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Technological aspects of gas turbine and fuel cell hybrid systems for aircraft: a review

Published online by Cambridge University Press:  03 February 2016

M. Santin ,
A. Traverso  and
A. Massardo
M. Santin
Affiliation:
TPG-DIMSET, University of Genoa, Genoa, Italy
A. Traverso
Affiliation:
TPG-DIMSET, University of Genoa, Genoa, Italy
A. Massardo
Affiliation:
TPG-DIMSET, University of Genoa, Genoa, Italy
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Abstract

The objective of this work is to make an overview of opportunities and issues related to the aeronautical application of solid oxide fuel cell hybrid systems. The great interest on fuel cells comes from their capacity of producing electric energy with high efficiency at low pollutant production. The application of these systems as full-time auxiliary power units is an interesting alternative in a future scenario, which is supposed to include a More Electric Aircraft and more restrictive environmental standards. A review of the technological aspects of this application is presented. The physical models found in literature were investigated and the results were compared and discussed.

Type
Research Article
Information
The Aeronautical Journal , Volume 112 , Issue 1134 , August 2008 , pp. 459 - 467
Copyright
Copyright © Royal Aeronautical Society 2008 

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References

1. Fuel Cell Handbook, 2004, 7th Edition. [Online], Available: http://www.netl.doe.gov, [Accessed 26 July 2006].Google Scholar
2. Adamson, K. and Crawley, G., Fuel cell today 2006 worldwide survey, Fuel Cell Today, [Online], Available: http://www.fuelcelltoday.com, [Accessed 30 January 2007].Google Scholar
3. Rajashekara, K., Hybrid fuel-cell Strategies for clean power generation, IEEE Transactions on Industry Applications, 41, (3), May 2005.Google Scholar
4. Miner, E.W. and Lewis, C.H., Liquid hydrogen fuelled aircraft — system analysis, Tech. rep., September 2003, Contract number: G4RD-CT-2000-00192.Google Scholar
5. Hyder, A.K., A Century of aerospace electrical power technology, J of Propulsion and Power, 19, (6), November 2003, AIAA-6949-855.Google Scholar
6. Saravanamutto, H.I.H., Rogers, G.F.C. and Cohen, H., Gas Turbine Theory, 5th ed. Prentice Hall, 2001.Google Scholar
7. Faleiro, L., Beyond the more electric aircraft, Aerospace America, September 2005, pp. 35–40.Google Scholar
8. Magistri, L., Traverso, A., Massardo, A.F. and Shah, R.K., Heat exchangers for fuel cell and hybrid system applications, J of Fuel Cell Sci and Tech, 3, (2), May 2006, pp 111–118.Google Scholar
9. Walsh, P.P. and Fletcher, P., Gas Turbine Performance, 2nd ed. Blackwell Science, 2004.Google Scholar
10. Costamagna, P., Magistri, L. and Massardo, A.F., Design and part-load performance of a hybrid system based on a solid oxide fuel cell reactor and a micro gas turbine, J of Power Sources, 96, June 2001, pp 352–368.Google Scholar
11. Ferrari, M.L., Traverso, A., and Massardo, A.F., Transient analysis of solid oxide fuel cell hybrids, Part B: anode recirculation model, Proceedings of ASME Turbo Expo 2004, 2004, GT2004-53716.Google Scholar
12. Magistri, L., Ferrari, M.L., Traverso, A., Costamagna, P. and Massardo, A.F., Transient analysis of solid oxide fuel cell hybrids, Part C: whole-cycle model, Proceedings of ASME Turbo Expo 2004, 2004, GT2004-53845.Google Scholar
13. Mueller, F., Brouwer, J., Jabbari, F. and Samuelsen, S., Dynamic simulation of an integrated solid oxide fuel cell system including current-based fuel flow control, Proceedings of FUELCELL 2005, 2005, FUELCELL2005-74107.Google Scholar
