electrode and to the base metal creates the heat needed for melting and joining
the metal parts. The electric current melts both the electrode and the base metal at
the joint to form a molten pool, which solidifies upon cooling. In SMAW method,
the core rod conducts electric current to form the arc and serves as a filler metal for
the joint. The electrode cover provides stability to the arc and protects the molten
metal. GTAW uses a non-consumable tungsten electrode that creates an arc
between the electrode and the weld pool. An inert shielding gas is used in the
process at no applied pressure. GMAW is a consumable electrode welding process
that produces an arc between the base metal and a continuously supplied filler
metal. Externally supplied gas is used to shield the arc. SAW forms an arc between
a bare metal electrode and the work contained in a blanket of granular flux. The
electrodes serve as the filler material, although a welding rod or metal granules may
be added (EPA 1994).
JOINING PROCESS
Resistance Welding
Non consumable Electrode
Consumable Electrode Oxyfuel Cutting
Arc Cutting
Others
Others
Shielded Metal Arc Welding (SMAW)
Gas Metal Arc Welding (GMAW)
Flux Cored Arc Welding(FCAW)
Submerged Arc Welding(SAW)
Electrogas Welding (EGW)
Electroslag Welding (ESW)
Gas Tungsten Arc Welding (GMAW)
Plasma Arc Welding (PAW)
Brazing Soldering Arc Welding
Oxyfuel Welding
Thermal Spraying
Thermal Cutting
Others
Fig. 59.1 Welding and cutting methods in shipbuilding (Celebi 2008)
796 T. Mert et al.
Welding Emissions
Welding process is an important source for harmful emissions. Welding fumes and
emissions, which include various numerous gases and particulates, are classified as
dangerous for human health and environment.
Hazardous metals listed in the 1990 Clean Air Act Amendments that have been
detected in welding fume include manganese, nickel, chromium, cobalt and lead.
Additionally, the hexavalent form of chrome (Chromeþ6) is also found in some welding fume emissions. The emissions of toxic air contaminants during welding
have potential adverse human health impacts (Mener et al. 2001). Both, the quantity
and characteristics of air emissions can change from one welding process to
another. The composition of base metals, welding electrodes, and operating vari-
ables of each process can influence welding emissions (Kura et al. 2009). The main
pollutants of concern generated during welding operations are particulate matter
and particulate phase hazardous air pollutants. Only electric arc welding generates
pollutants in quantities of major concern. The welding fume is formed by the
vaporization and recondensation of metallic elements upon cooling in ambient
air. As such, the particulate matter produced is generally submicron in size with
approximately 50–75% of the particles having diameters in the range of
0.4–0.8 μm. The amount of the emissions generated can vary substantially from process to process (NSRP 2001). Welding fume particles less than 1 mm in
diameter constitute the greatest health hazard because of their ability to penetrate
deep into the lungs (Konarski et al. 2003). Welding is considered as a dangerous
occupation because: (1) there are a multiplicity of factors that can endanger the
health of a welder, such as heat, burns, radiation, noise, fumes, gases, and electro-
cution; and (2) the high variability in chemical composition of welding fumes
which differ according to the work piece, method employed, and surrounding
environment. The particulates and gases generated during welding are considered
to be the most harmful in comparison with the other by-products of welding
(NIOSH 2002). Metal fume fever is a possibility after exposure to manganese
fume. Chronic manganese poisoning, characterized by a severe disorder of the
nervous system, has been reported in welders working in confined spaces on
high-manganese steels. Health effects can only occur if a worker is actually
exposed to the hazard. The risk of injury or disease usually increases with the
duration and frequency of exposure to the agent, and the intensity/concentration and
toxicity of the agent (NIOSH 1990).
In addition to the fume, it is known that gas phase pollutants, such as carbon
dioxide (CO2), carbon monoxide (CO), nitrogen oxides (NOx), sulfur dioxide (SO2)
and ozone (O3), are generated during welding operations. CO may be formed by the
incomplete combustion of the electrode cover or flux and by the use of CO2. High
concentrations of CO may be rapidly fatal without producing significant warning
symptoms (Popović et al. 2014). It is also known that CO has an effect on global
warming (AEA Energy & Environment 2008). CO2 plays a major role in the
atmosphere in global warming and anthropogenic climate change. CO2 is the
59 The Effect of Parameter Selection on Fume Formation Rate in SMAW of AH36. . . 797
largest contributor among well-mixed long-lived greenhouse gases, accounting for
more than 63% of the total. Besides, inhaling CO2 during welding may cause rapid
breathing, rapid beating of the heart, headache, sweating, mental depression and
death. SO2 emissions contribute as a secondary particulate pollutant to formation of
particulate matter (PM) in the atmosphere, an important air pollutant in terms of its
adverse impact on human health (Popović et al. 2014). In some recent studies, it
was indicated that while SO2 has an effect on global cooling (AEA Energy &
Environment 2008), PM has effects both on global warming and global cooling
(Endresen et al. 2003). Ozone and nitrogen oxides are produced by the interaction
of ultraviolet light (from the welding arc) with the surrounding air. These com-
pounds are irritating to the eyes, nose and throat (Popović et al. 2014). In a recent
study, it is also indicated that NOx emissions may have more impact on global
warming than CO2 (Henningsen 2000).
Experimental Study
Fume emission experiments have been realized inside a fume chamber (Fig. 59.2).
AH-36 grade ship building steel round plates with diameter of 290 mm have been
used in the experiments and these plates have been welded with rutile (EN ISO
2560-A: E 42 0 RR 12) and basic (EN ISO 2560-A: E 46 6 B 42 H5) covered
electrodes for 45 s. Welding power source was Lincoln Electric Invertec V260-S.
Chemical composition of base metal and the electrodes are given in Table 59.1.
Voltage values have been measured using Fluke 375 True Rms clamp meter. Fume
was captured on Whatman GF/A glass fiber filters. Filters have been stored in a
furnace at 110 �C for at least 1 h before and after the experiments. Shimadzu BL-320H electronic balance has been used to weigh filters and electrodes. Three
different welding speeds (i.e. 25 cm min�1, 35 cm min�1 and 45 cm min�1) and three different current settings (i.e. 100 A, 120 A, 140 A) have been utilized in the
experiments.
Design of Experiment (L18 Taguchi Design)
Taguchi method is one of the most robust and reliable design of experiment
methods, whose aims are to analyze the effect of process parameters on process
performance, define contribution of each variable and optimize the process.
Table 59.2 shows three process factors (i.e. electrode type, welding speed and
current) and three levels, which were used to form L18 orthogonal array for
Taguchi design.
798 T. Mert et al.
Results and Discussion
Table 59.3 presents L18 orthogonal array experimental set and FFR measurements.
Experimental data were analyzed using signal to noise (S/N) ratio and the
analysis of variance (ANOVA) methods with the help of Minitab 17 software.
Since it is better to have smaller FFR in welding, smaller is better equation was
chosen (Eq. 59.1). Here, n is the number of repeated experiments, Y is the measured
value of the response variable.
Fig. 59.2 Fume chamber
Table 59.1 Chemical composition of AH-36 steel,
rutile and basic covered
electrodes (% wt.)
Material/electrode C Mn Si Pmax Smax
AH-36 steel 0.18 1.30 0.45 0.035 0.035
Rutile electrode 0.07 0.5 0.3 – –
Basic electrode 0.08 1.4 0.4 – –
Table 59.2 Experimental factors and levels
Symbol Factor Level 1 Level 2 Level 3
A Electrode type Rutile Basic –
B Welding speed (cm min�1) 25 35 45 C Current (A) 100 120 140
59 The Effect of Parameter Selection on Fume Formation Rate in SMAW of AH36. . . 799
The lower—the better: S=N ¼ �10log X
Y2
=n
ð59:1Þ
Table 59.4 shows response table for S/N ratios. S/N ratios in Taguchi method are
used to investigate the significance of the factors. Higher S/N ratios yield to the aim,
which is lower FFR. S/N ratios in Table 59.4 and Fig. 59.3 depict electrode type and
current are significant in formation of fume, unlike welding speed and selection of
the covered electrode (rutile or basic) is the biggest contributor in fume formation.
It is clearly understood that FFR is minimum at first level of electrode type (A1),
first level of welding speed (B1) and first level of current (C1). Therefore, optimum
design parameter combination was found to be A1B1C1.
ANOVA analysis was performed to investigate the significance of the factors on
FFR. ANOVA results were based on general linear model. P-value should be equal
or less than 0.05 with 95% confidence level. Since P-values in Table 59.5 are less
than 0.05, confidence level is assured. The percentile effects of each factor were
also calculated. The percentile effect of electrode type, welding speed and current
were found to be 60.10%, 1.16% and 37.16%, respectively. Coefficient of deter-
mination (R-sq (adj)) in ANOVA analysis was 97.78%.
Table 59.3 L18 experimental set and FFR measurements
Factors and levels Output
Run Electrode type
Welding speed
(cm min�1) Current (A) FFR (g min�1)
1 1 1 1 0.129
2 1 1 2 0.187
3 1 1 3 0.235
4 1 2 1 0.143
5 1 2 2 0.195
6 1 2 3 0.268
7 1 3 1 0.145
8 1 3 2 0.179
9 1 3 3 0.283
10 2 1 1 0.275
11 2 1 2 0.293
12 2 1 3 0.396
13 2 2 1 0.283
14 2 2 2 0.324
15 2 2 3 0.423
16 2 3 1 0.264
17 2 3 2 0.337
18 2 3 3 0.436
800 T. Mert et al.
Conclusion
Due to the high preferability of welding in joining processes, it is one of the
important sources of greenhouse gases. Although the production of greenhouse
gas strongly depends on the welding conditions, such as electrode type, current
value, type of the base material, welding speed, the ability of the welder etc.,
greenhouse gases (most particularly CO2) are inevitable end products for most of
the welding processes. Despite the fact that the harmful effects of welding fume are
well documented, there is little research on hazardous gas emissions and further
investigations of their effect on global warming must be realized.
Table 59.4 Response table for S/N ratios
Level A B C
1 14.465 12.476 14.200
2 9.598 11.801 12.272
3 – 11.817 9.623
Delta 4.867 0.675 4.577
Rank 1 3 2
Fig. 59.3 S/N ratios of factor levels for FFR
Table 59.5 ANOVA results for FFR
Source Degree of freedom Adj SS Adj MS F-value P-value % Effect
A 1 0.089324 0.089324 460.88 0.000 60.10
B 2 0.001734 0.000867 4.47 0.035 1.16
C 2 0.055238 0.027619 142.51 0.000 37.16
Error 12 0.002326 0.000194 1.56
Total 17 0.148622 100
59 The Effect of Parameter Selection on Fume Formation Rate in SMAW of AH36. . . 801
Permissible exposure limits for the welding workers have a great importance for
their health. Therefore, studies on welding fume and emissions are the first step to
investigate and understand the limits. This study mainly focused on welding fume
formation rate (FFR) and thus, it has the characteristics of a first stage of a long-
term welding experiment. It is believed the effect of welding on global warming
and worker exposure will be understood more comprehensively with the help of
these studies.
Acknowledgement This experimental study was performed under the sponsorship of Turk Loydu (Turkish Lloyd) and Coordinatorship of Scientific Research Projects of Yildiz Technical
University (Project No.: 2013-10-01-KAP05 and Project No.: 2013-06-01-GEP01).
References
AEA Energy & Environment. (2008). Greenhouse gas emissions from shipping trends, projections and abatement potential. Final report to the Committee on Climate Change, Restricted Commercial, ED 43808, Issue Number 4, 3 Sept 2008.
Celebi, U. B. (2008). Wastes in shipbuilding and painting emission estimation, Ph.D. thesis, Yildiz
Technical University, İstanbul (in Turkish).
Endresen, Ø., Sørgard, E., Sundet, J. K., Dalsøren, S. B., Isaksen, I. S. A., Berglen, T. F.,
et al. (2003). Emission from international sea transportation and environmental impact.
Journal of Geophysical Research, 108, 4560. doi:10.1029/2003JD003751. EPA. (1994). Development of particulate and hazardous emission factors for electric arc welding.
AP-42, Section 12.19, 20 May 1994.
Henningsen, R. F. (2000). Study of greenhouse gas emissions from ships. Final report to the
International Maritime Organization, Norwegian Marine Technology Research Institute
(MARINTEK), Trondheim, Norway, Mar 2000.
Konarski, P., Iwanejko, I., & Ćwil, M. (2003). Core–shell morphology of welding fume micro- and
nanoparticles. Vacuum, 70, 385–389. Kura, B., Jackens, J., & Keay, J. (2009). New weld fume chamber design to assess HAP emissions
potential and promote cleaner production. In Second international workshop/advances in cleaner production, key elements for a sustainable world: Energy, water and climate change, S~ao Paulo, Brazil, 20–22 May 2009.
Mener, W. C., Rosen, P. L., Austin, D. M., & ve Holt, W.S. (2001). Shipyard welding emission
factor development. In 10th international emission inventory conference—“one atmosphere, one inventory, many challenges”, May 1–3.
NIOSH. (1990).Welding: Fumes and gases. Australian Government Publishing Service, Canberra WAP 90/034GS.
NIOSH. (2002). Nomination of welding fumes for toxicity studies. National Institute for Occupa- tional Safety and Health, 20 Feb 2002.
NSRP. (2001). Emission factors for flux core rod used in gas shielded processes. Project No. N1-98-1 Subtask 43, 16 May 2001.
Popović, O., Cvetković, R. P., Burzić, M., Lukić, U., & Beljić, B. (2014). Fume and gas emission
during arc welding: Hazards and recommendation. Renewable and Sustainable Energy Reviews, 37, 509–516.
802 T. Mert et al.
Chapter 60
An Online Visualization Tool for Assessing the Robustness of Multimodal Transport Networks in Case of ExtremeWeather Events and Natural Hazards
Iraklis Stamos, Evangelos Mitsakis, and Georgia Aifadopoulou
Introduction
As climate change induced extreme weather events and natural hazards are
expected to gain in severity and intensity in the following years, it is of central
importance to quantify the potential impacts and effects, among others, in the
transportation sector as well. In an effort to do so, this paper builds on a recently
developed methodology for analysing the effects of EWE and NH on passenger
flows and presents the development of a user-friendly visualization tool for
depicting the outcomes of this analysis. The proposed tool addresses transport
related entities/experts (e.g. planning and decision making authorities, operators,
owners), policy entities, climate change related actors, meteorological agencies,
related international organizations and entities, as well as researchers and individ-
ual users. The tool’s aim is to provide visualized information on EWE and NH occurrence probabilities; climate change related projections; information on mul-
timodal transport networks; and visualized representation of substitutability oppor-
tunities between modes.
A limited number of efforts have taken place in the field of visualizing climate
related datasets. Such efforts include the Green and Blue Space adaptation for urban
areas and eco towns (GRaBS) and the Diachronic Inventory of Forest fires and the
mapping tool of the National Resources Defense Council (NRDC).
GRaBS (PPGIS 2015) has been developed in the framework of the Green and
Blue Space Adaptation for Urban Areas and Eco Towns (GRaBS) project, dealing
with the integration of climate change adaptation into regional planning and
development. In an effort to aid the strategic planning of climate change adaptation
I. Stamos (*) • E. Mitsakis • G. Aifadopoulou Center for Research and Technology Hellas—Hellenic Institute of Transport,
6th Km Charilaou Thermis Road, 57001 Thessaloniki, Greece
e-mail: [email protected]; [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_60
803
responses, a risk and vulnerability assessment tool has been developed, with an
emphasis on flooding and heat stress. The GRaBS tool assesses the vulnerability of
urban areas to climate change impacts, with an additional assessment of relative
patterns of spatial risk where suitable data is available (Fig. 60.1).
The National Observatory of Athens has developed an inventory of forest fires
(NOA 2015), aiming to depict the results of the mapping of burned areas over
Greece for the last 30 years (1984–2012). The services provide the user the ability
to select and switch between a set of datasets (background layers, fire layers, burnt
areas per year, areas which have been burnt mostly during this period, etc.)
(Fig. 60.2).
The National Resources Defense Council of the USA has developed an Extreme
Weather Event map for the year 2012 (NRDC 2012), when a series of “weather
records” were broken, to the frequency and intensity of recorded extreme weather
events and natural hazards attributed to the change of climate (Fig. 60.3).
Outline of the Visualization Tool
The proposed online visualization tool provides users with two services, as depicted
in Fig. 60.4:
– Information on past and future frequency of selected weather phenomena in
134 locations in Europe, visualized on the European territory.
Fig. 60.1 View from the GRaBS adaptation Toolkit (source: http://www.ppgis.manchester.ac.uk/ grabs/start.html)
804 I. Stamos et al.
Fig. 60.2 View from the NOA tool—Diachronic Inventory of Forest fires (source: http://ocean. space.noa.gr/diachronic_bsm/)
Fig. 60.3 View from the NRDC tool—ExtremeWeather Map 2012 (source: http://www.nrdc.org/ health/extremeweather/)
60 An Online Visualization Tool for Assessing the Robustness of Multimodal. . . 805
– Impacts of selected extreme weather events on passenger flows for surface and
air transport modes on 14 locations in Europe, visualized on the European
territory.
While the first service of the tool is only informative, providing to the end-users
with a limited range of actions, as they are only able to see visualized outputs of a
predefined dataset on preselected locations and as no computational process will
take place, the second service is more complex. It provides its users with interaction
capabilities, allowing own user’s input that will determine the visualized outputs, which are based on computations of certain parameters. The following figure
depicts the options for the end-user regarding the service of the visualization tool.
The visualization tool is a web-based application that provides information
about past and future weather phenomena and presents impact of EWE and NH
on passenger flows. Both cases are related to different European locations and the
visualization is done using a map. Particular emphasis is placed on simplicity,
usability and stylishness of the application. While it is important that the application
is as simple as possible, thus increasing usability, the information itself is visualized
in a comprehensive way so that the user can absorb it as efficiently as possible.
Data Needs
This section describes the data types and data formats needed for the development
and operation of the proposed visualization tool. Each dataset is described individ-
ually in the next sections.
Static
Information on past and future frequency of selected weather
phenomena
Visualized impact of selected extreme weather events on passenger flows
on selected European locations
ComputedStatic or computed
Fig. 60.4 Visualization tool end-user services
806 I. Stamos et al.
Geographical Data (GD)
Location coordinates (Latitude, Longitude) in WGS84 projection exist for all
134 locations that are used by the visualization tool. The 14 locations used for
depicting the impacts of extreme weather events are a subset of those 134 locations
(Table 60.1).
Temporal Periods (TP)
There are datasets for three periods in the visualization tool:
– 1971–2000
– 2001–2040
– 2041–2070
Weather Phenomena (WP)
The weather phenomena included in the databases of the visualization tool are the
following:
1. Wind Gusts (WG)
2. Snowfall (SF)
3. Blizzard (BL)
4. Heavy Precipitation (HP)
5. Heat Waves (HW)
6. Cold Waves (CW)
Table 60.1 Indicative format of locations and coordinates
data
Location Latitude Longitude
Achleiten 48.583 13.416
Algeciras 36.167 �5.527 Amsterdam 52.427 4.762
Antwerp 51.328 4.313
Athens 381.543 238.588
Barcelona 414.946 21.417
Basel 47.565 7.594
Belfast 54.614 �5.925 Belgrad 447.412 204.889
Bergen 60.387 5.326
Berlin 525.098 134.367
Bilbao 433.274 �30.248
60 An Online Visualization Tool for Assessing the Robustness of Multimodal. . . 807
Weather Phenomena Categories (WPC)
Each of the above defined weather phenomena (WP) has the following
sub-categories:
1. Wind Gusts (WG)
(a) 17 m/s
(b) 25 m/s
(c) 32 m/s
2. Snowfall (SF)
(a) 10 cm/d
(b) 10 cm/d
(c) 20 cm/d
3. Blizzard (BL)
4. Heavy Precipitation (HP)
(a) 30 mm/d
(b) 100 mm/d
(c) 150 mm/d
5. Heat Waves (HW)
(a) >25 �C (b) >32 �C (c) >43 �C
6. Cold Waves (CW)
(a) <0 �C (b) <�7 �C (c) <�20 �C
Weather Phenomena Categories Data (WPCD)
Each of the 134 locations receives one value for the above mentioned categories for
all weather phenomena, representing the number of days that this event will occur
in addition to the 1st Temporal Category (1971–2000). Tables, sized GD�WPC, for each WP and TP are available (i.e. five tables of 134� 3� 3 and one table of 134� 1� 3). Values within these Tables are ranged between: �60.7 and 196.6. An indicative layout format is depicted in the Table 60.2.
Additionally, these Tables will be also provided in such a way so as to represent
the probability of the event occurring in one of the second (2001–2040) or third
(2040–2070) temporal periods, with values ranging between 0 and 1.
808 I. Stamos et al.
Demand Data (DD)
Demand data describe travel demand information (i.e. number of trips per mode)
between certain nodes of a network. Demand data available for the proposed
visualization tool refer to 14 selected cities’ in-between connections. Demand data are classified in the three modes examined: rail, road and air transport.
Therefore, three Tables (for each mode of transport), sized 14� 14 are available. Values within these Tables range between 0 and 999,999,999. An indicative layout
format is depicted in Table 60.3 (for road transport).
Supply Data (SD)
Supply data are classified in Cost, Time and Value of Time data.
Cost Data (CD)
Cost data describe the cost in € for the connections of the 14 selected cities for each three modes that are examined in MOWE-IT. Therefore, three tables (for each
mode of transport), sized 14� 14 are available. Values within these Tables are ranged between 0 and 999,999,999. An indicative layout format for road transport is
depicted in Table 60.4.
