Multifunctional fuel cell system for civil aircraft: Study of the cathode exhaust gas dehumidification

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Authors

  • H. Cruz Champion
  • S. Kabelac

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Details

Original languageEnglish
Pages (from-to)29518-29531
Number of pages14
JournalInternational Journal of Hydrogen Energy
Volume42
Issue number49
Early online date31 Oct 2017
Publication statusPublished - 7 Dec 2017

Abstract

Integration of a multifunctional fuel cell into civil aircraft as on-board power generating system is a promising opportunity to improve energy efficiency while reducing emissions. In this approach, a PEMFC would provide electrical energy during on-ground operations and emergency situations, while by-products water vapour and oxygen depleted air (ODA) would be used during flight for water generation and inerting (provision of non-inflammable atmosphere). This study presents a novel cathode exhaust gas dehumidification system based on an air cycle machine (compressor, heat exchanger, cyclone, turbine) which supplies liquid water and dry ODA for the aforementioned functions. First, feasibility of the multifunctional approach, quality of the generated water and necessary level of dehumidification are discussed. Next, real fluid property data and the system thermodynamic model are presented. Feasibility of the novel system is demonstrated with a parametric study on the effect of stoichiometry, compressor pressure ratio and turbine outlet pressure. Computed results show that: the target average O2 concentration of 10.5% (vol.) is maintained at stoichiometries below λO2≤1.8; for maximum humidity ratio xmax=0.002kgH2O/kgODA there is not risk of ice formation on condenser when compressor pressure ratio is above π ≥ 2.8. Finally, an estimation of added and potentially removed weight is given, also possible system configurations are derived.

Keywords

    Civil aviation, Dehumidification, Multifunctional fuel cell, Tank inerting, Water generation

ASJC Scopus subject areas

Sustainable Development Goals

Cite this

Multifunctional fuel cell system for civil aircraft: Study of the cathode exhaust gas dehumidification. / Cruz Champion, H.; Kabelac, S.
In: International Journal of Hydrogen Energy, Vol. 42, No. 49, 07.12.2017, p. 29518-29531.

Research output: Contribution to journalArticleResearchpeer review

Cruz Champion H, Kabelac S. Multifunctional fuel cell system for civil aircraft: Study of the cathode exhaust gas dehumidification. International Journal of Hydrogen Energy. 2017 Dec 7;42(49):29518-29531. Epub 2017 Oct 31. doi: 10.1016/j.ijhydene.2017.09.175
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title = "Multifunctional fuel cell system for civil aircraft: Study of the cathode exhaust gas dehumidification",
abstract = "Integration of a multifunctional fuel cell into civil aircraft as on-board power generating system is a promising opportunity to improve energy efficiency while reducing emissions. In this approach, a PEMFC would provide electrical energy during on-ground operations and emergency situations, while by-products water vapour and oxygen depleted air (ODA) would be used during flight for water generation and inerting (provision of non-inflammable atmosphere). This study presents a novel cathode exhaust gas dehumidification system based on an air cycle machine (compressor, heat exchanger, cyclone, turbine) which supplies liquid water and dry ODA for the aforementioned functions. First, feasibility of the multifunctional approach, quality of the generated water and necessary level of dehumidification are discussed. Next, real fluid property data and the system thermodynamic model are presented. Feasibility of the novel system is demonstrated with a parametric study on the effect of stoichiometry, compressor pressure ratio and turbine outlet pressure. Computed results show that: the target average O2 concentration of 10.5% (vol.) is maintained at stoichiometries below λO2≤1.8; for maximum humidity ratio xmax=0.002kgH2O/kgODA there is not risk of ice formation on condenser when compressor pressure ratio is above π ≥ 2.8. Finally, an estimation of added and potentially removed weight is given, also possible system configurations are derived.",
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T2 - Study of the cathode exhaust gas dehumidification

AU - Cruz Champion, H.

AU - Kabelac, S.

N1 - Funding Information: This study is part of the research project ”FUel Cell and Hydrogen Systems (FUCHS)” and was supported by the German Federal Ministry of Economic Affairs and Energy (BMWi) under the research grant 20Y1105F . Special thanks to the Airbus Fuel Cell Team for their assistance understanding aircraft architecture and requirements. In particular, the authors gratefully acknowledge Dr. Lüdders (Airbus) for initiating and supporting the work on the presented exhaust gas dehumidification concept. Publisher Copyright: © 2017 Hydrogen Energy Publications LLC Copyright: Copyright 2017 Elsevier B.V., All rights reserved.

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N2 - Integration of a multifunctional fuel cell into civil aircraft as on-board power generating system is a promising opportunity to improve energy efficiency while reducing emissions. In this approach, a PEMFC would provide electrical energy during on-ground operations and emergency situations, while by-products water vapour and oxygen depleted air (ODA) would be used during flight for water generation and inerting (provision of non-inflammable atmosphere). This study presents a novel cathode exhaust gas dehumidification system based on an air cycle machine (compressor, heat exchanger, cyclone, turbine) which supplies liquid water and dry ODA for the aforementioned functions. First, feasibility of the multifunctional approach, quality of the generated water and necessary level of dehumidification are discussed. Next, real fluid property data and the system thermodynamic model are presented. Feasibility of the novel system is demonstrated with a parametric study on the effect of stoichiometry, compressor pressure ratio and turbine outlet pressure. Computed results show that: the target average O2 concentration of 10.5% (vol.) is maintained at stoichiometries below λO2≤1.8; for maximum humidity ratio xmax=0.002kgH2O/kgODA there is not risk of ice formation on condenser when compressor pressure ratio is above π ≥ 2.8. Finally, an estimation of added and potentially removed weight is given, also possible system configurations are derived.

AB - Integration of a multifunctional fuel cell into civil aircraft as on-board power generating system is a promising opportunity to improve energy efficiency while reducing emissions. In this approach, a PEMFC would provide electrical energy during on-ground operations and emergency situations, while by-products water vapour and oxygen depleted air (ODA) would be used during flight for water generation and inerting (provision of non-inflammable atmosphere). This study presents a novel cathode exhaust gas dehumidification system based on an air cycle machine (compressor, heat exchanger, cyclone, turbine) which supplies liquid water and dry ODA for the aforementioned functions. First, feasibility of the multifunctional approach, quality of the generated water and necessary level of dehumidification are discussed. Next, real fluid property data and the system thermodynamic model are presented. Feasibility of the novel system is demonstrated with a parametric study on the effect of stoichiometry, compressor pressure ratio and turbine outlet pressure. Computed results show that: the target average O2 concentration of 10.5% (vol.) is maintained at stoichiometries below λO2≤1.8; for maximum humidity ratio xmax=0.002kgH2O/kgODA there is not risk of ice formation on condenser when compressor pressure ratio is above π ≥ 2.8. Finally, an estimation of added and potentially removed weight is given, also possible system configurations are derived.

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