14. Ferrari, M., Magistri, L., Traverso, A. and Massardo, A.F., Control system for solid oxide fuel cell hybrid systems, Proceedings of ASME Turbo Expo 2005, 2005, GT2005-68102.Google Scholar
15. Stiller, C., Thorud, B., Bolland, O., Kandepub, R. and Imsland, L., Control strategy for a solid oxide fuel cell and gas turbine hybrid system, J of Power Sources, 158, (1), July 2006, pp 303–315.Google Scholar
16. Traverso, A., Massardo, A.F., Roberts, R.A., Brouwer, J. and Samuelsen, S., Gas turbine assessment for air management of pressurized SOFC/GT hybrid systems, First European Fuel Cell Conference, EFC2005-86228.Google Scholar
17. Daggett, D.L., Eelman, S. and Kristiansson, G., Fuel cell APU for commercial aircraft, AIAA International Air and Space Symposium and Exposition: The Next 100 Years, 2003, AIAA-2003-2660.Google Scholar
18. Hess, C., Technology for the good climate on board, Flug Revue Online, 1999, [Online], Available: http://www.flugrevue.rotor.com [Accessed 22 May 2007].Google Scholar
19. Freeh, J. E., Pratt, J. W., and Brouwer, J., Development of a solidoxide fuel cell/gas turbine hybrid system model for aerospace applications, Proceedings of ASME Turbo Expo 2004, 2004, GT2004-52616.Google Scholar
20. Tornabene, R., Wang, X., Steffen, C.J. and Freeh, J.E., Development of parametric mass and volume models for an aerospace SOFC/gas turbine hybrid system, Proceedings of ASME Turbo Expo 2005, 2005, GT2005-68334.Google Scholar
21. Steffen, C.J., Freeh, J.E. and Larosiliere, L.M., Solid oxide fuel cell/gas turbine hybrid technology for auxiliary aerospace power, Proceedings of ASME Turbo Expo 2005, 2005, GT2005-68619.Google Scholar
22. Freeh, J.E., Steffen, C.J. and Larosiliere, L.M., Off-design performance analysis of a solid-oxide fuel cell/gas turbine hybrid for auxiliary aerospace, Proceedings of ASME FUELCELL 2005, 2005, FUELCELL2005-74099.Google Scholar
23. Lenz, B., Bundschuh, N. and Schiller, G., Performance of a combined reformer/SOFC system for aircraft application, Sixth European Solid Oxide Fuel Cell Congress, 2004.Google Scholar
24. Bundschuh, N., Dollmayer, J. and Carl, U.B., Fuel weight penalty due to fuel cells and generators as energy source of the all-electric airplane, International Conference and Trade Fair on Hydrogen and Fuel Cell Technologies, H2 Expo 2006, Hamburg, 2006.Google Scholar
25. Nehter, P. and Winkler, W., System analysis of fuel cell APUs for aircraft applications, International Conference and Trade Fair on Hydrogen and Fuel Cell Technologies, H2 Expo 2005, Hamburg, 2005.Google Scholar
26. Nehter, P., A weight related SOFC-GT system analysis for aircraft applications, International Conference and Trade Fair on Hydrogen and Fuel Cell Technologies, H2 Expo 2006, Hamburg, 2006.Google Scholar
27. Rajashekara, K., Grieve, J. and Daggett, D., Solid oxide fuel cell/gas turbine hybrid APU system aerospace applications, IEEE IAS Annual Meeting, Seattle, October 2006.Google Scholar
28. Mak, A. and Meier, J., Fuel cell auxiliary power study, Volume 1: RASER Task Order 5, Tech. rep, February 2007, NASA/CR-2007-214461/VOL1.Google Scholar
29. Gummalla, M., et al Fuel cell airframe integration study for short-range aircraft, Volume 1: aircraft propulsion and subsystems integration evaluation, Tech. rep., September 2006, NASA/CR-2006-214457/VOL1.Google Scholar
30. Srinivasan, H., Yamanis, J., Welch, R., Tulyani, S. and Hardin, L., Solid oxide fuel cell APU feasibility study for a long range commercial aircraft using UTC ITAPS approach, Volume I: aircraft propulsion and subsystems integration evaluation, Tech rep, December 2006, NASA/CR-2006-214458/VOL1.Google Scholar