Table 60.2 Indicative format of Weather Phenomena Categories Data
1971–2000 2001–2040 2040–2070
Wind gust Wind gust Wind gust
Location 17 m/s 25 m/s 32 m/s 17 m/s 25 m/s 32 m/s 17 m/s 25 m/s 32 m/s
Achleiten 14.43 0.38 0.00 14.43 0.38 0.00 14.43 0.38 0.00
Algeciras 14.14 0.24 0.00 14.14 0.24 0.00 14.14 0.24 0.00
Amsterda 44.29 2.38 0.10 44.29 2.38 0.10 44.29 2.38 0.10
Antwerp 35.00 1.14 0.05 35.00 1.14 0.05 35.00 1.14 0.05
Athens 22.76 0.62 0.00 22.76 0.62 0.00 22.76 0.62 0.00
Barcelona 2.81 0.05 0.00 2.81 0.05 0.00 2.81 0.05 0.00
Basel 14.10 0.29 0.05 14.10 0.29 0.05 14.10 0.29 0.05
Belfast 75.33 6.81 0.52 75.33 6.81 0.52 75.33 6.81 0.52
Belgrad 2.14 0.00 0.00 2.14 0.00 0.00 2.14 0.00 0.00
Bergen 35.43 1.29 0.05 35.43 1.29 0.05 35.43 1.29 0.05
Berlin 18.62 0.33 0.00 18.62 0.33 0.00 18.62 0.33 0.00
Bilbao 23.57 1.76 0.10 23.57 1.76 0.10 23.57 1.76 0.10
Source: MOWE-IT project (2014)
60 An Online Visualization Tool for Assessing the Robustness of Multimodal. . . 809
T a b le
6 0 .3
In d ic at iv e fo rm
at o f D em
an d D at a (i n p as se n g er
tr ip s)
D em
an d D at a—
R o ad
T ra n sp o rt
A T H
A M S
B C N
C O P
F R A
L O N
M A D
M A L
M O S
M U C
P A R
R O M
S T O
Z U R
A T H
0 3 9 3
4 5 4
3 4 8
3 4 4
4 3 2
5 5 0
4 5 9
3 8 0
3 0 4
4 3 3
1 7 6
4 6 1
3 6 9
A M S
3 9 3
0 2 7 0
1 4 2
5 4
6 8
3 1 1
2 7 5
2 8 5
1 0 0
7 8
2 7 4
2 6 0
1 2 9
B C N
4 5 4
2 7 0
0 3 8 4
2 4 0
2 7 1
7 6
5 0 4
2 7 4
1 9 4
2 8 1
5 0 5
2 2 8
C O P
3 4 8
1 4 2
3 8 5
0 1 4 8
1 9 7
4 4 0
3 9 1
2 5 5
1 1 2
2 0 7
3 5 6
1 2 1
2 2 4
F R A
3 4 4
5 2 4 0
1 4 6
0 9 5
3 4 3
2 4 6
2 7 2
4 9
9 8
2 2 5
2 6 6
7 9
L O N
4 3 2
6 8
2 7 0
1 9 7
9 4
0 3 1 2
2 7 6
3 3 7
1 8 8
7 9
3 4 7
3 1 5
2 0 1
M A D
5 5 0
3 1 3
1 0 2
4 4 2
3 4 5
3 0 9
0 6 6
6 0 6
3 7 0
2 3 6
3 7 7
5 5 8
3 2 4
M A L
4 5 9
2 7 6
7 3 9 1
2 4 6
2 7 7
6 5
0 5 1 1
2 7 9
1 9 9
2 8 6
5 1 2
2 3 4
M O S
3 8 0
2 8 8
5 0 4
3 3 0
2 7 4
3 3 7
6 0 6
5 1 1
0 2 7 2
3 4 5
4 1 4
1 3 4
3 3 1
M U C
3 0 4
7 8
2 7 4
1 8 0
4 9
1 8 8
3 7 0
2 7 9
2 7 0
0 1 3 8
1 7 7
2 3 0
7 8
P A R
4 3 3
7 8
1 9 3
2 0 7
8 4
8 0
2 3 4
1 9 9
3 4 5
1 2 4
0 3 4 3
3 2 5
1 4 6
R O M
1 7 6
2 7 4
2 8 0
3 5 5
2 2 3
3 4 5
3 7 6
2 8 6
4 1 4
1 7 6
3 2 6
0 4 0 7
1 7 9
S T O
4 6 1
2 6 0
5 0 5
1 2 1
2 6 6
3 1 5
5 5 8
5 1 2
1 3 4
2 3 0
3 2 5
4 0 7
0 3 4 0
Z U R
3 6 9
1 3 0
2 2 8
2 2 3
7 9
2 0 1
3 2 4
2 3 3
3 3 1
7 7
1 4 5
1 7 9
3 4 0
0
S o u rc e:
E T IS P lu s p ro je ct
(2 0 1 0 )
810 I. Stamos et al.
T a b le
6 0 .4
In d ic at iv e fo rm
at o f C o st D at a (i n €)
In p u t D at a—
S u p p ly
D at a—
C o st —
R o ad
T ra n sp o rt
A T H
A M S
B C N
C O P
F R A
L O N
M A D
M A L
M O S
M U C
P A R
R O M
S T O
Z U R
A T H
0 3 9 3
4 5 4
3 4 8
3 4 4
4 3 2
5 5 0
4 5 9
3 8 0
3 0 4
4 3 3
1 7 6
4 6 1
3 6 9
A M S
3 9 3
0 2 7 0
1 4 2
5 4
6 8
3 1 1
2 7 5
2 8 5
1 0 0
7 8
2 7 4
2 6 0
1 2 9
B C N
4 5 4
2 7 0
0 3 8 4
2 4 0
2 7 1
7 6
5 0 4
2 7 4
1 9 4
2 8 1
5 0 5
2 2 8
C O P
3 4 8
1 4 2
3 8 5
0 1 4 8
1 9 7
4 4 0
3 9 1
2 5 5
1 1 2
2 0 7
3 5 6
1 2 1
2 2 4
F R A
3 4 4
5 2 4 0
1 4 6
0 9 5
3 4 3
2 4 6
2 7 2
4 9
9 8
2 2 5
2 6 6
7 9
L O N
4 3 2
6 8
2 7 0
1 9 7
9 4
0 3 1 2
2 7 6
3 3 7
1 8 8
7 9
3 4 7
3 1 5
2 0 1
M A D
5 5 0
3 1 3
1 0 2
4 4 2
3 4 5
3 0 9
0 6 6
6 0 6
3 7 0
2 3 6
3 7 7
5 5 8
3 2 4
M A L
4 5 9
2 7 6
7 3 9 1
2 4 6
2 7 7
6 5
0 5 1 1
2 7 9
1 9 9
2 8 6
5 1 2
2 3 4
M O S
3 8 0
2 8 8
5 0 4
3 3 0
2 7 4
3 3 7
6 0 6
5 1 1
0 2 7 2
3 4 5
4 1 4
1 3 4
3 3 1
M U C
3 0 4
7 8
2 7 4
1 8 0
4 9
1 8 8
3 7 0
2 7 9
2 7 0
0 1 3 8
1 7 7
2 3 0
7 8
P A R
4 3 3
7 8
1 9 3
2 0 7
8 4
8 0
2 3 4
1 9 9
3 4 5
1 2 4
0 3 4 3
3 2 5
1 4 6
R O M
1 7 6
2 7 4
2 8 0
3 5 5
2 2 3
3 4 5
3 7 6
2 8 6
4 1 4
1 7 6
3 2 6
0 4 0 7
1 7 9
S T O
4 6 1
2 6 0
5 0 5
1 2 1
2 6 6
3 1 5
5 5 8
5 1 2
1 3 4
2 3 0
3 2 5
4 0 7
0 3 4 0
Z U R
3 6 9
1 3 0
2 2 8
2 2 3
7 9
2 0 1
3 2 4
2 3 3
3 3 1
7 7
1 4 5
1 7 9
3 4 0
0
S o u rc e:
M O W E -I T p ro je ct
(2 0 1 4 )
60 An Online Visualization Tool for Assessing the Robustness of Multimodal. . . 811
Time Data (TD)
Time data describe the cost in € for the connections of the 14 selected cities for all three modes of transport that are examined in MOWE-IT. Therefore, three tables
(for each mode of transport), sized 14� 14 are available. Values within these Tables are ranged between 0 and 999,999,999. An indicative layout format for air
transport is depicted in Table 60.5.
Value of Time Data (VoTD)
This data category describes the Value of Time and refers to € per hour for all connections between the 14 selected cities, for all three modes of transport that are
examined. Therefore, three tables (for each transport mode transport), sized 14� 14 are available. Values within these tables range between 0 and 50. An indicative
layout format for rail transport is depicted in Table 60.6.
Model Parameters (MP)
This data category describes certain parameters that are used in the functions
“module” and concern:
– The weight of cost for every mode (WoC)
– The weight of time for every mode (WoT)
– The quality parameter for every mode (QP)
– A fixed scaling factor parameter for every mode (μ)
User Input
This section describes the inputs of the end-user to enable the visualization tool to
compute and depict the impacts of extreme weather events on passenger flows
per mode.
Type of Extreme Weather Event (WP)
The end-user chooses the type of the extreme weather event that will be examined
by the tool. The extreme weather event types are similar to the weather phenomena
described previously.
812 I. Stamos et al.
T a b le
6 0 .5
In d ic at iv e fo rm
at o f T im
e D at a (i n h o u rs )
In p u t D at a—
S u p p ly
D at a—
T im
e— A ir T ra n sp o rt
A T H
A M S
B C N
C O P
F R A
L O N
M A D
M A L
M O S
M U C
P A R
R O M
S T O
Z U R
A T H
0 5
2 5
6 2
3 3
6 2
3 1
1 2
4
A M S
2 0
2 1
1 1
3 8
4 2
1 2
2 4
B C N
3 2
0 5
4 2
2 1
4 2
2 2
7 2
C O P
6 1
3 0
2 2
8 5
7 2
2 5
1 4
F R A
4 1
4 1
0 4
4 8
8 1
1 2
2 3
L O N
4 1
2 2
2 0
2 1 0
6 4
1 3
4 2
M A D
5 3
1 6
3 2
0 1
7 5
2 7
7 2
M A L
4 5
1 7
2 6
1 0
9 2
5 4
7 2
M O S
5 6
1 0
5 1 2
6 2
8 0
3 6
6 1 0
6
M U C
3 2
2 2
1 5
5 7
9 0
2 2
7 1
P A R
3 1
2 2
1 1
2 2
5 2
0 2
6 1
R O M
2 3
2 5
2 3
3 6
6 2
2 0
9 2
S T O
7 2
3 1
4 2
6 1 2
1 1 0
7 6
0 5
Z U R
3 2
4 2
1 1
2 2
6 1
1 2
3 0
S o u rc e:
M O W E -I T p ro je ct
(2 0 1 4 )
60 An Online Visualization Tool for Assessing the Robustness of Multimodal. . . 813
T a b le
6 0 .6
In d ic at iv e fo rm
at o f V al u e o f T im
e D at a (i n €/ h )
V al u e o f T im
e— R ai l T ra n sp o rt
A T H
A M S
B C N
C O P
F R A
L O N
M A D
M A L
M O S
M U C
P A R
R O M
S T O
Z U R
A T H
0 1 8
1 7
1 9
1 8
1 9
1 7
1 7
1 7
1 8
1 9
1 8
1 9
2 1
A M S
1 8
0 1 8
2 0
1 9
1 9
1 8
1 8
1 8
1 9
2 0
1 9
2 0
2 1
B C N
1 7
1 8
0 1 9
1 8
1 8
1 7
1 7
1 7
1 8
1 9
1 8
1 9
2 0
C O P
1 9
2 0
1 9
0 2 0
2 1
1 9
1 9
1 9
2 0
2 1
2 0
2 1
2 2
F R A
1 8
1 9
1 8
2 0
0 1 9
1 8
1 8
1 8
1 9
2 0
1 9
2 0
2 1
L O N
1 9
1 9
1 8
2 1
1 9
0 1 8
1 8
1 9
1 9
2 0
2 0
2 0
2 2
M A D
1 7
1 8
1 7
1 9
1 8
1 8
0 1 7
1 7
1 8
1 9
1 8
1 9
2 0
M A L
1 7
1 8
1 7
1 9
1 8
1 8
1 7
0 1 7
1 8
1 9
1 8
1 9
2 0
M O S
1 7
1 8
1 7
1 9
1 8
1 9
1 7
1 7
0 1 8
1 9
1 8
1 9
2 1
M U C
1 8
1 9
1 8
2 0
1 9
1 9
1 8
1 8
1 8
0 2 0
1 9
2 0
2 1
P A R
1 9
2 0
1 9
2 1
2 0
2 0
1 9
1 9
1 9
2 0
0 2 0
2 1
2 2
R O M
1 8
1 9
1 8
2 0
1 9
2 0
1 8
1 8
1 8
1 9
2 0
0 2 0
2 2
S T O
1 9
2 0
1 9
2 1
2 0
2 0
1 9
1 9
1 9
2 0
2 1
2 0
0 2 2
Z U R
2 1
2 1
2 0
2 2
2 1
2 2
2 0
2 0
2 1
2 1
2 2
2 2
2 2
0
S o u rc e:
E W E N T p ro je ct
(2 0 1 2 )
814 I. Stamos et al.
Location of Occurrence (LO)
The end-user will have the ability to choose the exact location within the EU
territory that an extreme weather event occurs. In order for the tool to compute
the impacts of the chosen event, it will need to assign this event to the closest (based
on proximity—direct distance) city within the network of the 14 pre-selected cities.
The assignment of the event is a “one-to-one” relation with the city, as the end-user
is able to choose another additional event, which again is assigned to the closest city
(even if the city is the same).
Occurrence Probability (OP)
For each Weather Phenomenon identified previously, its probability of occurring in
one or more locations (out of the 14 considered herein) is provided by the end-user.
Values are ranged between 0 (when no event is present) to 1 (when an event is
occurring now, i.e. at real-time). Additionally, the end-user will need to be able to
choose the probability of the event based on the available Weather Phenomena
Categories Data—WPCD.
Duration of Impact (DI)
For each Weather Phenomenon identified, the expected duration of its impact in
hours in one or more locations (out of the 14 considered herein) is provided by the
end-user. Values range between 0 and 24.
Operation Reduction (OR)
For each Weather Phenomenon identified and for each mode considered, the
expected operation reduction of the performance of the respective network is
provided by the end-user. Values range between 0 (no impact at all) and 1 (full
operational impairment of the respective network). According to the process
described before, after the end-user chooses the location of the event, the event is
assigned to one of the 14 preselected cities. After this assignment, the operation
reduction is considered to impact all connections that have either as origin or as
destination the assigned city. For instance, if the end-user chooses that extreme heat
waves will occur in the Netherlands (assumingly creating wildfires), having as
impact that the road network operations will be affected by 50%, then a table of
the following form is created (Table 60.7).
60 An Online Visualization Tool for Assessing the Robustness of Multimodal. . . 815
T a b le
6 0 .7
E x em
p la ry
o u tp u t o f th e o p er at io n re d u ct io n in
ro ad
tr an sp o rt
H ea tw av es —
O p er at io n R ed u ce d b y (%
) O /D —
R o ad
T ra n sp o rt
A T H
A M S
B C N
C O P
F R A
L O N
M A D
M A L
M O S
M U C
P A R
R O M
S T O
Z U R
A T H
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
A M S
0 .5
0 .5
0 .5
0 .5
0 .5
0 .5
0 .5
0 .5
0 .5
0 .5
0 .5
0 .5
0 .5
0 .5
B C N
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
C O P
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
F R A
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
L O N
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
M A D
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
M A L
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
M O S
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
M U C
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
P A R
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
R O M
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
S T O
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
Z U R
0 .0
0 .5
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
0 .0
S o u rc e:
M O W E -I T p ro je ct
(2 0 1 4 )
816 I. Stamos et al.
Architecture
The architecture of the visualization tool is comprised of two main components as
depicted in Fig. 60.5 the server-side and the client-side. The server-side consists of
a pre-processor and a database. The pre-processor is responsible for creating the
client-side’s user interface (UI) when the user starts the application. Data for the UI is retrieved from the database by the pre-processor during the initialization of the
application. However, the pre-processor can provide additional data to the applica-
tion also during runtime. The role of the client-side is mainly to visualize the
available data to the user. However, the role includes also handling the
pre-visualization calculations for the data as well as the previously mentioned
communication with the server-side.
User Interface
The client-side User Interface (UI) is divided into two main functionalities based on
the source of data. The user is required to choose whether she/he wants to visualize
the static weather phenomena data or computed data. The latter are generated based
on input provided by the user and contain information of how extreme weather
events impact passenger flows.
Use of Static Data
In the case of static data, the UI consists of a map and a search field for locations.
The map shows a small marker for each of the 134 European locations, for which
existing weather phenomena data are stored in the tool. For displaying the data, the
user can select a dot or type the desired location into the search field. This action
leads to data being visualized with a tree-like structure on top of the selected
location. Figure 60.6 depicts an indicative illustration of the data tree.
The data tree consists of location name, climatic region, temporal period as well
as the actual data for each weather phenomenon. Each weather phenomenon has its
own icon which acts as an on/off switch for showing a tree branch containing the
corresponding weather phenomenon data. Thus, the user can decide which weather
phenomena data are visible. If the temporal period is changed, the data shown is
automatically changed, in order to correspond to the selected period.
60 An Online Visualization Tool for Assessing the Robustness of Multimodal. . . 817
Static or computed
computed
Type of extreme weather event - WP
Occurrence Probability - OP
Occurrence Probability - OP
Tool Functions
Presentation Modules
Maximum Operation Reduction
Cost Processing
Generalized Cost Processing
Probability of Mode choice
Computed Values Preparer
Information Preparer
Visualization Engine
Final Trips
Processed Cost Data
Processed Time Data
Processed Generalized Cost Data
Time Processing
VoT
TP
MP
DD
WPCD
WPC
Cost Data
Time Data
Project Data
Static
Duration of Impact -DI
Operation Reduction - OR
Fig. 60.5 Visualization tool architecture
818 I. Stamos et al.
Use of Computed Data
In the case of computed data, the UI consists of a map and a list of extreme weather
events added by the user. The user is able to add new weather events by using a
form, which is opened by selecting a dedicated button/link alongside the weather
event list. For each event type, subcategory, location, occurrence probability,
duration, operation reduction and transport mode must be defined. Type and
subcategory must be selected from predefined values, while location can be selected
from predefined values or pointed from the map. If location is selected from the
map, the tool will calculate which predefined location is closest to the selected
location and assign the matched predefined location to the event. Occurrence
probability can be chosen from predefined values or defined manually. Duration
and operation reduction must be defined manually, and finally, transport mode must
be selected from predefined values. Once all of these are defined for one event, and
the user provides a confirmation, the event is added to the list of all events. The user
can, in addition to adding new events, modify and remove existing events.
A marker is presented on the map for each location belonging to a group of
14 pre-selected locations in Europe. Before the user can interact with the map
locations, she/he is required to add at least one weather event. The location to which
the event is assigned to, will be the origin of the connection. At this point, the user is
able to select (click on) one of the other 13 locations, which will then be assigned as
the destination for the user selected connection. The connection data is then
visualized with two parallel lines connecting the two locations. These lines present
Fig. 60.6 Data tree visualization for static data
60 An Online Visualization Tool for Assessing the Robustness of Multimodal. . . 819
the data with and without the added weather event(s) respectively. Both lines are
composed of three parts, each of which represents one of the three transport modes
(air, rail and road). Each line is divided amongst these three modes by their
percentage of the total number of trips combined from all three modes. An indic-
ative visualization result is presented in the Fig. 60.7.
After the user has defined a connection with both origin and destination, she/he
is able to reverse the direction of the connection by selecting (clicking on) a button
alongside the lines. This leads to data being updated and presented respectively.
Conclusions
A data-driven method, which utilizes existing datasets for quantifying modal
differentiated passenger trips in cases of extreme weather event, has been recently
proposed, which enables the development of support tools for related entities and
stakeholders, which are confronted with the assessment of the resilience of passen-
ger transportation networks. The proposed visualization tool serves as a prototype
for presenting weather data and mobility of people between major locations in
Europe. The tool has been designed to be available for any additions in terms of
data or subject area coverage, for instance visualization of European patterns of
extreme weather events such as flooding etc. It is anticipated that such functionality
is useful in future projects, where these types of analyses will be required.
Fig. 60.7 Visualization of computed data
820 I. Stamos et al.
Policy-makers, operators and transport system users are likely to find the informa-
tion provided by the visualization tool useful in aiding choices and mapping of
alternatives in the case of anticipated disruptions. Also, in the case of unexpected
disruptions, the tool will also be useful as it allows for reacting to problems
encountered with best possible response. A major research challenge with respect
to passenger transport is the availability of substitution in quantity. There are supply
constraints on road and rail networks that prevent infinite expansion of volumes,
which is particularly relevant in high density routes. Also, carriage such as coaches
and buses may not exist physically at right locations, which will add to limitations
of substitution. One way to work with this problem would be to introduce disaster
preparation into fleet management of operators to better target the areas in need,
when disruptions take place. However, as the nature of extreme weather events
suggests, predicting periods are short and anticipation difficult. Future research
should lie in the field of obtaining data at real-time, so that the outcomes of the tool
can be used at any given time. In addition, all input in the tool should be filtered and
checked for inconsistencies in order to improve the accuracy and validity of
presented results.
Acknowledgement This work was supported by the European Commission Seventh Framework Programme, under the “MOWE-IT: Management of Weather Events in the Transport System”
project.
References
ETISPlus project. http://www.etisplus.eu/default.aspx.
EWENT Project. Retrieved March 15, 2015 from http://ewent.vtt.fi/.
MOWE-IT project, Retrieved March 18, 2015 from http://www.mowe-it.eu/.
Retrieved February 20, 2015 from http://www.ppgis.manchester.ac.uk/grabs/start.html.
Retrieved March 02, 2015 from http://ocean.space.noa.gr/diachronic_bsm/.
Retrieved March 14, 2015 from http://www.nrdc.org/health/extremeweather/.
60 An Online Visualization Tool for Assessing the Robustness of Multimodal. . . 821
Part XV
Securing Sustainable Mobility to Mitigate Climate Change
Climate Impact Effects of Air and Maritime Transport
Chapter 61
Manmade Changes in Cirrus Clouds from 1984 to 2007: A Preliminary Study
Kostas Eleftheratos, Gunnar Myhre, Patrick Minnis,
Ioannis Kapsomenakis, and Christos Zerefos
Introduction
Aircraft flying at high altitudes form line shaped clouds which are called contrails.
Contrails form if the ambient air is cold enough (Schumann 1996). In dry air the
contrails dissipate quickly, and their impact is of minor importance, but in moist air
which is super-saturated with respect to ice, the contrails spread and grow with the
uptake of ambient water vapour, and become contrail-cirrus (Schumann 2005).
Contrail-cirrus would not exist without the prior formation of contrails (i.e., Gierens
2007). This kind of cirrus formation occurs in regions with high air traffic (i.e.,
North America, North Atlantic and Europe). Contrail evolution into cirrus clouds
K. Eleftheratos (*) Laboratory of Climatology and Atmospheric Environment, Faculty of Geology and
Geoenvironment, National and Kapodistrian University of Athens, Athens 15784, Greece
Biomedical Research Foundation of the Academy of Athens, Athens, Greece
e-mail: [email protected]
G. Myhre
Center for International Climate and Environmental Research Cicero-Oslo (CICERO),
Oslo, Norway
P. Minnis
Atmospheric Sciences, NASA Langley Research Center, Hampton, VA, USA
I. Kapsomenakis
Research Centre for Atmospheric Physics and Climatology, Academy of Athens,
Athens, Greece
C. Zerefos
Biomedical Research Foundation of the Academy of Athens, Athens, Greece
Research Centre for Atmospheric Physics and Climatology, Academy of Athens,
Athens, Greece
Navarino Environmental Observatory (N.E.O.), Messinia, Greece
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_61
827
has been observed both in North America and Europe (Minnis et al. 1998; Haywood
et al. 2009).
The possible influence of air traffic emissions on cirrus cloud positive trends has
been examined using various methods and different datasets for different periods of
records (i.e., Zerefos et al. 2003; Minnis et al. 2004; Stubenrauch and Schumann
2005; Stordal et al. 2005; Mannstein and Schumann 2005; Krebs 2006). The major
findings of those studies were summarized by Gierens (2007). For example, in
central Europe it was found that the observed positive trends in cirrus due to aircraft
are about 1–2% cover per decade. Mannstein and Schumann (2005) had estimated
~3% additional cloud coverage due to aircraft over Europe, which is about ten
times higher than the coverage by linear contrails (~0.3%) alone. However, their
conclusion that the coverage by additional cirrus clouds in Europe is about 10 times
higher than by linear contrails was no longer supported (Mannstein and Schumann
2007). As air traffic increases (~5% per year), manmade (aviation) cirrus clouds are
expected to increase. These additional clouds contribute to the greenhouse effect
(i.e., Minnis et al. 2004; Sausen et al. 2005).
The objective of this study is to analyse long-term changes in cirrus clouds from
ISCCP over congested air traffic corridors during the past two decades or so, in
association with the changes in global air traffic. Radiative forcing calculations of
the additional cirrus coverage due to aircraft are also provided.
Data Sources
The cloud data set analysed in this study was produced by the International Satellite
Cloud Climatology Project (Rossow and Schiffer 1999). The data are based on
observations from a suite of operational geostationary and polar orbiting satellites.
Visible radiances are used to retrieve the optical thickness of clouds and infrared
radiances to retrieve cloud top temperature and pressure. The D2 dataset used in this
study has a spatial resolution of 280 km (2.5o at the equator) and provides monthly
averages of cloud properties of 15 different cloud types. The cloud types are derived
based on radiometric definitions that rely on cloud optical thickness and cloud top
pressure. Cirrus clouds are defined as those with optical thickness less than 3.6 and
cloud top pressure less than 440 hPa. In this study we made use of the cirrus cloud
data for the period 1984–2007. The ISCCP cloud properties have been tested
extensively both against other satellite cloud retrievals and against surface cloud
observations (Rossow and Schiffer 1999). Further information can be found by
Zerefos et al. (2003).
The analysis also includes the study of relative humidity at high-flying altitude
levels from the independently produced NCEP-DOE and ERA-Interim Reanalysis
projects. The 250 and 300 hPa levels were selected for this study as a compromise
upper tropospheric level for the tropics, middle and high latitudes. Both projects
provide mean monthly gridded values of various atmospheric and surface param-
eters on 2.5o� 2.5o grid boxes and on global scale. We used monthly daily means
828 K. Eleftheratos et al.
which are monthly means computed at base times 0000, 0600, 1200 and 1800 UTC.
The NCEP-DOE Reanalysis-2 data were downloaded from the internet at the
webpage http://www.esrl.noaa.gov/psd/data/gridded/data.ncep.reanalysis2.html.
The ERA-Interim monthly mean data were downloaded from the webpage http://
data-portal.ecmwf.int/data/d/interim_moda/levtype¼pl/. To overcome the effect of seasonal variations, all trends were calculated after
removing variations related to the seasonal cycle of the data. Cirrus cloud data were
deseasonalized by subtracting the long-term monthly mean (1984–2007) pertaining
to the same calendar month. All trends were evaluated as to their statistical
significance by applying the t-test of each trend against the null hypothesis of no-trend for the appropriate number of degrees of freedom. Cirrus cloud data for
the period 1991–1993 were not used in our trend analysis in order to minimize
artificial satellite cloud retrievals after the eruption of Mt. Pinatubo in 1991
(Rossow and Schiffer 1999; Luo et al. 2002; Zerefos et al. 2003).
Results and Discussion
Manmade Changes in Cirrus Clouds
Manmade changes in cirrus cloudiness were examined by comparing cirrus cloud
cover over higher traffic regions and over lower traffic regions in the northern
mid-latitudes (e.g. United States of America, Europe, North Atlantic and North
Pacific Ocean). We have restricted the analysis to the northern mid-latitudes
because in the tropics it is difficult to detect possible effects of regional persistent
contrails on cirrus cloud trends. This is because trends in dynamics and thermody-
namics mask possible man-made trends in cirrus clouds in those regions. Taking
also into account that flight frequencies and fuel consumption are moderate over the
tropical air traffic corridors, it makes it even more difficult to detect and quantify
any possible anthropogenic effects (Zerefos et al. 2007). In addition, because we
wanted to avoid the strong impact of El Nino/Southern Oscillation on cirrus clouds
in the tropics (Eleftheratos et al. 2007).
Regions that correspond to different air traffic loading have been compared
using air traffic statistics based on the emissions inventory of the QUANTIFY
project. More specifically, two adjacent regions one with low and another with high
air traffic over North America, Europe, North Atlantic and North Pacific have been
selected, respectively. Analytical information on the spatial distribution of the
selected areas is presented in Table 61.1. Table 61.2 shows the density of air traffic
over the selected regions as fractions of the total air traffic. This analysis basically
assumes that the differences in the trends are the result of differences in air traffic
between the adjacent regions.
Figure 61.1 shows the annual mean cirrus coverage averaged over all high air
traffic regions in North America, Europe, North Atlantic and North Pacific in
61 Manmade Changes in Cirrus Clouds from 1984 to 2007: A Preliminary Study 829
comparison to the adjacent lower air traffic regions. Although both time series show
the same variability from year to year, their long-term trends differ. From 1984 to
2004 cirrus cloud cover increased from 10.3 to 12.1% in high air traffic corridors
(¼1.8% increase), whereas no such change could be detected in low traffic areas. At the same time, global average annual mean fuel consumption rose from 139 to
222 Tg from 1984 to 2004 (¼60% increase). Air traffic increased much faster at 5–6% on a global annual average, i.e. by 165–220% in that period (Lee et al. 2009).
The high air traffic corridor cirrus increased at least at the global average rate. Thus,
we estimate an additional cloud coverage of up to 0.01% over these corridors for
every per cent increase in air traffic in the period 1984–2004.
Long-term trends in cirrus clouds for each high and low air traffic region are
summarized in Table 61.3. Long-term trends were estimated as the increase or
decrease of cirrus cloud cover in per cent per decade inferred from a least square
linear fit to the data.
The differences between the trends over high air traffic relative to the low air
traffic regions are statistically significant at the 99% confidence level. The trend
differences could provide indications for the additional cloud coverage that has
been induced by aviation over heavy air traffic regions. The results show an
increase in cirrus coverage in high air traffic areas of +0.6% per decade, contrasted
by a decrease of 0.3% per decade in low traffic areas, which could be interpreted as
a 0.9%/decade change in cirrus due to air traffic. In all cases the differences have a
positive trend which is consistent with the increasing trend in global air traffic
during the past 20 years.
Table 61.1 Definition of high and adjacent low air traffic regions analysed in this study
High air traffic Low air traffic
North America 30�N-45�N, 60�W-130�W 45�N-60�N, 60�W-130�W Europe 40�N-60�N, 10�W-40�E 20�N-40�N, 10�W-40�E North Atlantic 40�N-60�N, 10�W-60�W 20�N-40�N, 10�W-60�W North Pacific 45�N-60�N, 145�E-130�W 30�N-45�N, 145�E-130�W
Table 61.2 Million kilometres travelled by aviation over high and adjacent low air traffic regions as fraction of the global kilometres travelled in the year 2000 at 9760–11590 m height (from the
QUANTIFY emissions inventory)
High air traffic Low air traffic
Million km
travelled
Fraction (%) of
global
Million km
travelled
Fraction (%) of
global
North America 4448 28.1 631 4.0
Europe 2322 14.7 634 4.0
North Atlantic 1019 6.4 321 2.0
North Pacific 347 2.2 152 1.0
All regions above
8136 51.4 1738 11.0
Global 15837
830 K. Eleftheratos et al.
1982 1985 1988 1991 1994 1997 2000 2003 2006 2009
global aviation fuel consumption
120
160
200
240
F ue lc on su m pt io n (T g)
-1.4
0
1.4
D if fe re nc es of %
differences HIGH-LOW
10
12
14
C ir ru s co ve ra ge (% )
LOW air traffic corridors
10
12
14
C ir ru s co ve ra ge (% )
HIGH air traffic corridors
(+0.6% per decade)
(-0.3% per decade)
(+0.9% per decade)
Fig. 61.1 Annual mean cirrus cloud cover averaged over high and over low air traffic regions in North America, Europe, North Atlantic and North Pacific in comparison to the global air traffic
fuel consumption
Table 61.3 Trends in cirrus cloud cover (% per decade) and mean cirrus coverage (%) over high and low air traffic corridors
1984–2007
High air traffic Low air traffic
Trend differenceTrend Mean Trend Mean
North America +0.7 (99%) 18.7 +0.1 (�) 17.4 +0.6 (95%) Europe +0.6 (99%) 10.3 �0.3 (95%) 7.7 +0.9 (99%) North Atlantic +0.5 (99%) 10.4 �0.4 (90%) 12.6 +0.9 (99%) North Pacific +0.3 (�) 7.1 �0.6 (99%) 10.1 +0.9 (99%) All regions above +0.6 (99%) 11.7 �0.3 (95%) 12.0 +0.9 (99%) Values in brackets refer to statistical significance of each trend
61 Manmade Changes in Cirrus Clouds from 1984 to 2007: A Preliminary Study 831
We also examined the seasonal changes of cirrus cloud cover over the high and
low air traffic regions in North America, Europe, North Atlantic and North Pacific
in comparison to the seasonal distribution of kilometres travelled by high-flying
aircraft over these areas. The results are presented in Fig. 61.2.
It appears that there are positive changes in cirrus clouds over the high air traffic
regions in all seasons and negative changes over the adjacent low air traffic
counterparts. The trend differences are consistent with the differential increase in
annual mean cirrus cloud amount. It should be mentioned here that the average
percentage of cirrus cloud coverage over higher traffic areas in Europe and the US is
higher in absolute numbers than the values of the nearest lower traffic continental
regions. The difference is on the order of 2% and the average is 18%. The opposite
is true over the oceans where the absolute average of cirrus cloud cover over higher
traffic oceanic areas is about 2% less compared to that over adjacent lower traffic
oceanic regions.
The observed cloud changes could be related to changes in natural parameters.
We have studied the temporal variability of relative humidity at 250 and 300 hPa
and its relationship to changes in cirrus cloud cover. The results are presented in
Fig. 61.3 which shows the changes in annual mean cirrus cloudiness over the
examined high and low air traffic regions with respect to the changes in mean
0.4
0.8
C irr
us cl
ou d
ch an
ge (%
pe r
de ca
de )
1800
2000
2200
m ill
io n
km tr
av el
le d
by av
ia tio
n in
20 00
Cirrus changes km travelled
WINTER SPRING SUMMER AUTUMN
-0.8
-0.4
0
380
420
460
LOW air traffic regions
HIGH air traffic regions
Fig. 61.2 Seasonal changes in cirrus clouds
over the selected high and
low air traffic regions
832 K. Eleftheratos et al.
1982 1985 1988 1991 1994 1997 2000 2003 2006 2009
-60
-30
0
30
60
F u
el co
n su
m p
ti o
n d
ep ar
tu re
s fr
o m
th e
m ea
n (i
n %
)
Global air traffic fuel consumption change
-20
-10
0
10
20
C ir
ru s
cl o
u d
s d
ep ar
tu re
s fr
o m
th e
m ea
n (i
n %
)
-5
-2.5
0
2.5
5
R el
at iv
e h
u m
id it
y d
ep ar
tu re
s fr
o m
th e
m ea
n (i
n %
)
HIGH air traffic regions
-20
-10
0
10
20
C ir
ru s
cl o
u d
s d
ep ar
tu re
s fr
o m
th e
m ea
n (i
n %
)
-5
-2.5
0
2.5
5
R el
at iv
e h
u m
id it
y d
ep ar
tu re
s fr
o m
th e
m ea
n (i
n %
)
Cirrus (ISCCP) Rel. Humidity 250 & 300 (NCEP-DOE) Rel. Humidity 250 & 300 (ERA-Interim)
LOW air traffic regionsa
b
c
Fig. 61.3 Cirrus cloud changes (in % from the long-term mean) over low and high air traffic corridors with respect to corresponding changes in mean relative humidity at 250 and 300 hPa
from the NCEP-DOE and ERA-Interim Reanalysis projects and in comparison to the global air
traffic fuel consumption change
61 Manmade Changes in Cirrus Clouds from 1984 to 2007: A Preliminary Study 833
relative humidity at 250 and 300 hPa. The changes were calculated as percent
departures from the long-term mean (1984–2007). It appears that over low air
traffic regions there is general consistency between the observed changes in cirrus
clouds and the changes in mean relative humidity. On the other hand, over the high
air traffic regions the observed changes in cirrus clouds are less related to changes in
relative humidity, and they follow the course of upward trends seen in global air
traffic. The relative humidity changes at 250 and 300 hPa from the independently
produced NCEP-DOE and ERA-Interim data sets are consistent with each other.
While the greater disconnect between cirrus changes and relative humidity may in
part be due to dehydration by contrails (Schumann et al. 2015), the increase in air
traffic producing more contrails is most likely the primary cause.
Impact on Radiative Forcing
The result of manmade cirrus increase by 0.9% per decade over the western air
traffic corridors was expected to have a measurable effect in radiative forcing. We
studied the effect using the DISORT radiative transfer code (Stamnes et al. 1988;
Myhre and Stordal 2001). Meteorological data for temperature, water vapour, and
clouds were taken from ECMWF analyses and are similar to the UiO model in
Myhre et al. (2009). The cirrus optical properties are the same as in Myhre
et al. (2009). The differences in cirrus cloud cover at the end of 24 years of
increased air traffic are estimated to cause a radiative forcing of 17 mW/m2 using
an assumed optical depth of 0.4 for the additional cirrus cloud cover and 31 mW/m2
using an assumed optical depth of 1.0. Table 61.2 shows that the four regions with
highest aircraft traffic cover about 50% of the global air traffic. Under the assump-
tion that aircraft activity has the same impact in other regions as these four main
aircraft regions we estimate a global radiative forcing of 34 mW/m2 for optical
depths of 0.4 and 62 mW/m2 for optical depths of 1.0. These numbers are for
contrail-induced cirrus for the period 1984–2007. Since the contrail induced cirrus
optical depth is uncertain this causes a large uncertainty in our RF simulations. Our
lower estimate is greater than the mean estimates of radiative forcing for the
aviation-induced cirrus clouds from Minnis et al. (2004) for the period
1971–1995 (25 mW/m2), from Sausen et al. (2005) for the year 2000 (30 mW/m2
), and from Lee et al. (2009) for the year 2005 (33 mW/m2). Much of the difference
could be due to the assumed optical depth, which exceeds that of the earlier
estimates. The upper end of the range is far greater than any of the previous
estimates and is probably unrealistic.
834 K. Eleftheratos et al.
Conclusions
Manmade changes due to aviation were determined by comparing cirrus cloud
trends inside and outside of high air traffic regions in North America, Europe, North
Atlantic and North Pacific. Cirrus cloud cover increased by 0.9% per decade in the
period 1984–2007 over high air traffic regions, whereas no such change could be
detected in low air traffic areas. This estimate is in agreement with earlier studies
examining trends in cirrus cloudiness in relation to aviation (Zerefos et al. 2003;
Minnis et al. 2004; Stordal et al. 2005; Stubenrauch and Schumann 2005) despite
the differences among the examined datasets and periods of records. The resulting
manmade cirrus increase of 0.9% per decade over the western air traffic corridors
was expected to have a measurable effect in radiative forcing. Radiative forcing
calculations of the additional cloud cover due to aircraft yield a quite strong effect
of approximately +34 mW/m2 using an assumed optical depth of 0.4 for the
additional cloud cover and +62 mW/m2 for an optical depth of 1.0. Our estimates
for the RF from aviation-induced cirrus clouds are greater than those from earlier
studies (Minnis et al. 2004; Sausen et al. 2005; Lee et al. 2009). This could be due to
the assumed optical depth, which exceeds that of the earlier estimates. As such, the
upper end of the range is far greater than any of the previous estimates and is
probably unrealistic.
Acknowledgement This study was conducted within the FP6 Integrated Project QUANTIFY (003893-GOCE) funded by EU.
References
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study on natural and manmade global interannual fluctuations of cirrus cloud cover for the
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Meteorologische Zeitschrift, 14, 549–554.
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836 K. Eleftheratos et al.
Chapter 62
Emission Routing in Maritime Transportation
Levent Bilgili and Ugur Bugra Celebi
Introduction
Worldwide shipping activities have a major role in trading and transportation across
the globe. Beside the great benefits of ships, they play a considerable role on
environmental issues due to their great potential to produce various types of
solid, liquid and gaseous wastes such as rubbish, sludge, ballast water and air
emissions.
According to International Maritime Organization (IMO), more than 90% of
global trade is carried by ships. Besides, a dramatic improvement was observed
during the last century (IMO 2012). In a report, which is prepared by United
Nations Conference on Trade and Development (UNCTAD), it is indicated that
world seaborne trade and the world fleet grew by 3.8 and 4.1% in 2013, respec-
tively. Thus, the total trading volume and the total world fleet reach to 9.6 billion
tons and 1.69 billion DWT, respectively (UNCTAD 2014).
Industrial revolution brought new technologies and fuels for different machines.
After long centuries of human and wind power, ships began to use fossil fuels, first
coal, then liquid fuels such as heavy fuel oil (HFO), marine diesel oil (MDO) and
marine gas oil (MGO). Although these new energy sources are much stronger than
natural sources, they have considerable side effects: Gas emissions. After the
invention of internal combustion, liquid fossil fuels became more important.
L. Bilgili (*) • U.B. Celebi Yildiz Technical University, Barbaros Bulvari, Istanbul 34349, Turkey
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_62
837
Due to their carbon-based chemical structure, carbon-based gases are inevitable
end products of combustion processes. Carbon dioxide (CO2), carbon monoxide
(CO), black carbon (BC) are the most common carbon-based exhaust gas emis-
sions. Besides, due to the sulfur content of fossil fuels, sulfur-based by-products
(sulfur oxides-SOx) are produced during combustion. The amount of SOx entirely
depends on the amount of sulfur in the fossil fuel. Nitrogen oxides (NOx) are other
end products. They are formed due to air used during combustion process. NOx amount strongly depends on the combustion characteristics and quality. Poor
burning process results with the production of particulate matter (PM). PM consists
of soot, ash and micro-sized carbon particles. Besides, due to the fossil fuels’ contents, volatile organic compounds (VOC’s) are produced during combustion.
Although it has been estimated that diesel exhaust contains almost 450 different
compounds (Andreoni et al. 2008), generally some of them are considered and
investigated due to the harmful impacts on environment and human health. Carbon
dioxide, carbon monoxide, sulfur and nitrogen oxides and particulate matter are the
main harmful emissions from internal combustion process of ships’ diesel engines (Bilgili and Celebi 2014). CO2, NOx, SOx, CO, PM, VOC’s, methane (CH4), black carbon (BC) and particulate organic matter (POM) are the most dangerous exhaust
emissions for human health and environment, especially for global warming.
Shipping related air emissions strongly depend on fuel type and engine type
characteristics, characteristic combustion efficiency, characteristics of the lubricat-
ing oil, operation conditions of the ship, ship form and equipment efficiencies
(Bilgili et al. 2014).
Air emissions from ships are investigated and documented well. In a recent
study, it is estimated that there are almost 450 different types of components in ship
exhaust emission (Andreoni et al. 2008).
There are several and comprehensive studies on ship emissions amount and
their impacts on environment and human health. For nitrogen oxides Andreoni
et al. (2008), MEPC (2005); for sulfur oxides Corbett et al. (2007); for particulate
matter Schreier et al. (2007), Lauer et al. (2007), Eyring et al. (2010),
Corbett et al. (2007); for carbon dioxide and carbon monoxide AEA Energy and
Environment (2008), Miola et al. (2009), Haglind (2008) are the main and impor-
tant studies.
According to the several recent studies, the estimated amount of CO2 emission
caused by shipping is 943.5 million tons (Psaraftis and Kontovas 2009) and around
one billion tons, which corresponds the 2–4% of global emissions (Tzannatos
2010). IMO estimated that the CO2 emissions are about one billion tons in 2012
(IMO 2014). It is predicted that the ratio of shipping related CO2 emissions in
global amount will be increase to 12–18% in 2050 (Heitmann and Khalilian 2010).
Nitrogen oxides include nitrogen dioxide (NOx) and nitrogen oxide (NO). Recent
estimations presents that the amount of nitrogen oxide emissions from international
shipping is 6.87 Tg (Corbett and K€ohler 2003). It is also estimated that shipping related NOx emissions are responsible for 15% of global NOx emissions (Eyring
838 L. Bilgili and U.B. Celebi
et al. 2005). Furthermore, in a recent study it is indicated that NOx may have a
considerable effect on global warming as well as, or more than, CO2 (Henningsen
2000). Sulfur oxide emissions strongly depend on the sulfur content of fuel and
shipping activities are responsible for 6.49 Tg of SOx in terms of SO2 which
corresponds 5–8% of global SOx emissions (Corbett and K€ohler 2003). It is known that SOx emissions have an effect on global cooling (Andreoni
et al. 2008). PM has different types, named accordingly to the diameter of the
particles such as PM2.5 and PM10 that are smaller than 2.5 and 10 μm, respectively. According to recent estimations, shipping activities are responsible for 0.9–1.7
million tons of PM, annually (Endresen et al. 2003). PM has both effects on global
warming and global cooling. Especially on frequently used shipping routes, it is
observed that lower layer clouds are affected by the PM emissions, and thus,
changed their characteristics. These new clouds are called as cloud condensation
nuclei and by reflecting the solar energy back to the space, they contribute to global
cooling (Bilgili et al. 2014). VOC’s have also positive effect on global warming (AEA Energy and Environment 2008).
Mediterranean Sea may be the most important and one of the most intense basins
all over the world. It was estimated that NOx, SO2, PM and CO2 emissions were
2, 1.45, 0.157 and 87.6 million tons, respectively, in 2005 (Cofala et al. 2007).
Besides, in a recent study, it is estimated that 70, 44 and 36% of the ship traffic
occur within 200, 50 and 25 nautical miles from shore (IMO 2009). Thus, shipping
emissions must be considered in detail for especially the population that settles in
big cities near shores.
Application of the Models
In this study, it is aimed to calculate the total emissions produced during a total
80,000 DWT load by two different bulk carrier ships. While Ship A is 80,000 DWT,
Ship Bis 40,000 DWT. Table 62.1 presents the main characteristics of ships.
Table 62.1 Main characteristics of ships
Main characteristics Ship A Ship B
LOA 230 m 190 m
B 32 m 26 m
D 20 m 16 m
T 14.5 m 11.8 m
DWT 80,000 tons 40,000 tons
Main engine power 11060 kW 8825 kW
Auxiliary engine power 2160 kW 1776 kW
Speed 14.2 knots 12.75 knots
62 Emission Routing in Maritime Transportation 839
There are three main estimation methods in order to calculate the emissions:
Fuel consumption (FC) method, engine power (EP) method and energy (E) method.
FC method is totally based on fuel consumption data which is gained from the noon
reports of ships. Due to the real-time data, this method can be more reliable. EP
method depends on engine power and cruising time. E method uses the fuel
consumption data, fundamentally but focuses on the energy that is gained by
combustion. Thus, the results may be different in three methods.
Trozzi (2010) offers the two following equations for FC and EP methods,
respectively:
ETrip, i, j,m ¼ X
FCj,m,p*EFi, j,m,p � � ð62:1Þ
ETrip, i, j,m ¼ X
TP X
Pe*LFe*EFe, i, j,m,p � �h i ð62:2Þ
Equation (62.3) can be used for E method:
ETrip, i, j,m ¼ X
FCj,m,p*CVm*EFi, j,m,p � ð62:3Þ
Table 62.2 presents the meaning of abbreviations and indices of the equations.
The ships follow the route from Puerto la Cruz, Venezuela to Istanbul, Turkey
with a 5 days stop for loading in Puerto la Cruz, 7 days stop in Thessaloniki, Greece
for unloading and loading and 1 day stop in Istanbul for unloading. The route data is
real and was taken from noon reports of the ships. The distance of the route is
5244 nm from Jose Terminal to Thessaloniki and 333 nm from Thessaloniki to
Istanbul. The total distance is 5577 nm. Ship B follows the route twice to reach
80,000 DWT. Figure 62.1 presents the routes of the ships.
The emission factors that are used in this study are taken from the study of
Cooper and Gustafsson (2004) and are shown in Table 62.3 for each type of
Table 62.2 Abbreviations and indices of equations
Equation (62.1) Equation (62.2) Equation (62.3)
ETrip Emission over a complete trip (tons)
FC Fuel consumption (tons) – Fuel consumption (tons)
EF Emission factors (kg/tons) Emission factors (kg/kWh) Emission factors (Gg/tons)
i Pollutant type
j Engine type
m Fuel type
p Different phases of trip
LF – Engine load factor (%) –
P – Engine nominal power (kW) –
T – Time (hours) –
e – Engine category –
CV – – Calorific value (TJ/tons)
840 L. Bilgili and U.B. Celebi
estimation methods. Both ships’ main engines are classified as slow speed diesel engines. The auxiliary engines are classified as medium speed diesel engines. Thus,
the emission factors were chosen properly to the speeds of the engines.
Discussion
The estimations, which are calculated by using Eqs. (62.1), (62.2) and (62.3), are
shown in Tables 62.4 and 62.5 for Ship A and Ship B, respectively.
The emissions of Ship B must be multiplied by 2 due to reach the total 80,000
DWT load. In Fig. 62.2, the total emission amounts of total voyages are presented
for FC method.
Figure 62.3 presents the total emissions according to the results of EP method.
In Fig. 62.3, the total emission estimations according to E method is shown.
As it can be seen in Figs. 62.2, 62.3 and 62.4, there is a considerable difference
between the emissions of two ships when they carry the same amount of load in the
same route. Thus, it can be said that bigger ships are more efficient in terms of
emission/DWT ratio and environment issues.
In Figs. 62.5, 62.6 and 62.7, emission/DWT ratios of hip A and Ship B according
to the results of the FC, EP and E methods are presented, respectively.
Fig. 62.1 The routes of the ships. 1Puerto la Cruz; 2Thessaloniki; 3Istanbul
62 Emission Routing in Maritime Transportation 841
T a b le
6 2 .3
E m is si o n fa ct o rs
F u el
co n su m p ti o n m et h o d a
E n g in e p o w er
m et h o d b
E n er g y m et h o d c
M ai n en g in e
A u x . E n g in e
M ai n en g in e
A u x . E n g in e
M ai n en g in e
A u x . E n g in e
H F O
M D O
H F O
M D O
H F O
M D O
H F O
M D O
H F O
M D O
H F O
M D O
C O 2
3 1 7 9
3 1 7 9
3 1 7 9
3 1 7 9
6 2 0
5 8 8
7 2 2
6 9 0
7 8
7 4
7 8
7 4
C O
2 .5 4 5
2 .7 0 3
3 .9 2 4
4 .1 2 7
0 .5
0 .5
0 .9
0 .9
0 .0 6 2
0 .0 6 3
0 .1 2
0 .1 3
N O x
8 7 .1 3 6
9 1 .5 6 1
6 1 .7 2 8
6 2 .4 4 0
1 8 .1
1 7
1 4
1 3 .5
2 .1 3
2 .1 4
1 .5 1
1 .4 8
S O x
4 6
8 4 6
8 9
1 .5
1 0 .4
1 .7
1 .1
0 .1 9
1 .1
0 .1 9
P M
6 .6 6 7
1 .0 8 1
2 .2 0 3
0 .9 2 2
1 .3
0 .2
0 .5
0 .2
0 .1 6
0 .0 2 5
0 .0 5 7
0 .0 2 3
C H 4
0 .0 3 0 8
0 .0 3 2 4
0 .0 1 7 6
0 .0 1 8 4
0 .0 0 6
0 .0 0 6
0 .0 0 4
0 .0 0 4
0 .0 0 0 7 5
0 .0 0 0 7 6
0 .0 0 0 4 5
0 .0 0 0 4 6
N M V O C
1 .5 2 5
1 .6 2 2
0 .8 7 1
0 .9 1 6
0 .3
0 .3
0 .2
0 .2
0 .0 3 7
0 .0 3 8
0 .0 2 2
0 .0 2 3
a k g /t o n
b g /k W h
c t/ T J
842 L. Bilgili and U.B. Celebi
Conclusion
Although the ratio of total shipping activities in all kind of gaseous emissions is
relatively low, especially the main and dense shipping routes, closed basins with
high population such as Mediterranean and Aegean Seas and narrow water ways
such as Turkish Straits are in high threat in terms of deleterious emissions. The
share of shipping activities in GHG emission is low, as well. However, due to the
great harmful effects of global warming, these emissions must be considered and
minimized.
Ship emission estimation methods, which are mentioned in this study, provide
the correct amounts to a certain degree. Due to the uncertainty, as well as differ-
ences between the results of the studies, of emissions factors, the amounts of
estimated emissions may be totally different. Besides, obtaining the necessary
data for calculations is considerably difficult. In this study, one of the emission
minimization methods is investigated. Although the weather and sea conditions
have remarkable effects on ship efficiency during voyage, they are ignored in this
study. As it can be seen in Tables 62.3 and 62.4, ships produce similar amounts of
emissions. However, when considering the load amount, Ship A is much more
efficient in terms of emissions/DWT ratio, which can be used as an indicator for
Table 62.4 Emission amounts for Ship A (in tons)
Fuel consumption method Engine power method Energy method
CO2 2527.94 2363.55 2451.2
CO 2.22 1.98 2.29
NOx 65.86 67.48 63.68
SOx 34.90 32.40 32.99
PM 4.63 4.67 4.41
CH4 0.02 0.02 0.02
NMVOC 1.12 1.11 1.08
Total 2636.72 2471.24 2555.69
Table 62.5 Emission amounts for Ship B (in tons)
Fuel consumption Method Engine power method Energy method
CO2 1605.61 2647.61 1557.71
CO 1.45 2.28 1.53
NOx 41.17 74.39 39.86
SOx 20.99 34.80 19.85
PM 2.78 5.00 2.65
CH4 0.01 0.02 0.01
NMVOC 0.69 1.22 0.67
Total 1672.73 2765.35 1622.32
62 Emission Routing in Maritime Transportation 843
capacity-environment relationship. Considering the difficulty to establish a reliable
comparison between ships, indicators, such as developed in this study, are quite
important. It is obvious that bigger ships are, generally, more environmental
friendly. Although the bigger ships need more energy and material during
manufacturing process, they may provide two-way benefits and solutions for
carrying more goods with less energy and thus, emissions, in long-term.
Ship A 2,22
2,9
65,86
82,34
34,9
41,98
4,63
5,56
0,02
0,02
1,12
1,38
CO
90
0
20 30 40 50 60 70 80
NOx SOx PM CH4 NMVOC
Ship A Ship B
Ship B
4000
0
500 1000 1500 2000 2500 3000 3500
Ship A Ship B
2527,94
3211,22
2636,72
3345,46
CO2 Total
Ship A
Ship B
Fig. 62.2 Ship emissions for fuel consumption method
844 L. Bilgili and U.B. Celebi
Ship A 1,98
4,56
67,48
148,78
32,4
69,6
4,67
10
0,02
0,04
1,11
2,44
CO
160
0
20 40 60 80
100 120 140
NOx SOx PM CH4 NMVOC
Ship A Ship B
Ship B
6000
0
1000 2000 3000 4000 5000
Ship A Ship B
2363,55
5295,22
2471,24
5530,7
CO2 Total
Ship A
Ship B
Fig. 62.3 Ship emissions for engine power method
62 Emission Routing in Maritime Transportation 845
Ship A 2,29
3,06
63,68
79,72
32,99
39,7
4,41
5,3
0,02
0,02
1,08
1,34
CO
100
0 20 40 60 80
NOx SOx PM CH4 NMVOC
Ship A Ship B
Ship B
2451,2
3115,42
2555,69
3244,64
CO2 0
500 1000 1500 2000 2500 3000 3500
Total
Ship A
Ship B
Ship A Ship B
Fig. 62.4 Ship emissions for energy method
846 L. Bilgili and U.B. Celebi
Ship A 0,027
0,036
0,82
1
0,43
0,52
0,057
0,069
0,00025
0,00025
0,014
0,017
CO
1,2
0
0,2 0,4 0,6 0,8
1
NOx SOx PM CH4 NMVOC
Ship A Ship B
Ship B
50
0
10 20 30 40
Ship A Ship B
31
40
32
41
CO2 Total
Ship A
Ship B
Fig. 62.5 (Emission/DWT)*1000 values for fuel consumption method
Ship A 0,24
0,057
0,84
1,8
0,4
0,87
0,058
0,12
0,00025
0,0005
0,013
0,03
CO
2
0
0,5 1
1,5
NOx SOx PM CH4 NMVOC
Ship A Ship B
Ship B
80
0
20 40 60
Ship A Ship B
29
66
30
69
CO2 Total
Ship A
Ship B
Fig. 62.6 (Emission/DWT)*1000 values for engine power method
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Jonson, J.E., Whall, C., & Stavrakaki, A. (2007). Analysis of policy measures to reduce ship
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0,038
0,79
0,99
0,41
0,49
0,055
0,066
0,00025
0,00025
0,013
0,016
CO
1,2
0
0,2 0,4 0,6 0,8
1
NOx SOx PM CH4 NMVOC
Ship A Ship B
Ship B
50
0
10 20 30 40
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38
31
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CO2 Total
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Ship B
Fig. 62.7 (Emission/DWT)*1000 values for energy method
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056861-6.
62 Emission Routing in Maritime Transportation 849
Chapter 63
Pollution Effects Onboard and Its Generated Solution for Minimized Pollution Effect
Munir Suner and Tankut Yildiz
Introduction
Mechanics and thermal energy proficiency is very important on board. The initial
ones among the most important factors are viscosity, pollution and speed. These
(pollution, speed and viscosity) cause mechanics and thermal energy losses Also
the increase of these gives a rise to irregular turbulence and hydrodynamic rough-
ness. The hydrodynamic roughness is not a problem in regular flow, but in turbu-
lence flow besides increasing energy losses, it also causes vibration, voice
pollution, cavitation and corrosion. In addition, due to flow of fluid it results in
dynamic fatigue of materials, system failures and increasing amount of operational
costs. In this section these so important terms will be mentioned about.
In the research conducted by S.D. Sharma and others in 2003, they gathered
some useful information to help us comprehend the commencement of cavitation
observed in propellers, measurement of sound of cavitation, number of cavitation,
geometry of propellers and cavitation of turbulence much better (Sharma
et al. 2003). During a survey conducted in 2010, the resistance of cast-iron against
cavitation as well as the resistance of other metals except for iron against cavitation
were examined and the obtained values were compared to the rates of carbon steel
(Hattori and Kitagawa 2010). In a study conducted by X. Y. Li and others, the
inspection and examination of using copper-manganese and aluminum alloys used
for the method of welding to repair a vessel propeller exposed to cavitation was
performed (Li et al. 2004). In another study conducted in 2010, sorts of cavitation
M. Suner (*) ITU Maritime Faculty Marine Engineering, Tuzla, Istanbul, Turkey
e-mail: [email protected]
T. Yildiz
Alsancak Academy, Alsancak Izmir, Turkey
e-mail: [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_63
851
and the cavitation which on the rudder tiller to the increase of cavitation in line with
the acceleration of the speed of vessel were examined (Rhee et al. 2010). Ahmet
Celek examined and inspected the effects of pollution, corrosion and cavitation
which cause energy losses in his project titled “How to avoid energy losses on
vessels” in 2012 (Çelek 2013). In one study Suner M. and Birdal O. illustrated that
the impact of cavitation in ships on emissions. According to this study, the higher
cavitation lead to higher energy losses and fuel consumption. This increase in
energy loses and fuel consumption lead to higher CO2 emissions, which results in
temperature increases. Increase of CO2 will be % 0.1155. If cavitation is prevented,
it decrease consumption of fuel and this is approximately % CO2 0.040425, and the
others emission gases will also decrease. On other hand cavitation lead to depre-
cation of the systems, which lead to the wear of the materials? The worn materials
pollute the water and leads to toxicity (Suner and Birdal 2013). During a survey
conducted by Ballou and his friends (2008), Models represented powerful tools that
could aid in fuel saving. An exemplary case is the voyage and vessel optimization
system (VVOS), proven to reduce fuel consumption and related GHG emission
through optimization of vessel operation reference to ocean environment parame-
ters while recognizing ship performance criteria and safe operating limits (Ballou
et al. 2008). In the study of Harrould-Kolieb and Savitz (2010), their forecasts
demonstrated that the present IMO mitigation policy didn’t reduce emissions in the short-run. Policies regulating carbon dioxide emissions from ships were yet to see
implementation by IMO regardless of their immense emission reduction potentials
achievable via available operational and technical measures (Harrould-Kolieb and
Savitz 2010). In study of Hochkirch and Bertram (2010), the energy consuming
equipment on the ship could be reduced by adopting a number of approaches.
Energy savings could be achieved by adopting efficient electronically controlled
pumps, HVAC ventilation system, and energy saving lighting. The exhaust heat
could be used for steam generation and hot coolant could be used for producing
fresh water from sea water (Hochkirch and Bertram 2010). In one study, Mewis and
Hollenbach (2007), illustrated that the typical fuel savings was 13% for bulkers or
tankers, 16–19% for containerships, for a speed reduction of 5% (Mewis and
Hollenbach 2007). Hollenbach and Friesch (2007) illustrated that the high-
efficiency rudders such as a twisted rudder with a Costa bulb might lower power
consumption by 4% (Hollenbach and Friesch 2007). In fact, 3% of the world
emissions reductions (44 Gt CO2 per year) that is pivotal to stabilization of
temperature under 2 �C must be provided by the Shipping sector (Vergara et al. 2012; Kontovas and Psaraftis 2011). Technologies revolving around refine-
ment of mission, hull resistance reduction, prime mover and propulsion, and low
carbon new fuels are crucial recipes for mitigating maritime emissions (Vergara
et al. 2012; Kontovas and Psaraftis 2011). The design of vessels to achieve fuel
efficiency is practicable for new ships as well as those yet to be constructed by
manufactures. Apparently, historic vessels already in use prove difficult or most
probably do not lend themselves easy to engineering modifications (Kontovas and
Psaraftis 2011; Vergara et al. 2012). Adopting short-run simulations, Corbett
et al. (2009) found out that speed reductions may result in emission reduction
852 M. Suner and T. Yildiz
across a range of containership routes up to 70% and lower speeds provide CO2 reduction on most routes with higher costs when additional ships are added to
maintain scheduled frequency (Corbett et al. 2009). Arteconi et al. (2010) in their
study focused on assessing the emissions of GHG alone, comparing the use of LNG
as a fuel in heavy-duty goods vehicles instead of the diesel normally used in such
vehicles. Then they considered: (1) the life cycle of diesel fuel; (2) the life cycle of
LNG brought to Europe by methane carrier ships and collected in liquid form at the
regasification terminal (LNG-TER); (3) the life cycle of LNG produced at small-
scale liquefaction plants (LNG-SSL) installed at service stations. In study was
compared diesel and LNG fuels for use in heavy-duty vehicles in terms of GHG
emissions throughout their life-cycle, in the setting of the European market
(EU-15). For LNG, they considered two possible procurement strategies: its pur-
chase directly from the regasification terminal (LNG-TER) and its small-scale
production at the service stations (LNG-SSL). It emerged that LNG-TER afforded
a 10% reduction in GHG emissions by comparison with diesel, the majority of
which was attributable to the combustion phase in the vehicle (14%), while
emissions relating to the production phase were much the same for the two fuels,
and they were higher for LNG during the distribution phase because its procure-
ment chain is less capillary and articulated (Arteconi et al. 2013). Gangolells
et al. (2015) studied on an intelligent energy management system and applied on
underground metro stations. They saw maintenance phase had very small positive
impact (less than less than 0.5%). In any case, the impact on resources was the
largest (about 51%), whereas the human health damage category amounted to
approximately 35% and the ecosystem quality damage category represented
about 14% of the total impact (Gangolells et al. 2015). Chua et al. (2013) reviewed
the most recent developments concerning innovative cooling technologies and
strategies found in literature that could potentially lower the kW/R ton of cooling
systems. They presented intelligent air-control strategies and smart chiller sequenc-
ing methodologies that reduce the primary energy utilization for cooling. Finally,
they illustrated through various literature sources how recent efforts had gradually
but surely lowered the kW per R ton for air conditioning (Chua et al. 2015).
As it has been seen from the studies, as if in the literature, energy efficiency on
vessel, pollution effects on the environmental (emission) there isn’t any study pollution effect on injector, service pump, hydraulic cycles, Air Tower on the
Heat Transfer, turbocharger vessel so.
In this study, the effects of turbulence, corrosion, pollution and vibration
observed on vessels have been dealt with. The consideration of the significance
of the matter with the samples experienced in life and presentation of suggestions
for solving such problems are targeted. Afterwards, those events experienced on the
vessel named M/V Infinity which was 30 years old in 2014 operated by Makro
Maritime Lines, all of the incidents such as vibration, turbulence, corrosion, and
pollution and their effects on vessels with the help of data and photographs taken
and recorded on site will be examined thoroughly and those practiced suggestions
for solutions for such incidents will be considered and dealt with.
63 Pollution Effects Onboard and Its Generated Solution for Minimized Pollution. . . 853
Theory
Turbulence
As it is known; turbulence is irregular, in other words, mixed flow of fluid and
transition among flow layers. The characteristic of flow is determined by Re
number. Re number is shown in Eq. (63.1).
Re ¼ ρV:lc μ
ð63:1Þ
Here; ρ is density of fluid (kg/m2), v is speed of fluid (m/s), lc is characteristic length (m), μ is dynamics viscosity (Pa s), v is kinematic viscosity of fluid [v¼ μ/ρ] (m2/s)
On plate if Re > 500000, the flow is turbulent. In internal flow if Re > 4000 the flow is turbulent. Turbulence takes place inner and outer systems (pumps, pipe circuits, heat
exchanger, air towers propeller) on vessels. The problem that occurs on board is
basic structural element. Besides increasing energy losses; it also results in increas-
ing of coefficient energy losses, fatigue of materials and failures in systems in time.
Cavitation
While fluid is passing through an enclosed space, if it is statics pressure decreases
under the point pressure at heat, minerals and gases in fusion form in fluid turn into
balloons. Later when is goes into this balloon explode and compact and fluid with
high pressure effect, all these balloons explode. This matter is known as cavitation
(Suner and Birdal 2013). On vessels it gives arise to big wearing, vibration and
dynamic contraction, expansion, bottom area, screw propeller and valves. Also,
increases pollutions.
Corrosion
Corrosion is being effected of material characteristics as a result of a chemical and
electrochemical reaction of materials with environment in a negative way. Chem-
ical reaction is a sort of reaction in which electron deals directly with another
element in an environment where metal takes place. Metal usually gives electron to
oxygen in environment and as a results of this reaction metal oxide oxidization is
clear especially in high heats and corrosion product which appears in this situation
is known as scaling in technical language (http://www.saritas.com.tr/ktlg/pdf/
854 M. Suner and T. Yildiz
Paslanmaz%20Celik%20Saritas%2006.pdf). Corrosion is observed on outer space
(hull), especially when in contact o electric leakages with sea water, on metal and
alloys in contact with seawater and machine, equipment and parts on vessels.
Pollution
As it is known, an important part of thermal and mechanic energy losses appearing
materialize on border layer surface. During fluid flow both heat transfer and
mechanic energy losses increase and also cause increase of resistance coefficient.
This situation is an important problem in turbulence flow. Also pollution is a
problem causing different difficulties. If amount of pollution is above regular
below layer on border below layer; in other words if it is goes beyond, it takes
the name of hydrodynamic pollution. Several sources such as cargo carried in
engine, waste gas leakages in engines, seawater, oil and fuel taken are reason of
pollution. Also corrosion and wearing out are sources of pollution and they are
important problems. They cause failures such as clogging and being stuck of
mechanic parts. One hundred percent of pollution prevention cannot be possible.
Vibration
Formation of vibration is observed during operation of ship engine, in structure of
ship hull and in most mechanism. The source of this vibration is unbalanced forces
and moments. Central inertial force of masses with rotary movement, moment of
inertia forces, change of propeller trusts, engine rotation moment, insufficient
balance of ring and intermediate shaft (Mocoşoglu 2013). Rupture and refraction
appear in joining places as results of fatigue.
Applications M/V Infinity
IMO numbered vessel has been operated by Makro Shipping and Ship Management
Ltd Since 2011. The deck of the vessel is seen in Fig. 63.1 and the Engine Room is
seen in Fig. 63.2. M/V Infinity 1985 is a dry cargo vessel constructed in England.
The Liberian Flaggedand 8115215.
In the following section of the study, some sample incidents such as turbulence,
cavitation, corrosion, pollution and their effects experienced on the M/V Infinity
Vessel from October 2013 to April 2014 will be examined and dealt with the
photographs and data provided.
63 Pollution Effects Onboard and Its Generated Solution for Minimized Pollution. . . 855
Cavitation Impeller
Hammering cause’s energy and productivity losses at serious rates in pumping systems when experienced. Hammering creates worn outs Thus, it appears as an
important hinder while performing fluidal substance transfer procedures. Its impact
can be observed quite clearly on the impellers and the sockets of the impellers of the
Fig. 63.1 M/V infinity
Fig. 63.2 M/V infinivity engine room
856 M. Suner and T. Yildiz
general service pump belonging to the M/V Infinity which has not gone through
maintenance services for a long time. Those cracks and worn outs shown in
Fig. 63.3a and those worn outs shown in Fig. 63.3b caused loss of pressure. After
replacing the impeller with a new spare part and fulfilling the required maintenance,
it was observed that the pressure at the pump outlet increased approximately 1 bar.
Corrosion in General Service Pump
Owing to of the effects the high rates of chlorine in the sea water and compounds of
chlorine, high rates of humid and current oxygen content both in the air and water,
corrosion becomes a significant issue to be dealt with delicately (Craig et al. 2006).
The cases of general service pumps as shown in Fig. 63.4 and besides the sea
water of the main engine which belongs to the M/V Infinity as seen in Fig. 63.5
display an obvious sample to this situation. Both the leakages occurring in the
packing gland and the sea water given to the throttle of packing gland for protection
cause a considerable amount of corrosion in the long run and they also cause serious
worn out on the material as well as some damages such as punctures and fractures
here and there.
Therefore, it is necessary to avoid the contact of the risky parts of machines such
as the cycle pump case with sea water and also paint containing additives or
corrosion proof chemicals must be utilized in order to stop corrosion.
Fig. 63.3 (a) The impellers of the general service pump, (b) the socket of the ımpellers in the impellers and in the sockets of pumps
63 Pollution Effects Onboard and Its Generated Solution for Minimized Pollution. . . 857
Corrosion on Outer Surface of Injector
Due to the misuse of the components and apparatus on ships or losing their edges
such as the properties of sealing in time as a result of being worn out, several fresh
water and sea water leakages are likely to occur and those leakages cause corrosion
by affecting many parts of machines negatively.
Fig. 63.5 The case of the general service pump
Fig. 63.4 The case of the main engine sea water pump close view
858 M. Suner and T. Yildiz
As it is observed in Fig. 63.6, the leakage in the block of the main engine injector
cooling water cycle belonging to the M/V Infinity caused serious amount of
corrosion on the outer surface of the injector. Such corrosion incidents hinder
performing disassembling parts of the injector to maintain and corrosion also
gives damages on task performing parts of the injector in the long run and thus it
creates many important problems. For this reason, it is necessary to avoid leakages
and contact of machine parts with sea water.
Corrosion on the Deck of the Vessel
Corrosion effect of sea water causes many important problems on the deck of the
vessel and the equipment on the deck. In Fig. 63.7, the hydraulic circuit of the hatch
cover exposed to corrosion is observed. This corrosion impact exploded the links of
the cycle valve and thus both the valve and the plastic hose had to be replaced with
new ones.
Figure 63.8a, b present the effects of pollution and corrosion on the capstan
located on the poop deck can be observed. The seal of capstan (Fig. 63.10) worn
out, and resulted in oil leakage. Rust, pollution and corrosion occurred on the
equipment of the capstan because they were constantly exposed to sea water and
rain water yet no maintenance task was carried out for a long time, hydraulic oil
leakages and gear jamming occurred as shown in Fig. 63.9.
Fig. 63.6 Outer surface of the injector
63 Pollution Effects Onboard and Its Generated Solution for Minimized Pollution. . . 859
The Effect of Pollution in Air Tower on the Heat Transfer
Air Towers are utilized to cool the air of scavenge whereas turbochargers are used
to boost the amount of air in scavenges both of which are adopted to increase the
efficiency and productivity of the engine.
Those three diesel generators Model VTR-250 manufactured by Daihatsu Diesel
Mfg. Co. Ltd which were installed on M/V Infinity have inter cooling systems and
those and manufactured by BBC Brown Broveri VTR-250 model have turbo-
chargers. Those turbo chargers own 22,500 rpm and maximum 630 �C working heat.
Fig. 63.7 Corrosion impact on the hydraulic cycle of the hatch cover
Fig. 63.8 (a) Corrosion impact on the gear of the capstan, (b) different view
860 M. Suner and T. Yildiz
As shown in Figs. 63.11, 63.12, 63.13, 63.14 and 63.15 those air towers,
turbochargers, turbocharger socket, and close view of the socket as well as the
scavengers of which cleaning and maintenance jobs were not performed for a long
period of time resulted in decrease in their air pressures and consequently serious
amounts of temperature increase occurred in their exhaust. Due to those
Fig. 63.9 Worn out oil seal on the capstan gear because of corrosion impact
Fig. 63.10 Gear jamming because of corrosion impact
63 Pollution Effects Onboard and Its Generated Solution for Minimized Pollution. . . 861
Fig. 63.11 Air tower
Fig. 63.12 A disassembled turbocharger
Fig. 63.13 The socket of a turbocharger
temperature increases, occasionally two generators had to be employed to perform
jobs which can be carried out by only one generator in order to avoid probable
harms and damages likely to occur because of excessive work load. In such cases,
fuel expenses rose dramatically which caused monetary losses. Besides, another
negative effect appeared since the life spans of the related machines were shortened
considerably.
As seen in Fig. 63.15, after fulfilling all sorts of necessary cleaning and main-
tenance jobs of the air towers and turbochargers of the number 3 generator properly,
Fig. 63.14 Close view of the socket of a turbocharger
Fig. 63.15 Cleaning process of air tower
63 Pollution Effects Onboard and Its Generated Solution for Minimized Pollution. . . 863
the pressure of the scavenge went up from the rate of 0.4 bar to 1.2 bar and
approximately 50 �C decrease was observed at the exhaust temperatures.
Conclusions
It has been investigated by examples that vibration, turbulence, cavitation, corro-
sion and pollution effects on board affect energy efficiency. Vibration local vibra-
tion throughout the vessel cause serious on board. On systems just after vibration it
gives arise to material worn out, rupture and refraction in long term. Systems must
be correctly fixed and hydraulic oils of vibration damper must be regularly checked
and in the critical rotating specified during ship design voyage must be kept in
minimum.
Turbulence is a problem which comes true in most of systems in which fluid flow
inside vessel and around hull and propeller vessel. It is seen in pumps, pipelines and
cantilevers where friction coefficient is high. It is reason of cavitation source,
increase of energy losses and material fatigue. Just as the problems caused by
vibration turbulence caused problems and decrease of energy. Pollution effect of
the foremost plan here and must be prevented.
Corrosion is the important cause of increase of energy losses, decrease of heat
transfer and material frazzling. Electric failures oxidization is important problems
on board. Engine and its equipment exposed to corrosion must be maintained in the
shortest time. On other hand, it has risk such as refraction, wearing and being
pierced if they aren’t maintained shortest time. These risks must be minimized projective paints must be used. Pollution is formed by external material such as
powder, waste oil, exhaust gases, scaling, biological (sea organism and creatures),
pollution, mud, and send. It is a problem that is most commonly faced with on
board. It is a matter which concern the management directly. It is an important
increase in energy losses, clogging, not carrying out function of systems and surface
friction outsides vessels.
For instance the cleaning of evaporator, which is used for fresh water production,
has provided 30% increase in fresh water production. Again as pointed out in this
study, due to clogging and stoppage of important equipment.
In other words hot carrying out its function, pollution give arise to accidents on
board. Its solution is to maintain periodically. Serpentines, filters, pumps, valves,
cooler, circuits must be regularly cleaned. This regular cleaning reduces risk of
decrease of energy losses and fuel consumption and failure of systems as a results of
energy losses pollution increases fuel amount.
Together with this situation because of use of fossil originated. Emissions
increase. On vessels its effects can be reduced. Important rates as a result of
appropriate operation and maintenance.
864 M. Suner and T. Yildiz
Acknowledgements The data, images and photographs used in this study are compiled by the author of this essay during the long term marine training voyage, actualized on board of the M/V
Infinity Vessel, from October 2013 to April 2014. We would like to present our heartfelt
gratitude to all of the seafarers and to the despondent owner, Makro Maritime Lines Ltd for
their valuable contribution.
Nomenclature
P Pressure (N/m2)
T Temperature (�C)
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866 M. Suner and T. Yildiz
Chapter 64
Carbon-Mitigating Air Transport: Analysis of Current Policy Instruments
Ioanna Pagoni and Voula Psaraki-Kalouptsidi
Introduction
In response to the increasing evolution of aviation greenhouse gas emissions and to
the current forecasts for further emissions’ growth (in nominal terms) in the future, several environmental measures have been implemented worldwide. These mea-
sures are related to technological improvements, operational efficiency improve-
ments, use of alternative fuels and economic instruments. This chapter provides an
overall review of the environmental measures implemented on aviation sector
focusing on the market-based measures for air transport discussing their character-
istics, their geographic area of applicability and their potential effect on airline
market and environment.
Economic instruments encompass a range of policy tools that allow internaliza-
tion of the environmental external costs in the context of the principle “the polluter
pays.” There are various forms of economic instruments for air transport such as
emission charges/fees, extra landing charges based on the amount of emissions,
trading schemes and voluntary carbon offsetting schemes. The extent to which
these economic policies could affect the air ticket price is an important issue and
has been studied by various researchers. Scheelhaase et al. (2010) studied the
economic impact of EU ETS on Lufthansa and Continental Airlines. The results
indicated that Lufthansa’s environmental costs are higher, due to its wide extent of operations within the EU region. Girardet and Spinler (2013) used dynamic pro-
gramming to calculate the optimal percentage of ticket price change due to changes
in kerosene’s price and carbon-dioxide (CO2) emissions’ charges. Albers
I. Pagoni (*) • V. Psaraki-Kalouptsidi Department of Transportation Planning and Engineering, School of Civil Engineering,
National Technical University of Athens, 5, Iroon Polythechniou, Zografou,
Athens 15773, Greece
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_64
867
et al. (2007) examined the impact of EU ETS on the EU and non-EU carriers’ profitability and route demand for selected routes. To capture the potential effects
on air travel demand they used values for price elasticities calculated in other
studies and concluded that on the whole the competitive implications for individual
airlines are only marginal and could not threaten any airline’s competitive position. Lu (2009) examined the impact of environmental charges on air passenger demand
using the study of six intra-European short-haul routes in two city pairs. The results
indicate that the potential demand reduction is higher for the low-cost carrier
Easyjet compared to that of full service carriers, because of its lower fares. Miyoshi
(2014) investigated the differences in terms of equity between Annex I and
non-Annex I airlines and their passengers after the implementation of EU ETS.
The author selected a specific route and constructed a logit model to estimate the
impact of travel costs increase on the route’s market share. The results demon- strated that the EU ETS is an effective instrument unless the carbon price is
very low.
This chapter contributes to the above literature by considering the effects of a
carbon scheme on a U.S. airline network encompassing the top ten air travel
markets. The associated aircraft fuel burn and CO2 emissions are computed and
the results are presented at both a disaggregate level (flight-level analysis) and an
aggregate level (market-level analysis). The computations are conducted for all
flight modes based on data from the 1st quarter of 2012. A unit carbon price is
applied to calculate the resulting carbon costs an airline has to pay in the context of
the carbon scheme. Data from a combination of databases derived from ICAO,
EUROCONTROL and U.S. Department of Transportation are used. We assume
that the carbon cost is passed onto the passengers, resulting in air fare increase. The
results indicate that the prevailing carbon price plays a critical role to the efficiency
of a carbon fee scheme. Air ticket prices are found to increase to some extent.
However, the results differ from flight to flight and from market to market,
since flights’ parameters, such as aircraft type, distance and flight profile, are differentiated.
Four-Pillar Approach for Sustainable Aviation
Most aviation organizations, aiming to achieve aviation environmental goals, rely
their initiatives on a four-pillar approach (FAA 2015; IATA 2013a; Sgouridis
et al. 2011) presented in Table 64.1. This approach is related to technological
improvements (i.e. enhanced aircraft and engine performance efficiency), opera-
tional efficiency improvements (i.e. air traffic management, fuel optimized flight
path), use of alternative fuels and deployment of market-based instruments.
868 I. Pagoni and V. Psaraki-Kalouptsidi
Technological Improvements
Technological improvements are expected to significantly contribute to fuel burn
and emissions reduction. The initiatives for improving aircraft fuel efficiency focus
on reducing aircraft weight, improving aircraft aerodynamics to reduce drag and
improving engine efficiency, to reduce fuel burn per unit thrust (Grote et al. 2014).
The evolution of newer and more fuel-efficient airframes and engines, the use of
new composite lightweight materials, the introduction of new aircraft designs are
some of the future technologies considered by aircraft, engine and equipment
manufacturers. According to IATA (2013b) the most promising airframe technol-
ogy is the deployment of “Hybrid-Wing-Body aircraft” which may offer 10–25%
fuel reduction benefits and is estimated to be market available after 2026. Among
engine technologies, the introduction of “New engine core concepts” is estimated to
provide the greatest emission reduction of around 25–30% (IATA 2013b). How-
ever, the success of such technologies strongly depends on uncertain factors such as
development status, benefits, risk and research and development costs. For exam-
ple, some technologies, such advanced airframes which are expected to have large
potential on emissions reduction, may be years away from being available, and
developing and adopting them is likely to face high development costs.
Operational Efficiency Improvements
Achieving more efficient aircraft operations is another pillar for reducing emissions
from aviation. These improvements can be achieved through optimized airline
operations, such as aircraft operational weight reductions by removing unnecessary
onboard equipment, or optimized air traffic management operations, such as fuel
optimized flight path, continuous descent approach and reduced flight delays. Both
the United States and the European Union have taken important steps towards
developing modernized air traffic management systems. In the United States,
Federal Aviation Administration (FAA) is leading a multiagency effort to transform
Table 64.1 Four-pillar approach adopted by aviation stakeholders
I. Technological Improvements II. Operational efficiency
improvements
New composite lightweight materials
New aircraft designs (improved aerodynamics and reduced
drag)
Wing configuration
Newer and more fuel-efficient engines
Operational weight reduction
Fuel optimized flight path
Continuous descent approach
More efficient air traffic man-
agement infrastructure
III. Alternative fuels IV. Market-based measures
Fuel made from plant oil, animal fat or waste organic mate-
rial such as Camelina, Jatropha, Algae, Halophytes etc
Emission charges
Cap-and-trade programs
Emission offsetting
64 Carbon-Mitigating Air Transport: Analysis of Current Policy Instruments 869
current U.S. air traffic control system to the Next Generation Air Transportation
System (NextGen). NextGen is believed to increase safety, capacity and efficiency
of the U.S. airspace system (FAA 2014). In Europe, the European Union launched
the Single European Sky initiative which de-fragments the European airspace in
order to provide air traffic conditions with lower delays, greater safety standards,
lower aircraft emissions and lower costs related to service provision (Commission
of the European Communities 2008). According to IATA (2013b), CO2 emissions
from commercial flights could be reduced by 28 million tones in 2020 through
airline operational measures.
Alternative Fuels
Sustainable alternative fuels will play a critical role in the effort of achieving
environmentally-friendly aircraft operations. Four drivers for the development of
alternative jet fuel are recognized by Hileman and Stratton (2014): economic
sustainability, environmental sustainability, energy supply diversity and competi-
tion for energy resources. Alternative fuels have lower lifecycle carbon dioxide
(CO2) emissions than conventional kerosene and thus offer the opportunity to
reduce aviation’s contribution to climate change and to air quality. However, the
widespread production and development of alternative fuels may raise several
concerns with the most important being the requirements on land and water usage
(Hileman and Stratton 2014; Rojo et al. 2015). Since the approval for commercial
use of biofuels, various airlines have experimented with using of biofuels on
commercial flights which have demonstrated that alternative fuels can be safe and
technically sound (IATA 2014a).
Market-Based Instruments
Technology, operations and alternative fuel measures are the long-term solution for
aviation’s sustainable growth. However, due to the time required for their imple- mentation, market-based measures are viewed as a short-term promising option for
reducing aviation emissions. Market-based instruments may take the form of an
emission charge, a cap-and-trade program with allowance auctions or an emission
offsetting (Carlsson and Hammar 2002; IMF 2011; GAO 2009). The aim of such
policies is to establish a price per unit of emitted CO2 and motivate airlines to adopt
low-emissions technologies on their aircraft fleet in order to reduce their emissions.
Under an emission charge on carbon dioxide (or other greenhouse gas), a fee for every tonne of carbon dioxide emitted is levied to each polluter (airline). It can be
implemented on any aircraft operation within a given airline network or an airport.
Most known examples of emissions charges include the charges imposed by
airports to airlines for their landing and take-off operations at the airports.
870 I. Pagoni and V. Psaraki-Kalouptsidi
According to economic theory, an optimal emissions charge should be set at a level
that represents the marginal damage cost of the emissions (GAO 2009).
Within a cap-and-trade program the amount of total emissions is capped to a predefined limit. Cap-and-trade programs are also known as emissions trading
schemes. The airlines are issued emission permits up to the established cap. If
they exceed the cap, they can “buy” additional emission allowances to cover the
excess between what they emit and the cap. If an airline emits less CO2 than the cap
they can “sell” the emission allowances.
Carbon offset schemes allow individuals or companies to invest in environmen- tal projects around the world in order to mitigate the carbon emissions from their
activities. In the field of air transport, there is a variety of voluntary offset programs
currently operating. At the time of ticket purchase, passengers are encouraged to
pay for the amount of CO2 emissions resulting from their travel by making
charitable contributions to several environmental projects such as forest conserva-
tion and renewable energy (IATA 2008). The use of carbon offsets can be concep-
tually related to emissions trading. However, offsetting is a voluntary activity,
undertaken by passengers in a largely unregulated environment.
The next section gives a detailed overview of the existing or under-consideration
market-based instruments in the aviation industry.
Existing or Under-Consideration Market-Based Instruments for Air Transport
European Emissions Trading Scheme (EU ETS)
The most known cap-and-trade policy is the European Union Emissions Trading
Scheme (EU ETS). In the context of the Kyoto Protocol’s requirements, EU implemented the EU ETS in 2005 which included several sectors such as power
and heat generation, mineral industries etc. (EU 2003). In 2008, the EU ETS was
expanded so that, from 2012, it would include air traffic operations, by EU and
non-EU airlines that depart from or arrive at European airports, i.e. both intra-EU
flights and between EU and non-EU airports (EU 2008). This meant that, for
example, an American air carrier operating a flight from New York to London
would still have to comply with the EU ETS. Within the EU ETS, a cap is set on the
carbon dioxide emissions from all covered flights by aircraft operators and, then,
allowances are allocated, bought or sold among the airlines.
The inclusion of non-EU airlines in the EU ETS prompted strong objections
from several countries and stakeholders in United States, China, Russia, and India.
In light of these disagreements, in 2014, the EU ETS directive was amended in
order to apply to flights that both originate and end within the European Economic
Area (EU 2014). Thus, from 2014 to 2016 flights to and from countries outside the
EU would benefit from a general exemption. All CO2 emissions from flights
64 Carbon-Mitigating Air Transport: Analysis of Current Policy Instruments 871
between airports in the EU would continue to be covered, while all overflights are
exempt (Arvanitakis and Hind 2014).
Emission Charges
Emission charges represent any charge imposed to an airline for the amount of CO2 it emits either at an airport during the Landing and Take-Off (LTO) phase (airport
charge) or during cruise (en-route charge). In other studies, emission charges may
be referred to as “emission fees” or “emission taxes.”
There are several examples of airport emission charges being applied in Europe,
with Swiss and Swedish airports having the longest history. In 1997, Zurich airport
became the first airport worldwide to introduce an NOX emission-based charge in
order to address air quality problems caused by air traffic. Later, Geneva airport
followed this measure in 1998, Bern airport in 2001, Basel airport in 2003 and
Lugano airport in 2007 (Zurich Airport n.d.). Other airports in Germany and United
Kingdom have already implemented such a policy by imposing extra landing
charges on airlines, based on their amount of emissions generated at the vicinity
of the airports. Table 64.2 presents the emission charges applied to European
airports.
Airport emission charges reflect cost externalities and aim to compensate society
for the consequences of relevant emissions. The charge at Zurich airport was
introduced to encourage airlines to use less polluting aircraft when using the airport.
At the same time, the weight-based landing fee was reduced to ensure that the
charge remained revenue-neutral for the airport (Zurich Airport n.d.).
Table 64.2 Airport emission charges in several European countries
Country Airport
Emission charge per landing or per take-off
(for 2014 or else as indicated) Start year
Switzerland Zurich 2.50 CHF per kg NOX 1997
Geneva 1.40 CHF per kg NOX 1998
Berne 3.30 CHF per kg NOX (year 2010) 2001
Lugano 3.40 CHF per kg NOX (year 2010) 2007
United Kingdom Heathrow ₤8.82 per kg NOX 2004
Gatwick ₤5.26 per kg NOX (year 2013) 2005
Germany Frankfurt 1.50€ per kg NOX 2008
Munich 2008
Cologne Bonn 2008
Hamburg 2010
Dusseldorf 2011
Denmark Copenhagen DKK 16.60 per kg NOx 2010
872 I. Pagoni and V. Psaraki-Kalouptsidi
An example of a CO2 emission charge applied to the entire part of flight (and not
only to the LTO phase at the vicinity of airports) is the Norwegian CO2 tax on
aviation fuel. It was implemented in 1999 for all domestic and international flights,
although it later withdrew the tax relating to international flights due to violation of
many bilateral aviation agreements which Norway had with other countries (OECD
2005). Along with the introduction of ETS for aviation on the 1st of January 2012,
the CO2 tax has been reduced in Norway (ICAO 2012).
Voluntary Carbon Offset Programs by Airlines
Carbon offset programs give the passengers the option to “neutralize” their propor-
tion of aircraft emissions on a particular journey. Passengers who are willing to
offset their emissions, pay an extra fee to the ticket price in order to invest in
environmental projects. These projects are usually based in developing countries
and most commonly designed to reduce future emissions.
Various airlines have already implemented voluntary carbon offset programs.
Until 2014, over 35 airlines had launched their own voluntary carbon offset
schemes (IATA 2014c); some of them are the following:
• U.S. airlines: Delta, JetBlue, United, Virgin Atlantic. • Canadian airlines: Air Canada. • European airlines: Austrian Airlines, Brussels Airlines, Easyjet, Lufthansa,
SAS, TAP Portugal.
• Australian airlines: Cathay Pacific, Jetstar, Qantas Airways, Virgin Australia. • Asian airlines: Japan Airlines, Qatar Airlines, Thai Airways. • African airlines: Kenya Airways, South African Airways.
Given that the above carbon offset schemes are not mandatory, their success, in
terms of passengers participating, may be uncertain. Reports by various airlines
demonstrate a relatively satisfactory uptake of voluntary carbon offsets. For exam-
ple, Jetstar and Virgin Australia indicate that 10% of their domestic aviation
passengers choose to offset their flights (Australian Government 2012).
Portuguese CO2 Tax
In 2014, a CO2 tax was proposed to be applied to flights departing from Portuguese
airports. According to the proposal (IATA 2014b), the CO2 levy would be imposed
as follows:
• For domestic flights (between Portuguese airports) the levy would be 3€ per passenger per flight.
64 Carbon-Mitigating Air Transport: Analysis of Current Policy Instruments 873
• For flights departing from Portugal to an airport outside of the European
Economic Area, a 15€ per passenger would be collected for each flight. • International flights departing from Portugal and arriving at airports outside
Portugal and within the European Economic Area were excluded from the
scheme.
However, the above proposal was not supported by the Portuguese Government
and thus was not implemented. Given that EU ETS was implemented in 2012 for
aviation, domestic flights within Portugal would be charged twice (both under the
EU ETS and the Portuguese CO2 tax).
ICAO Global Market-Based Measure
International Civil Aviation Organization (ICAO) recommends that as part of a
broader package of measures including new technology, more efficient operations
and better use of infrastructure, a single global market-based measure should be
agreed to address aviation’s climate impacts. Therefore, during its 38th session held in 2013, ICAO agreed on the development of a global market-based measure to
mitigate carbon emissions from international aviation. This scheme will be final-
ized and adopted at the next ICAO Assembly in 2016 and will be implemented in
2020 (Arvanitakis and Hind 2014).
Trading schemes, emission-related airport charges and en-route charge/taxes
provide regulated airlines an incentive to reduce their fuel consumption in the
most cost-effective way since they are imposed an extra cost for polluting. This
cost, which can be referred to as “carbon cost,” is related to the amount of emissions
under the scheme, the unit price of carbon and the structure of the scheme. An
airline may decide to pass the carbon cost (either fully or partially) onto the
passengers, which will lead to a ticket price increase. Ticket price increases also
occur in the case when a passenger chooses to voluntarily offset the CO2 emissions
of his air travel, via the voluntary carbon offset schemes offered by the airlines.
The extent to which airlines would pass any carbon costs to passengers through
higher fares and the way passengers would respond to these changes still need to be
investigated. The next section examines the implementation of a carbon scheme in
domestic air travel within United States and its impact on ticket prices.
Implementing an Emission Fee Scheme in United States
In this section we develop a carbon emission fee scheme for domestic flights
operating between airports in the United States by American air carriers. Although
there is currently no national market-based instrument to mitigate aviation emis-
sions in the United States, we believe that emission costs on U.S. airline market
874 I. Pagoni and V. Psaraki-Kalouptsidi
have been and may continue to be a reality. This can be explained if we consider the
impact of the existing and the planned economic instruments on the economy of
U.S. air carriers and, in some cases, the ticket prices; for example, the proposed
global market-based measure by ICAO and the existing voluntary carbon offset
programs offered to passengers by American air carriers. Furthermore, until EU
ETS amendment in 2014, American air carriers were obliged to comply with EU
ETS requirements and were imposed the extra carbon cost for every flight between
U.S. and Europe. Major U.S. airlines, including Delta, United and American
Airlines, responded to the EU ETS by introducing a $3 surcharge per passenger
for each flight under the EU ETS.
CO2 emissions are the largest and most certain of the greenhouse gas emissions
from the aviation sector. While non-CO2 emissions are potentially significant,
there currently exists a high degree of scientific uncertainty regarding their impact.
A CO2-based scheme is most likely to be compatible with other trading schemes
(i.e. ICAO global scheme, EU ETS etc.) and so enhances the potential for future
trading between schemes.
The examined emission fee scheme is implemented in a selected airline network
within U.S. This encompasses the ten most popular origin and destination cities, in
terms of passengers travelled, within the U.S. air travel market. The sample period
is the first quarter of 2012 (2012:Q1). Air traffic data is derived from publicly
available data from the U.S. Department of Transportation. The database of the
Airline Origin and Destination Survey (DB1B) is used as it includes a 10% sample
of domestic airline tickets sold by U.S. airlines including detailed data on flight
fares, itineraries (Origin, Connecting and Destination airports), air carriers and
number of passengers.
The selected flight network is given in Table 64.3 and illustrated in Fig. 64.1.
It should be noted that Fig. 64.1 illustrates not only the origin and destination
airports, which form the ten most popular routes given in Table 64.3, but also the
connecting airports of the non-direct flights. Table 64.4 presents the airports located
in the origin and destination cities of the top ten routes.
For each flight in the selected network fuel consumption and related CO2 emissions are calculated. The methodology to compute fuel burn and carbon
emissions flight-by-flight is presented in a companion paper (Pagoni and Psaraki
2015). Fuel and emissions are computed separately for Landing/Take-off phase and
the Climb-Cruise-Descent phase. The ICAO Engine Exhaust Emissions Databank
(ICAO 2014) is used to compute the fuel consumption during the Landing/Take-off
phase. For the remaining flight above 3000 feet (Climb-Cruise-Descent phase), the
EUROCONTROL’s Base of Aircraft Data (BADA) model (EUROCONTROL 2013) is used.
Then a unit carbon price is applied flight-by-flight to compute the extra carbon
costs the regulated airline has to pay to cope with the scheme. The unit carbon price
is determined based on historical price data from the well-known EU ETS. The
average unit CO2 price has fallen the last years due to the proposed EU ETS reform
in 2012 and the economic recession in EU. The average price of one EU-allowance
(one tonne of CO2) in EU ETS was 22€ in 2008 and dropped to 7.3€ in 2012
64 Carbon-Mitigating Air Transport: Analysis of Current Policy Instruments 875
(SENDECO2 2014). In this paper, a carbon price of $20 per tonne CO2 is adopted
as baseline scenario. However results are also presented for values of $10 and $50
per tonne CO2 for sensitivity purposes. We assume that each airline would pass the
100% of carbon cost onto the passengers. This is consistent with the profit
Table 64.3 Top 10 markets for the sample period 2012:Q1
Market id Origin city Destination city Passengers in our sample
1 San Francisco, CA Los Angeles, CA 619,480
2 Los Angeles, CA San Francisco, CA 616,950
3 New York City, NY Miami, FL 440,330
4 Miami, FL New York City, NY 435,280
5 New York City, NY Orlando, FL 284,290
6 Orlando, FL New York City, NY 282,530
7 Los Angeles, CA New York City, NY 275,790
8 New York City, NY Los Angeles, CA 275,020
9 Chicago, IL New York City, NY 229,460
10 New York City, NY Chicago, IL 228,120
Fig. 64.1 Illustration of the U.S. network selected for the implementation of the carbon scheme
Table 64.4 Airports included in the sample
Origin or destination city Airports included
San Francisco, CA OAK, SFO, SJC
Los Angeles, CA BUR, LAX, LGB, ONT, SNA
New York City, NY EWR, HPN, ISP, JFK, LGA, SWF
Miami, FL FLL, MIA
Orlando, FL MCO
Chicago, IL MDW, ORD
876 I. Pagoni and V. Psaraki-Kalouptsidi
maximizing behavior observed in competitive markets. The resulting fee on an
airline is determined by the product of the unit carbon price times the total amount
of CO2 emitted by the aircraft of the airline.
Results and Discussion
Flight-Level Analysis
We first present our results on individual flight-level. Direct or one-stop flights
between the top ten origin and destination cities are selected for this purpose. Each
row of Table 64.5 represents a unique flight along with the origin and destination
airports, the connecting airport (if existing), the ticketing airline, the average air
fare for the sample period (2012:Q1) and the aircraft type (for each segment). Fuel
consumption and CO2 emissions are accordingly calculated for each flight. The
estimations include all flight phases: take-off at the origin and the connecting
(if existing) airports, landing at the connecting (if existing) and destination airports
and cruise phase. At a final step, carbon emissions and carbon costs per passenger
are calculated for the three scenarios: baseline ($20 per tn CO2), low ($10 per tn
CO2) and high ($50 per tn CO2).
Figure 64.2 presents the carbon costs per passenger and the percentage change in
air fares in case the airline fully passes these costs onto the passengers. Computa-
tions refer to the baseline scenario. Figure 64.2 illustrates results derived from the
online carbon calculators by Delta, JetBlue and United airlines. These are devel-
oped from the airlines in the context of their carbon offset programs. It should be
noted that these carbon calculators do not explain their assumptions on aircraft type
used and whether the flight is direct or one-stop. Thus, differences from these
estimates are expected.
Market-Level Analysis
Fuel burn and emissions calculations are then aggregated for each of the ten
selected origin and destination markets. For each market (see also Table 64.3)
within the selected flight network, the associated CO2 emissions and the impact of
different carbon prices scenarios (low: $10, baseline: $20 and high: $50 per tonne
CO2) on average air fares and air travel demand is estimated. To compute the
impact of carbon costs on demand, price elasticity of demand is required. The value
of �1.601 is assumed based on Pagoni and Psaraki (2015). Table 64.6 presents the results of the market-level analysis. Each row refers to
the market (Origin and destination city) along with the distance flown between the
64 Carbon-Mitigating Air Transport: Analysis of Current Policy Instruments 877
T a b le
6 4 .5
C al cu la te d fu el
an d C O 2 em
is si o n s an d as so ci at ed
fe e fo r in d iv id u al
fl ig h ts
M ar k et id
O ri g in
C o n n .
D es t.
A ir li n e
F ar e [$ ]
A ir cr af t ty p e [s eg .1 /s eg .2 ]
F u el b u rn
[t n ]
C O 2 [t n ]
C O 2 [t n /p ax ]
C O 2 co st [$ /p ax ]
B as el in e
L o w
H ig h
2 L A X
– O A K
D L
1 1 0
C R J2
1 .4 9
4 .7 0
0 .1 1 8
2 .3 5
1 .1 8
5 .8 8
3 E W R
A T L
F L L
D L
1 9 2
A 3 1 9 /B 7 5 2
1 0 .4 4
3 2 .9 5
0 .2 6 5
5 .3 0
2 .6 5
1 3 .2 6
6 M C O
– L G A
B 6
1 8 0
A 3 2 1
6 .1 6
1 9 .4 6
0 .1 4 7
2 .9 5
1 .4 7
7 .3 7
7 O N T
IA H
E W R
U A
2 4 6
B 7 3 8 /B 7 3 8
1 3 .4 9
4 2 .5 9
0 .3 7 2
7 .4 5
3 .7 2
1 8 .6 2
9 O R D
– JF K
B 6
1 3 3
E 1 9 0
3 .2 7
1 0 .3 3
0 .1 1 5
2 .3 0
1 .1 5
5 .7 4
D L D el ta
A ir li n es , B 6 Je t B lu e, U A U n it ed , se g. 1/ 2 fl ig h t se g m en t 1 o r 2 , D es t d es ti n at io n ai rp o rt , C on
n co n n ec ti n g ai rp o rt
878 I. Pagoni and V. Psaraki-Kalouptsidi
cities, the total amount of CO2 emitted, the average fare increase for the three
scenarios and the corresponding average demand decrease. If the carbon price is set
to 20$/tn CO2 (baseline), one way ticket prices go up from $1.81 to $9.59, while
demand falls from 2.68 to 6.16%. More significant effects are noticed when the
carbon price is set to 50 $/tn CO2. Markets 7 and 8 will experience the greatest
impact due to the extra carbon cost as they generate the largest amount of CO2 emissions. In contrast, markets 1 and 2 impose the lowest carbon cost on the
passengers and will thus have the lowest demand drop of 2.68 % and 2.76%
respectively (for the baseline 20$/tn CO2).
The effectiveness of a carbon fee scheme program in balancing the benefits and
costs of the emission reductions depend on factors originating from its structure and
the prevailing carbon prices in the stock market. In general, a carbon fee which
8 3.5%
3.0%
2.5%
2.0%
1.5%
1.0%
0.5%
0.0%
7
6
5
4
3
C O
2 co
st [
$/ p
as se
n g
er )
A ir
f ar
e in
cr ea
se [
% ]
2
1
0 LAX-OAK/DL EWR-ATL-FLL/DL
CO2 cost (Baseline)
Air fare increase (Baseline)
CO2 cost (Airline calculators)
Air fare increase (Airline calculators)
ONT-IAH-EWR/UA ORD-JFK/B6MCO-LGA/B6
Fig. 64.2 Flight-level analysis: absolute and percentage change of air fare due to carbon fees
Table 64.6 Market-level analysis: CO2 emissions, air fare increase and travel demand decrease
Market
id
Distance
[statute
miles]
Total CO2 emissions
[tn]
Average price increase [$]
Average demand decrease
[%] (assumed price
elasticity¼�1.601)
Low Baseline High
Low
(%)
Baseline
(%)
High
(%)
1 340 69,073 0.91 1.81 4.53 �1.34 �2.68 �6.70 2 340 71,088 0.94 1.87 4.68 �1.38 �2.76 �6.90 3 1100 259,949 1.97 3.93 9.83 �1.78 �3.56 �8.91 4 1100 234,284 1.82 3.64 9.10 �1.64 �3.28 �8.20 5 975 133,901 1.73 3.46 8.65 �1.72 �3.43 �8.58 6 975 120,510 1.64 3.28 8.20 �1.63 �3.26 �8.14 7 2488 480,325 4.04 8.08 20.19 �2.60 �5.20 �13.00 8 2488 552,573 4.80 9.59 23.98 �3.08 �6.16 �15.41 9 735 71,193 1.41 2.81 7.03 �1.55 �3.09 �7.73 10 735 84,020 1.74 3.48 8.70 �1.92 �3.84 �9.60
64 Carbon-Mitigating Air Transport: Analysis of Current Policy Instruments 879
results in an extra cost for the airlines would provide them with an economic
incentive to reduce their emissions. However, the results of this paper indicate
that a carbon scheme could create strong incentives for CO2 reduction only if the
unit carbon price is set at a sufficiently high level.
Conclusions
This chapter examines the impact of a carbon scheme on air fares and air travel
demand. As a case study, a network is designed which consists of the top ten
markets, in terms of passengers travelled, within the United States. Carbon emis-
sions and resulting carbon costs are calculated for every flight operating in the
network. The results indicate that market ticket prices increase from $1.81 to $9.59
for the baseline carbon price of 20$/tn CO2. The findings confirm that the carbon
scheme will create incentives for CO2 reduction only if carbon prices are set at a
sufficiently high level. Further research examining the impact of strategic interac-
tions on carbon trading schemes is under way.
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882 I. Pagoni and V. Psaraki-Kalouptsidi
Chapter 65
Ship Life Cycle Greenhouse Gas Emissions
Stefanos Chatzinikolaou, Nikolaos Ventikos, Levent Bilgili,
and Ugur Bugra Celebi
Introduction
Ships play an indispensable role in trading and transportation across the world. Due
to the great carrying capacity, they have a wide area of utilization. It is estimated
and accepted that more than 90% of global trade is carried by ships. Throughout the
last century, the shipping industry has seen a general trend of increases in total trade
volume (IMO 2012). According to the last annual review of United Nations
Conference on Trade and Development (UNCTAD), world seaborne trade grew
by 3.8% in 2013, and the total trading volume reached to nearly 9.6 billion tons.
Similarly, the world fleet grew by 4.1% in 2013. Thus, the total world fleet reaches
to 1.69 billion DWT in January 2014 (UNCTAD 2014). The growth in population
and the global economy cause an intense demand for maritime transport. Since
shipping activities are already contributing to some important environmental
impacts, the projected growth of international shipping is expected to result in
further environmental problems in the future.
Although CH4, and N2Ox gases have much more potential for global warming,
CO2, which is the major end product of internal combustion in marine engines
should be the main focus (Helfre and Boot 2013; Edwards et al. 1996). In addition,
S. Chatzinikolaou (*) RINA SERVICES, 5, Aitolikou str., Piraeus 18545, Greece
e-mail: [email protected]
N. Ventikos
National Technical University of Athens, 9, Herron Politechniou str.,
Zografou - Athens, Greece
e-mail: [email protected]
L. Bilgili • U.B. Celebi
Yildiz Technical University, Yildiz Campus Barbaros Bulvari,
34349 Besiktas, Istanbul, Turkey
e-mail: [email protected]; [email protected]
© Springer International Publishing Switzerland 2016 P. Grammelis (ed.), Energy, Transportation and Global Warming, Green Energy and Technology, DOI 10.1007/978-3-319-30127-3_65
883
shipping activities cause numerous different air emissions such as sulfur oxides
(SOX), nitrogen oxides (NOX), particulate matter (PM) and black carbon (BC)
which have other considerable harmful effects on human health and the
environment.
Shipping-Related GHG Emissions
The main GHG emission of shipping is CO2. In 2012, it is estimated that the total
CO2 of international shipping was approximately 949 million tons. The total
GHG emissions (CO2, CH4 and N2O), is estimated at 972 million tons for this
year. Therefore, it is revealed that approximately 97.63% of the GHG emissions of
shipping are attributed to CO2. For the period 2007–2012, although CO2 from
shipping activities has increased, it accounted for only 3.1% of the annual global
CO2 and approximately 2.8% of the annual GHGs. It is also estimated that for
shipping, the average annual (2007–2012) totals for NOx (as NO2) and SOx (SO2)
are 20.9 and 11.3 million tons respectively. International shipping is estimated to
produce approximately 18.6 and 10.6 million tons of NOx (as NO2) and SOx (as SO2). Global NOx and SOx emissions from shipping activities represent about
15 and 13% of the global NOx and SOx anthropogenic emissions respectively. The
total CH4, N2O and NMVOC emissions amount is estimated approximately
at 300,000, 40,000 and 700 tons in 2012, respectively. Refrigerant and air condi-
tioning gas releases account for the majority of HFC (and HCFC) emissions from
ships. Use of SF6 and PCFs in ships is documented as rarely being used in
considerable quantities; hence these emissions are not covered in this study.
Refrigerant and air conditioning gas releases from shipping result in an additional
15 million tons of CO2 equivalent emissions. Inclusion of reefer container refrig-
erant emissions yields 13.5 and 21.8 million tons of CO2 emissions. Combustion
emissions of SOx, NOx, PM, CO and NMVOCs are also correlated with fuel
consumption patterns, with some variability according to properties of combustion
across engine types, fuel properties etc., which affect emissions substances differ-
ently (IMO 2014).
The Mediterranean Sea is an important area with respect to shipping activities
which includes vital routes of international trade. Moreover, this basin is considered
as one of the most congested sea areas of the world due to the heavy coastal and
interantional sea transportation activities. For the Mediterranean Sea, it was esti-
mated that NOx, SO2, PM and CO2 emissions were 2, 1.45, 0.157 and 87.6 million
tons, respectively, in 2005 (Cofala et al. 2007). Considering that 70, 44 and 36% of
the ship traffic occurs within 200, 50 and 25 nautical miles from shore (IMO 2009),
it is reasonable for ship air emissions to be considered and explored in detail for
their impacts to populations especially those located near the coast line.
884 S. Chatzinikolaou et al.
Emission Abatement Technologies and Legislations
Although ship air emissions represent a small part of the total global emissions, the
international shipping sector is putting effort to implement solutions for decreasing
the environmental footprint of ships and specifically control both GHG and non
GHG emissions. Despite the fact that it is impossible to eliminate the carbon-based
emissions, reductions are possible with the implementation of conventional and
innovative methods and technologies. These methods and technologies can be
divided into sub-categories according to their focus. These sub-categories are
(1) Ship Design, (2) Propulsion, (3) Machinery, (4) Operation, (5) Fuel Type.
Ship design refers more to the ship’s hull form optimization. Increasing ship size or capacity may also reduce the fuel consumption (in terms of fuel consumption per
ton-nm of cargo transported) by about 10–25%. The main advantage of this method
is that it is suitable for application to all kinds of ships (ABS 2013). Modern design
methods may facilitate improvements in propeller design, especially if design
methods progress to reliable prediction of full‐scale wake fields and hull propeller interaction, considering speed and load case ranges instead of just a single operation
point. Such improved propeller design procedures may be in place within the next
10 years. Potential savings of 0‐4% were reported in a survey among experts from ship model basins (MEPC 2011). Counter-rotating propellers (coupled counter-
rotating propellers allow for the trailing aft propeller to recover some of the energy
from the slipstream of the forward propeller); optimized propeller-hull interface
(optimized design of the hull, protruding appendages and the propeller(s) to reduce
frictional and residual resistance results in reduced hull propulsion system interfer-
ence and improved fuel consumption); optimized propeller blade sections (propel-
ler blades designed for reduced friction and cavitation reduce fuel consumption)
can be used for all types of ships and provide 12; 4 and 2% emission reduction,
respectively. Using wind power with Flettner rotor and kites may have a reduction
effect up to 30 and 20%, respectively (Crist 2009). Propeller polishing, which
provides a smooth surface and thus reduces the resistance, can decrease the
emission by 3–8% (Wang and Lutsey 2013). Machinery modifications are fre-
quently used as effective methods for reducing emissions. Although the hybrid
machinery systems (using diesel engine and fuel cells together) have a limited
effect on general efficiency, CO2 emissions can be reduced by 30%. Internal engine
modifications (IEM) (changing fuel valves with low-NOx slide valves, retard
injection, higher compression ratio, increased turbo efficiency, common rail injec-
tion, valve timing and different nozzles) have considerable effects on NOx, VOCs
and PM emissions. IEM methods can reduce the NOx emissions up to 30–40%.
Exhaust Gas Recirculation (EGR) and Selective Catalytic Reduction (SCR) tech-
nologies are accepted solutions in the industry and can reduce the NOx emission by
35 and 90–95%, respectively (Andreoni et al. 2008). From the operational mea-
sures perspective, the reduction of the service speed of the ship has also consider-
able positive effects on fuel consumption and currently it is widely applied as a
win-win solution for environmental and economic performance of the vessel.
65 Ship Life Cycle Greenhouse Gas Emissions 885
Reducing speed by 1 knot may reduce fuel consumption by 12–22% (ABS 2013).
Weather routing is a relatively easy and effective solution, which provides a
reduction by 10%. Cleaner and well-coated hulls may reduce the emission by
3–5%. Besides, overall energy awareness of the crew have a positive effect on
reducing the emission up to 10% (Crist 2009). PM emission can be reduced around
18 and 20% by reducing the sulfur content of the fuel to 1.5 and 0.5%, respectively
(ENTEC 2005).
The international law of the sea finds its highest authority in the IMO which is a
body of the United Nations (UN) appointed to set international standards for safety
and pollution. Regarding the protection of marine environment, MARPOL repre-
sents the most important IMO convention currently into force. Annex VI of
MARPOL sets limits on SOx, NOx and other emissions from marine vessel oper-
ations and prohibits deliberate emissions of ozone-depleting substances (Miola
et al. 2010). Figures 65.1 and 65.2 presents the SOx and NOx limits according to
Regulation 14 and Regulation 13, respectively.
IMO has developed two major programs for shipping-related emissions: Energy
Efficiency Design Index (EEDI) and Ship Energy Efficiency Management Plan
(SEEMP). Both mechanisms, which fall under the category “energy efficiency/
emissions standards,” are the first ever mandatory GHG regulations for the shipping
industry. These mechanisms, which came into effect on 1 January 2013, apply to all
ships of 400 tons gross tonnage and above. While the EEDI sets a minimum energy
efficiency standard for new ships, the SEEMP enables ship owners to measure
the fuel efficiency of existing ships and to monitor the effects of any changes
in operation. The EEDI, which is probably the most important measure, will
allow ship designers and builders to use the solutions that they consider most
5
4
3
2
1
0 2000 2005 2010 2015
Year
F u
el s
u lp
h u
r co
n te
n t
[% ]
2020 2025
Globally SECAS
Fig. 65.1 Current and projected restrictions on fuel sulfur content according to IMO (Haglind 2008)
886 S. Chatzinikolaou et al.
cost-efficient to comply with the regulations. Based on the EEDI, the CO2 reduction
level (grams of CO2 per ton mile) for the first phase (2015–2019) is set to 10% and
will be tightened every 5 years. The baseline is the average efficiency for ships built
between 2000 and 2010. Note that developing countries will not have to implement
the standards until 2017, allowing them time to develop shipbuilding capacity
(Helfre and Boot 2013).
Results and Discussion
Emissions from shipping are produced throughout the ship life cycle which can be
divided in four important phases: (1) Shipbuilding, (2) Operation (3) Maintenance,
and (4) Dismantling/Recycling. The emissions and wastes of these phases might be
similar in some cases but in general are different in terms of emission type and
quantities. Various types of emissions and wastes are produced in solid, liquid and
gaseous form during the life cycle phases of the ship.
Ship Life Cycle Assessment
According to the ISO framework, the LCA method is the compilation and evalu-
ation of the inputs, outputs and potential environmental impacts of a product system
18
16
14
12
10
8
6
4
2
0 0 500 1000 1500 2000 2500
Tier I Tier II Tier III
N O
x em
is si
o n
s [g
/K W
h ]
Rated engine rotational speed [rpm]
Fig. 65.2 Current and projected NOx emission limits according to IMO (Haglind 2008)
65 Ship Life Cycle Greenhouse Gas Emissions 887
throughout its life cycle (ISO 2006). LCA usually consists of four main compo-
nents: goal definition and scoping, inventory analysis, impact assessment, and
interpretation. After the identification of the system and its boundaries the inventory
analysis is formulated in order to collect information on the quantities of energy and
materials used and environmental releases (e.g., air emissions) throughout the life
cycle of the system. The impact assessment step (usually referred to as Life Cycle
Impact Assessment, LCIA) translates the inventory results into impacts and it is
realized in three mandatory steps according to the ISO standards: (a) selection of
impact categories, (b) classification, and (c) characterization. Selection of impact
categories involves the identification of relevant categories of impact for the
particular study’s needs (i.e. climate change, eutrophication acidification etc.). Classification is the assignment of inventory results to impact categories. This
should be done by assigning the inventory results that are not only exclusive to
one impact category but also relate to other impact categories, including distinction
between parallel mechanisms. Various characterization methods are available to
address different environmental impacts (the impact categories) covered by the
LCA methodology. Each one of these characterization methods uses a cause-effect
pathway and impact indicators, to produce the so called characterization factors
(CFs). Therefore, CFs are weighting factors that aggregate life cycle emissions
(De Schryver 2010). There are available a number of impact assessment methods
for use in the LCA framework which have been reported and analysed thoroughly in
the literature (Hischier et al. 2010; EC-JRC 2011). Within the maritime transport
sector, previous life cycle studies conducted (starting from the 1990s) have dem-
onstrated that the LCA method may be well employed for the environmental life
cycle evaluation of ships. Analysts agree that for a ship which is a complex system
integrating multiple systems the LCA method might become more effective by
detailing the ship system into subsystems (i.e. hull, machinery, equipment for cargo
etc.). The ship LCA experimental studies have also highlighted the significance of
the system boundaries selection which is a highly subjective process and may
drastically affect the final results (Fet 2002; Chatzinikolaou and Ventikos 2013).
The usual life span of a cargo ship is 20–25 or more years and consists of four
major stages i.e. the shipbuilding, operation, maintenance, and disposal/recycling.
The Ship LCA framework accepts that the ship (the System) is a set of incorporated
subsystems functioning throughout these life cycle stages. A subsystem is defined
as an individual unit that is part of the defined total system. Subsystems are further
detailed into system elements which themselves consist of sets of processes. The
methodology accepts that processes have an environmental footprint at any life
cycle stage which is viewed as inputs (material and energy use) and outputs (air
emissions). Processes might be the same across life cycle stages but their footprint
usually alters owing to different inputs which in effect result in different air
emissions results. The initial goal is to identify important (in terms of emissions)
processes and thoroughly explore their environmental input-output which will
thereafter allow for emissions inventory and impact results to be provided at any
other level (system element, subsystem or overall system) or life cycle stage
(Chatzinikolaou and Ventikos 2015).
888 S. Chatzinikolaou et al.
This paper places particular focus on two ship subsystems due to their impor-
tance in air emissions outcome, namely the machinery main components and the
hull subsystem (Fig. 65.3).
The hull subsystem is divided in the hull material and hull protection system
element for which corresponded processes are identified and modelled in an input-
output context. The main machinery components subsystem is divided in system
elements that correspond to the primary components of the engine room, for
example main and auxiliary engines, boilers and generators.
The Ship LCA framework initial outcome is the development of an inventory
with results of air emissions from all the identified process of the system. The
emissions covered are: carbon dioxide (CO2), carbon monoxide (CO), sulphur
dioxide (SO2), sulphur oxide (SOx), nitrogen oxide (NOx), particulate matter
(PM), methane (CH4), volatile organic compound (VOC), and non-methane vola-
tile organic compounds (NMVOC). Air emissions results can be provided for any
ship system element, subsystem, and life cycle stage. Results are also available per
year and total life cycle.
Case Study
The results of ship emissions are from previous work of Chatzinikolaou and
Ventikos (2013), (2014), and (2015) on ship life cycle assessment. They have
developed a framework for a ship LCA and conducted a case study in order to
test this framework using a recently built ship, a Panamax type oil tanker (details of
the ship are provided in Table 65.1).
The emissions produced during the life cycle of the case study ship are provided
in the following figure. This table contains results for all emissions covered in the
Fig. 65.3 Ship-related air emissions assessment from a life cycle perspective (Chatzinikolaou and Ventikos, 2014)
65 Ship Life Cycle Greenhouse Gas Emissions 889
LCA framework. The following results per life cycle stage are focusing specifically
to the CO2 emissions (Table 65.2).
For the hull subsystem the important life cycle stages are shipbuilding, mainte-
nance and disposal/recycling. The operation life cycle stage has no important
emissions contribution to this subsystem. The operation life cycle stage is very
important for the machinery subsystem due to the process of combustion of fuels in
main and auxiliary engines which is responsible for 98% of the GHG emissions of
the ship system.
GHG Emissions in Shipbuilding
The shipbuilding life cycle stage results reveal that the hull subsystem produces
larger amount of emissions compared to the construction of the machinery
sub-system. Looking deeper into the hull subsystem, the hull material system
element produces larger amount of emissions than the hull protection system
Table 65.1 Case study for ship LCA: Panamax oil tanker (Chatzinikolaou and Ventikos 2014)
Year of built 2009
Country S. Korea
General data Main particulars
Displacement (tonnes) 88,221 LBP (m) 219.00
DWT (tonnes) 74,296 Breadth (m) 32.24
Lightship (tonnes) 13,925 Depth (m) 20.60
Steel weight (tonnes) 12,022 Draught (m) 14.17
Design speed (knots) 15.30 Block coefficient CB 0.85
Machinery Main engine Auxiliary engines (3)
MAN B&W 2 Stroke 4 Stroke
Country of construction S. Korea S. Korea
Unit power (kW) 12,240 740
RPM 105 720
Weight (tonnes) 368 19.7
Table 65.2 Life cycle emission inventory—case study Panamax oil tanker
Emissions Shipbuilding Operation Maintenance Dismantling Total life cycle
CO2 Tons 2.29Eþ 04 1.06Eþ 06 9.62Eþ 03 8.51Eþ 03 1.10Eþ 06 CO Tons 4.53Eþ 02 3.17Eþ 03 8.16Eþ 01 7.72Eþ 02 4.48Eþ 03 CH4 Tons 4.06Eþ 00 2.81Eþ 01 1.48Eþ 00 2.13Eþ 00 3.58Eþ 01 NOx Tons 1.28Eþ 02 3.04Eþ 04 9.20Eþ 01 1.07Eþ 02 3.07Eþ 04 PM (all) Tons 2.29Eþ 01 2.45Eþ 03 8.69Eþ 00 2.25Eþ 01 2.51Eþ 03 SO2 Tons 1.02Eþ 02 1.57Eþ 04 7.39Eþ 01 1.28Eþ 02 1.60Eþ 04 VOC Tons 2.00Eþ 01 – 5.78Eþ 01 2.99E-01 7.81Eþ 01
890 S. Chatzinikolaou et al.
element. Steel production and elaboration is the main process with respect to air
emissions. Other processes included in the hull material system element are:
transport of steel to yard, cutting of steel, sandblasting and welding.
Coating is a major operation in any shipyard. It refers to all kinds of paint
application performed at various stages from the initial priming of the steel, to the
final paint application. Outdoor painting (layers of paint applied to the outer skin of
a ship hull), is in general higher than indoor painting (layers applied to the inner
parts of the ship). Emission calculations are based on the work of Celebi (2008). For
the ship of the case study the distribution of CO2 emissions per shipbuilding process
is shown in the following figure (Fig. 65.4). Steel production process (which is
included in the hull material system element) is responsible for nearly 90% of the
total CO2 emissions during shipbuilding.
GHG Emissions in Operation
CO2, NOx, SOx, CO, PM, VOCs, methane (CH4), PM, black carbon (BC) and
particulate organic matter (POM) are the most dangerous exhaust emissions for
human health and environment, especially for global warming. Shipping related air
emissions strongly depend on fuel type and engine type characteristics, character-
istic combustion efficiency, characteristics of the lubricating oil, operation condi-
tions of the ship, ship form and equipment efficiencies (Bilgili et al. 2014). The vast
part of emissions in the phase of operation is produced from the machinery
subsystem. Marine engines operation remains the largest source of environmental
impacts in the life cycle of the ship, representing for example 98% of the total life
cycle impact for a for a cargo vessel according to Kameyama et al. (2004). In
Fig. 65.5, emissions of CO2 in the operation phase are shown in an annual basis
(assuming a 25 years life cycle). This analysis of emissions per year demonstrates
Fig. 65.4 CO2 emissions in shipbuilding process—Panamax oil tanker vessel (Chatzinikolaou and Ventikos, 2014)
65 Ship Life Cycle Greenhouse Gas Emissions 891
that emissions are continuously increasing in intervals of 5 years which corresponds
to the typical period between major maintenance works also known as dry-docking
periods (Chatzinikolaou and Ventikos 2013). As a result, every 5 years there is an
emission peak which reflects the impact of the deterioration of the hull of the ship
due to marine growth. This phenomenon increases the frictional resistance of the
ship which in effect increases the propulsion power demand to keep the same speed.
The case study’s scenario examined in this study assumes that the ballast and laden speeds remain constant throughout the ship’s life cycle at the service speed of the ship (14 knots). This particular scenario is acknowledged that it is not reflecting the
current shipping practice; however it is the scenario that matches better to the
design specifications of this ship and can be used as a reference point for any other
real scenario of operation. Overall, 96% of the total CO2 emissions are produced
during the phase of operation (1.06 million tons) (Chatzinikolaou and Ventikos
2015).
GHG Emissions in Maintenance
Emissions in the phase of maintenance are mainly derived by the hull subsystem.
No important maintenance processes have been identified for the machinery of the
ship. The processes considered in the maintenance of the hull are identical to the
shipbuilding processes but with different input–output (use of energy and materials
and resulting emissions).
It is estimated that maintenance process is responsible for 0.01% of total CO2 emissions of a ship’s life cycle (Fig. 65.6).
Fig. 65.5 Carbon Dioxide emissions per year of operation—machinery subsystem (Panamax oil tanker vessel) (Chatzinikolaou and Ventikos 2013)
892 S. Chatzinikolaou et al.
GHG Emissions in Disposal/Recycling
If there’s no appropriate integrated system for the recycling or reusing of ship related steel, machines, auxiliaries and even furnishings, such materials will remain
unused and useless at the end of the ship’s life. In this respect, ship recycling
facilities contribute to sustainable development and represent and environmentally
friendly way of dismantling ships. At the end of a ship’s life cycle, the ship contains not only various recyclable materials but also a range of hazardous and toxic
substances. Many substances in a ship’s structure and equipment may be defined
as hazardous and toxic under the existing 1989 Basel Convention on the Control of
Transboundary Movements of Hazardous Wastes and Their Disposal. The so called
Hong Kong Convention, adopted by IMO in 2009, is the last and most important
regulation on ship recycling wastes. Environmental information regarding the final
life cycle stage of ships is generally unavailable. Owing to certain incentives
(i.e. low labour costs, imperative need for steel and second hand material) the
global ship dismantling centre is currently located in the so called Indian subcon-
tinent (India, Bangladesh, Pakistan). Some 80% or more of the end of life ships
ends up in the Indian subcontinent dismantling sites and usually takes place by
applying the beaching method which allows the demand for infrastructure (piers,
sufficient depth of the harbour, cranes etc.) to be replaced by a mud flat and a huge
labour force. The dismantling operations are based around the principle of maxi-
mum separation of the steel structure of the ship without making any use of
technology similar to shipbuilding. Safety, environmental and human health
aspects are critical in the majority of these sites. The ship recycling scenario
which has been examined in the case study of the Panamax tanker has made use
of information for the process or steel re-rolling which is common practice in these
dismantling sites. The amount of steel of the ship treated and recovered with this
specific method of re-rerolling for an oil tanker vessel ranges from 72 to 81% of the
Fig. 65.6 Carbon Dioxide emissions during maintenance periods of the Panamax tanker (Chatzinikolaou and Ventikos 2014)
65 Ship Life Cycle Greenhouse Gas Emissions 893
total steel weight of the ship (Chatzinikolaou and Ventikos 2013). The estimated
GHG emissions from the re-rolling of the case study ship are 8500 tons of CO2 and
2.13 tons CH4. It is acknowledged though, that by using only this information only
an indication of the environmental footprint of ship recycling is provided. It is also
acknowledged that the current mechanisms established in the majority of these ship
recycling sites are forming severe threats to the environment and human health at
the local level. In fact, these practices could be used as an illustrative example of the
benefits of life cycle thinking as a holistic approach of studying the ship system
(Chatzinikolaou and Ventikos 2014).
Conclusion
This work discusses important issues related to air emissions throughout the ship
life cycle with particular focus on GHG of cargo ships. Literature information is
provided as regards the contribution of the international maritime transport sector to
GHG as well as non GHG emissions and available measures that are implemented
for reducing these emissions have been also reported. This study also includes
important elements of a framework which has been developed for assessing ship air
emissions from a life cycle perspective, and some illustrative results from a case
study conducted to evaluate and test this framework.
Overall, this work aims at providing assistance to the understanding, quantifica-
tion and communication of knowledge related to shipping air emissions aspects. It
is without any doubt that adding knowledge to these issues is part of the solution to
continuously improving the efficiency of maritime transport and increasing its
benefit to the society at large.
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65 Ship Life Cycle Greenhouse Gas Emissions 895
- Preface
- Contents
- Part I: Global Warming and Climate Change: General Issues and Challenges
- Chapter 1: Urban Development Policy and Urban Sprawl in Turkey
- Introduction
- Urban Sprawl
- Urban Sprawl and Energy Consumption
- Urban Development Policy in Turkey
- Conclusion
- References
- Chapter 2: Perspectives on the Implementation of Climate Change Public Policies in Brazil
- Introduction
- Public Policies
- Perspectives and Opportunities for Mitigation
- Final Remarks
- References
- Chapter 3: 30 Years Air Temperature Data Analysis in Athens and Thessaloniki, Greece
- Introduction
- Methodology
- Results
- Conclusions
- References
- Chapter 4: Mitigation and Adaptation Policies Related to Climate Change in Greece
- Introduction
- National Greenhouse Gas Emissions
- GHG Time Series Trend Assessment
- Level of Achievement of the National Commitment Under the KP
- Effect of GHG Mitigation Policies
- Adaptation Measures for Climate Change
- References
- Chapter 5: Assessing Air Quality in the Urban Environment: the Gender Gap
- Introduction
- Gender Priorities in the European Union
- Gender Priorities in Greece
- Results and Discussion
- Gender, Air Quality and Global Warming
- Gender Balance in Environmental Decision Making
- Conclusions
- References
- Chapter 6: Promotion of Sustainability by Quantifying and Reducing the Carbon Footprint: New Practices for Organizations
- Introduction
- Diagnosis and Analysis of the Situation
- The Quantify-Reduce-Promote (QRP) Proposal
- Opportunities and Advantages
- Final Remarks
- References
- Part II: Global Warming and Climate Change: General Issues and Challenges
- Chapter 7: Group Comparison, Trends and Cluster Analysis to Understand Historical Precipitation
- Introduction
- Methodology
- Results and Discussion
- Changes in Annual Rainfall and Snowfall
- Changes in Monthly and Seasonal Distribution of Rainfall and Snowfall-Trend Analysis
- Changes in Monthly and Seasonal Distribution of Rainfall and Snowfall-Cluster Analysis
- Conclusions
- References
- Chapter 8: Ground Response to Global Warming
- Introduction
- Methodology
- Dominating Equation
- Reference Depth
- Results
- Application of Derived Equation
- Conclusions
- Nomenclature
- References
- Chapter 9: Specific Case: Regional Estimates of Global Climate Change: A Dynamical Downscaling Approach to Southeast Europe
- Introduction
- Methods
- General Circulation Model
- Regional Climate Downscaling
- Results and Discussion
- Conclusions
- References
- Part III: Global Warming and Climate Change: General Issues and Challenges
- Chapter 10: Drought Conditions in Turkey Between 2004 and 2013 Via Drought Indices Derived from Remotely Sensed Data
- Introduction
- Data and Methodology
- Results and Conclusion
- References
- Chapter 11: Carbon Foot Print of a Passanger Aircraft Engine at Landing and Take-Off Cycle
- Introduction
- Turbofan Engine and Evaluation Methodology
- Results and Discussion
- Conclusions
- Nomenclature
- References
- Chapter 12: Greenhouse Gas Emissions Trends from Waste in Greece
- Introduction
- Solid Waste Disposal on Land
- Wastewater Handling
- Waste Incineration
- Emissions Trend
- Total Emissions
- Waste Sector
- Solid Waste Disposal
- Projections
- Conclusions
- References
- Part IV: Global Warming and Climate Change: General Issues and Challenges
- Chapter 13: Development of Models for the Estimation of Global Solar Radiation Over Selected Stations in India
- Introduction
- Clear Sky Solar Radiation
- Meteorological Data
- Development of Models
- Methods of Comparison
- Root Mean Square Error (RMSE)
- Mean Bias Error (MBE)
- t-Statistics
- Results and Discussion
- Conclusions
- Nomenclature
- References
- Chapter 14: Effect of Gap Between Absorber Plate and Condenser Cover on the Performance of a Solar Still
- Introduction
- Conventional Solar Still
- Heat Transfer in a Solar Still
- Factors Affecting Performance of Solar Still
- Performance Gap
- Experimental Setup and Procedure
- Fabrication of Solar Still
- Instrumentation
- Observations
- Results and Discussion
- Conclusions
- References
- Chapter 15: Solar Assisted Organic Rankine Cycle for Power Generation: A Comparative Analysis for Natural Working Fluids
- Introduction
- Natural Refrigerants and System Description
- Thermodynamic Analysis
- Results and Discussion
- Conclusions
- References
- Chapter 16: Rainfall Trend Analysis in the Region of Curitiba Using Regional Climate Model Scenarios
- Introduction
- Methods
- Study Area and Data
- Preliminary Analysis
- Annual Analysis
- Seasonal Analysis
- Results and Discussions
- Conclusions
- References
- Chapter 17: Modelling of Wind Speed Using Artificial Neural Networks for University Campus of Burdur (Turkey)
- Introduction
- Artificial Neural Networks (ANNs)
- Study Field and Data Collection
- Application of ANNs
- Results and Discussion
- Conclusions
- References
- Chapter 18: Cultural Landscapes as a Means of Energy Reduction at Global Warming
- Introduction
- Reflection Framework
- Project Terminology, Clarifications and Limitations
- Methodology
- Valuation
- 1. Cultural Landscapes Outside the Urban Tissue
- 1.1 Alternative use of oil platforms at the end of their service life for energy retain.
- Opening Question
- Identification of the Cultural Landscape
- Summary
- 1.2 A Gateway to the Amvrakikos Gulf
- Opening Question
- Identification of the Cultural Landscape
- Ecosystem
- Human Presence and Intervention
- Today´s Picture-Ecosystem and Environmental Problems
- Ecological Reconstruction Proposal
- Urban Planning Intervention a Gateway to the Amvrakikos Gulf on the Waterfront of Preveza
- Effects on the Ecosystem
- 2. Cultural Landscapes Within the Dense Urban Tissue
- 2.1 Museum Clusters
- Opening Question
- Identification of the Cultural Landscape
- Summary
- 2.2 Rome Community Ring-Forte Portuense
- Opening Question
- Identification of the Cultural Landscape
- Proposal
- Conclusion and Suggestion
- References
- Part V: Energy Technologies and Their Effect on Global Warming
- Chapter 19: Solar-Driven Continuous Methane Reforming Reactor
- Introduction
- Concept
- Production of Monolith
- Experimental Set-up
- Conclusion
- References
- Chapter 20: Specific Applications/Examples: Use of Solar Energy in Fishing: Community Initiatives
- Research Background
- Introduction
- Problem
- Community Initiatives
- Why Solar Energy
- Techno-Economic Assessments and Pilot Trials
- Solar Power for Multi-Day Fishing Boats
- Solar Lanterns for Catamaran Fishermen and Fish Vending Women
- Fish Vending Women use Candles
- Catamaran Fishermen Use Solar Lantern
- Cost Benefit Analysis
- Solar Powered Refrigerated Trucks for the Transportation of Fresh Fish
- Features
- The Larger Picture
- Ongoing Programme
- Suggestions
- Conclusion
- References
- Chapter 21: Diagnostic of Sensors for Induction Machine Powered by Photovoltaic Generator Based on Fuzzy Logic Techniques
- Introduction
- Control of Asynchronous Machines
- Control Scheme of an Asynchronous Machine
- Induction Machine Model
- Indirect Field-Oriented Control of an Induction Machine
- Sensorless Control of the Induction Machine
- The Structure of Model Reference Adaptive System MRAS
- The Fuzzy Logic Adaptation
- Control by Fuzzy Logic
- The Fuzzification
- Inference Mechanism
- The Defuzzification
- The Fuzzy Logic Adaptation Mechanism Principle
- The Basic Rules of the Fuzzy Controller
- Modelisation and Control of Generator Photovoltaique
- Model of a Generator Photovoltaic
- GPV Control
- Simulation Results
- Conclusion
- Annexes
- References
- Chapter 22: Air Conditioning Based on Hydroxides with Solar Driving for Low GHG Emissions
- Introduction
- Solar Air Conditioning Proposal
- Description of the Hydroxide Based Solar System
- Heat Transfer Effectiveness
- Results
- Conclusion
- Nomenclature
- References
- Chapter 23: Life Cycle Analysis as a Decision Criterion for the Implementation of Solar Photovoltaic Panels in as Northeast Br...
- Introduction
- Polygeneration System
- Life Cycle Analysis
- Equipment
- Energy Utilities
- Optimization Model
- Results and Discussion
- Conclusions
- References
- Part VI: Energy Technologies and Their Effect on Global Warming
- Chapter 24: Energy Conservation Through Sunrays Reflecting Coating on Buildings
- Introduction
- Method of Examination
- Theoretical Basis of the Direct Comparative Method
- Comparison of Surfaces with Different Emissivities
- Presentation of Results
- Applications in the Thermotechnique of Buildings
- ALUMA-CHRON´s Properties
- Performance Characteristics
- Basic Uses of AL-CHR Coating
- Role of Pigment in Sun´s Rays Utilization
- Pigments and Absorption Spectra
- Results
- Conclusions
- References
- Chapter 25: Comparison of Heating and Cooling Loads of a Typical Building with TRNSYS and eQUEST
- Introduction
- Simulation Data
- Examined Building
- Results
- Main Case Comparison
- Parametric Study
- Infiltration Rate
- Building Orientation
- Insulation Thickness
- Windows Area
- Conclusions
- References
- Chapter 26: Optimum Insulation Thickness for Cooling Applications Through Exergy Analysis and Environmental Methods
- Introduction
- Modeling and Analysis
- Results and Discussion
- Conclusions
- Nomenclature
- References
- Chapter 27: Novel Tungsten Bronze Nanoparticles for ShieldingNear Infrared Ray and Decreasing CO2 Emission
- Introduction
- Experimental
- Results and Discussion
- Conclusions
- References
- Chapter 28: Modelling of a Solar Assisted Floor Heating System with TRNSYS
- Introduction
- General Information
- Examined Building
- Active Layer (Underfloor Heating System)
- Mathematical Equations
- Building
- Flat Plate Collectors
- Storage Tank
- Auxiliary Heater
- Other System Parameters
- System Description
- Results
- Area Segmentation and Heater Control Strategy
- Heater Power Analyses
- The Solar Stand-Alone Underfloor Heating System
- Conclusions
- Nomenclature
- References
- Part VII: Energy Technologies and Their Effect on Global Warming
- Chapter 29: Biogas Production from Napier Grass at Various Cutting Intervals
- Introduction
- Materials and Method
- Two-Stage Anaerobic Operation
- Analysis of Materials
- Results
- Biogas Production
- Organic Substrate Degradation
- CH4 Yield
- Annual CH4 Gas Produced per the Napier Grass Added to Reactors
- Conclusions
- References
- Chapter 30: Sustainability Assessment of Fuels Production via Hydrotreating Waste Lipids and Co-processing Waste Lipids with P...
- Introduction
- Methodology
- Inventory Data
- Renewable Diesel
- Hybrid Diesel
- Results and Discussion
- Environmental Evaluation of the Renewable Diesel and the Hybrid Diesel
- Comparison with Other Fuels
- Conclusions
- Nomenclature
- References
- Part VIII: Energy Technologies and Their Effect on Global Warming
- Chapter 31: Spark-Ignition Engine Fueled with Methane-Hydrogen Blends
- Introduction
- Experimental Facilities
- Engine Modifications
- Experimental Procedures
- CFD Code
- Combustion Model
- Computational Details
- Results and Discussion
- Test Cases Considered
- CFD Code Validation
- Engine Performance
- NO Emissions
- Combustion Analysis
- Summary and Conclusions
- References
- Chapter 32: Hydrogen Fueled Airplanes, Test Case: Aviation in Libya
- Introduction
- An Overview of Civil Aviation and Airports in Libya
- Airports in New Libya
- Hydrogen Powered Airplanes
- Rationale for Change and Development
- UNCSD RIO+20 Libya Focal Point for Sustainable Development
- Greener Skies Initiative in Libya
- Libyan Strategy
- Discussion of Case Study Survey Results from Respondents
- Concluding Remarks
- References
- Chapter 33: Perspectives of Hydrogen Automotive Applications in Croatia
- Introduction
- Global Warming
- Transition to Low-Carbon Society and Hydrogen Economy
- Description of Croatian Power System and Renewable Energy
- Hydrogen in Transport
- Methodology
- Results and Discussion
- Conclusions and Future Work
- References
- Part IX: Energy Technologies and Their Effect on Global Warming
- Chapter 34: Contribution to Multi-Criteria Evaluation of the Impacts of Air Pollution: Case of Cement Plant (Ain Touta- ALGERI...
- Introduction
- Method and Material
- Proposed Methodology
- Presentation of the AHP Method
- Application of the Methodology
- Results and Discussion
- Conclusion
- References
- Chapter 35: Environmental Impact Assessment of Electricity Production, A Case Study of Turkey
- Introduction
- Materials and Methods
- Results and Discussion
- Conclusions
- Nomenclature
- References
- Chapter 36: Hybridization of Parabolic Trough Power Plants with Natural Gas Through Integration of Industrial Gas Turbines
- Introduction
- The Site
- The Base Case Power Plant
- Solar-HTF-Cycle
- Water/Steam Cycle
- Technical Boundary Conditions
- Operational Logic
- The Base Case Power Plant with Front End Gasturbine
- Concept Layout
- Gas Turbine Selection
- The Solar Only Bench Mark Model
- Results and Discussion
- Base Case Power Plant
- Cross Comparison
- Conclusions
- HeadingsSec160002682258
- References
- Part X: Energy Technologies and Their Effect on Global Warming
- Chapter 37: Performance Analyses of CO2-N2O Cascade System for Cooling
- Introduction
- Performance Analyses of CO2-N2O Cascade
- Results and Discussion
- Conclusion
- Nomenclature
- References
- Chapter 38: Comparison of Thermal Repowering Alternatives for Thermal Power Plants
- Introduction
- Repowering Alternatives
- Feedwater Heating
- Hot Windbox
- Parallel Repowering
- Design Parameters of Soma A Thermal Power Plant
- Results
- Conclusions
- Nomenclature
- References
- Chapter 39: Experimental Study of Heat Transfer for a Non-Newtonian Fluid in a Heated Cylindrical Pipe
- Introduction
- Materials and Methods
- Conception of the Heating Conduct
- Used Product
- Results and Discussion
- Rheological Characterization of the Flowing Suspension
- Heat Transfer of in the Flow of Non Newtonien Fluids
- Nusselt Number Effect
- Profile of the Number of Nusselt According to the Number of Graetz
- Determination of the Number of Asymptotic Nusselt
- Study of the Conduction
- Conclusion
- References
- Chapter 40: The SOC Estimation of LCO Battery Based on BP Neural Network
- Introduction
- Types of Lithium Ion Batteries
- Methods for Measuring SOC
- Battery Charge/Discharge Test and Experimental Data Storage
- Design and Training of Back Propagation Neural Network
- Estimation of Battery SOC Through ANN
- Conclusion
- References
- Chapter 41: Investigating the Effect of Different Refrigerants on the Performance of a Supercritical Organic Rankine Cycle
- Introduction
- System Description
- Modeling
- Results and Discussion
- Conclusions
- Nomenclature
- References
- Part XI: Environmental Technologies Related to Global Warming
- Chapter 42: CaO-Based Sorbents for Post Combustion CO2 Capture via Carbonate Looping
- Introduction
- Experimental
- Sorbent Preparation
- Physicochemical Characterization
- Preliminary Evaluation in TGA
- Bench-Scale Testing
- Results and Discussion
- Physicochemical Characterization
- Preliminary Evaluation in TGA
- Bench-Scale Testing in a Fixed Bed Reactor
- Conclusions
- Nomenclature
- References
- Chapter 43: Kinetics of CO2 Capture by Carbon Dioxide Binding Organic Liquids
- Introduction
- Analysis
- Material and Method
- Reagents
- Kinetic Measurement
- Results and Discussion
- Activation Energies
- Conclusion
- Nomenclature
- References
- Chapter 44: Flue Gas CO2 Sequestration by Turkish Coal Fly Ashes and Anatolian Geothermal Hot Waters
- Introduction
- CO2 Sequestration and Carbonation
- Method of Mineral Sequestration
- Experimental Work
- Results and Discussion
- Conclusion
- References
- Chapter 45: Geo.: Gas Production in Offshore Reservoirs in Brazil´s Pre-salt Region
- Introduction
- Carbon Capture and Geological Storage Review
- Carbon Capture and Geological Storage (CCGS)
- CO2 Capture in the Pre-salt Fields
- Methodology
- Results
- Pre-salt Natural Gas Production
- Concluding Remarks
- References
- Part XII: Environmental Technologies Related to Global Warming
- Chapter 46: Spatial and Temporal Patterns of the Water Quality in the Hammam Boughrara Reservoir in Algeria
- Introduction
- Materials and Methods
- Presentation of the Study Site
- Sources of Pollution
- Domestic pollution
- Industrial pollution
- Agricultural pollution
- Pollution from the Moroccan side
- Data and Methods
- Results and Interpretations
- Study of Physicochemical and Biotic Parameters
- Modelisation of Water Plane
- Estimate of Tolerable and Dangerous Loads of Phosphorus Concentration in the Dam Hammam Boughrara According Vollenweider
- Simple Model of the Phosphorus Cycle (Vollenweider Model)
- The OCDE Model, 1982
- Application of Models in the Dam of Hammam Boughrara
- Adaptation of the OCDE Model for Estimating Phosphorus Concentrations Dam Hammam Boughrara
- Qualitative Predictions
- Conclusion
- References
- Chapter 47: Natural Tracers for Identifying Causes of the Quality Reduction in Groundwater Emerging Along the Aegean Volcanic ...
- Introduction
- Sampling and Analysis
- Results and Discussion
- The Origin of the Waters and the Sources of the Quality Reduction in Ground Water
- The Case of Santorini, Kos and Nisyros Islands
- The Case of Loutraki and Egina Waters
- The Case of Milos Waters
- Conclusions
- References
- Chapter 48: Experimental Study of Longitudinal Dispersion on Trapezoidal Open Channel
- Introduction
- Phenomenon of Transport in Rivers
- Experimental Setup
- Measurement Tools
- Experimental Procedure
- Hydraulic Study of Fume Flow
- Results and Discussion
- Concentration Profiles of Longitudinal Dispersion
- Discussion
- Flow Discharge Influence
- Concentration Peaks According Discharge Flow
- Discussion
- Conclusion
- Nomenclature
- References
- Chapter 49: Mygdonia Basin (N. Greece) in the View of Isotope Geochemistry
- Introduction
- Results and Discussion
- Oxygen delta18O and delta2H Isotopes
- Carbon Isotopes delta13C
- Conclusions
- References
- Chapter 50: Sustainable Management of Sewage Sludge Conditioning and Valorization
- Introduction
- Methodology
- Sewage Sludge Methanization
- Solar Drying of Sewage Sludge
- Sewage Sludge Agricultural Valorization
- Results and Discussion
- Renewable Electricity Generated from Sewage Sludge
- Sewage Sludge Dryness Induced by Solar Energy
- Biomass Production Induced by Sewage Sludge Spreading
- Conclusion
- References
- Chapter 51: Photocatalytic Degradation of Tylosin and Spiramycin in Water by Using TiO2 and ZnO Catalysts Under UV Radiation
- Introduction
- Materials and Methods
- Chemical and Reagents
- Results and Discussion
- Effect of TiO2 on the Co-degradation
- Effect of ZnO on Co-degradation
- Comparison Between ZnO and TiO2 Efficiency on the Photodegradation Process
- Conclusion
- Nomenclature
- References
- Chapter 52: Comparison Between the Photocatalytic Degradation of a Textile Dye Under Sun Light and Artificial Irradiation
- Introduction
- Materials and Measurement Method
- Chemical Reagents
- Experimental Facility
- Measurement of the Pollutant Concentration
- Results and Discussion
- Determination of the Wavelength of the BR46
- Direct Photolysis and Photocatalysis
- Photolysis of BR46
- Photocatalytic Degradation of BR46 by Sun Radiation and UV
- Influence of the Initial Concentration of the Pollutant Under Sunlight
- Effect of the Initial Concentration of the Pollutant Under UV Radiation
- Influence of the Catalyst Concentration Under Sun Radiation
- Influence of the Catalyst Concentration Under UV
- Conclusion
- References
- Chapter 53: Vulnerability and Impact of Climate Change Processes on Water Resource in Semi-Arid Areas: In Essaouira Basin (Mor...
- Introduction
- Climate Change on a Global Scale
- Climate Change in North African
- Climate Change and Essaouira Basin
- Geographic Location
- Geological Cadre
- Climate Cadre
- Piezometry
- Hydrochemistry
- Stable Isotopes
- Conclusion
- References
- Part XIII: Environmental Technologies Related to Global Warming
- Chapter 54: Experimental Study of Transverse Mixing of Pollutants in Trapezoidal Open Channel
- Introduction
- Transverse Mixing
- Notion of Mixing Zones
- Experimental Setup and Procedures
- Variables Studied
- Results and Discussion
- Flow Regimes
- Transverse Concentration Profiles
- Remarks and Interpretation
- Transverse Concentration Profiles Evolution at Downstream in Flow Direction
- Remarks and Interpretation
- Remarks and Interpretation
- Effect of Pollutant Quantity (Initial Phenol Concentration)
- Remarks and Interpretation
- Conclusion
- Nomenclature
- References
- Chapter 55: Elimination of Micropollutent Lysine Acetylsalicylate by Adsorption on Natural and Synthetical Supports
- Introduction
- Aspirin Properties
- Method and Procedure
- Results and Discussion
- Conclusions
- References
- Chapter 56: Integrated System for Optimized Data Collection and processing of End of Life Tires: Case of Greece
- Introduction
- Methodology
- Results and Discussion
- Conclusions
- References
- Chapter 57: Smart Recovery of Materials and Upgrade of Organic Compost and RDF in Existing Mechanical Biological Treatment Pla...
- Introduction
- Methodology
- Scope of the Project
- Innovation Activities
- The Technology
- Results
- Conclusions
- References
- Part XIV: Securing Sustainable Mobility to Mitigate Climate Change
- Chapter 58: Road Transport Induced GHG Emissions Calculation for Urban Transportation Networks: The Case of Athens and Thessal...
- Introduction
- Materials and Methods
- Traffic Modelling
- Emissions Modelling
- Results and Discussion
- Emissions on Micro Level
- Emissions on Macro Level
- Conclusions
- References
- Chapter 59: The Effect of Parameter Selection on Fume Formation Rate in SMAW of AH36 Shipbuilding Steel and Analysis with ANOV...
- Introduction
- Welding Types
- Welding Emissions
- Experimental Study
- Design of Experiment (L18 Taguchi Design)
- Results and Discussion
- Conclusion
- References
- Chapter 60: An Online Visualization Tool for Assessing the Robustness of Multimodal Transport Networks in Case of Extreme Weat...
- Introduction
- Outline of the Visualization Tool
- Data Needs
- Geographical Data (GD)
- Temporal Periods (TP)
- Weather Phenomena (WP)
- Weather Phenomena Categories (WPC)
- Weather Phenomena Categories Data (WPCD)
- Demand Data (DD)
- Supply Data (SD)
- Cost Data (CD)
- Time Data (TD)
- Value of Time Data (VoTD)
- Model Parameters (MP)
- User Input
- Type of Extreme Weather Event (WP)
- Location of Occurrence (LO)
- Occurrence Probability (OP)
- Duration of Impact (DI)
- Operation Reduction (OR)
- Architecture
- User Interface
- Use of Static Data
- Use of Computed Data
- Conclusions
- References
- Part XV: Securing Sustainable Mobility to Mitigate Climate Change
- Chapter 61: Manmade Changes in Cirrus Clouds from 1984 to 2007: A Preliminary Study
- Introduction
- Data Sources
- Results and Discussion
- Manmade Changes in Cirrus Clouds
- Impact on Radiative Forcing
- Conclusions
- References
- Chapter 62: Emission Routing in Maritime Transportation
- Introduction
- Application of the Models
- Discussion
- Conclusion
- References
- Chapter 63: Pollution Effects Onboard and Its Generated Solution for Minimized Pollution Effect
- Introduction
- Theory
- Turbulence
- Cavitation
- Corrosion
- Pollution
- Vibration
- Applications M/V Infinity
- Cavitation Impeller
- Corrosion in General Service Pump
- Corrosion on Outer Surface of Injector
- Corrosion on the Deck of the Vessel
- The Effect of Pollution in Air Tower on the Heat Transfer
- Conclusions
- Nomenclature
- References
- Chapter 64: Carbon-Mitigating Air Transport: Analysis of Current Policy Instruments
- Introduction
- Four-Pillar Approach for Sustainable Aviation
- Technological Improvements
- Operational Efficiency Improvements
- Alternative Fuels
- Market-Based Instruments
- Existing or Under-Consideration Market-Based Instruments for Air Transport
- European Emissions Trading Scheme (EU ETS)
- Emission Charges
- Voluntary Carbon Offset Programs by Airlines
- Portuguese CO2 Tax
- ICAO Global Market-Based Measure
- Implementing an Emission Fee Scheme in United States
- Results and Discussion
- Flight-Level Analysis
- Market-Level Analysis
- Conclusions
- References
- Chapter 65: Ship Life Cycle Greenhouse Gas Emissions
- Introduction
- Shipping-Related GHG Emissions
- Emission Abatement Technologies and Legislations
- Results and Discussion
- Ship Life Cycle Assessment
- Case Study
- GHG Emissions in Shipbuilding
- GHG Emissions in Operation
- GHG Emissions in Maintenance
- GHG Emissions in Disposal/Recycling
- Conclusion
- References