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  4. Model-based development of multifunctional fuel cell systems for more-electric-aircraft
 
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Model-based development of multifunctional fuel cell systems for more-electric-aircraft

Publikationstyp
Journal Article
Date Issued
2013-02-06
Sprache
English
Author(s)
Lüdders, Hauke Peer  
Strummel, Hendrik  
Thielecke, Frank  
Institut
Flugzeug-Systemtechnik M-7  
TORE-URI
http://hdl.handle.net/11420/6718
Journal
CEAS Aeronautical Journal  
Volume
4
Issue
2
Start Page
151
End Page
174
Citation
CEAS Aeronautical Journal 2 (4): 151-174 (2013)
Publisher DOI
10.1007/s13272-013-0062-3
Scopus ID
2-s2.0-84886636330
Publisher
Springer
© Deutsches Zentrum für Luft- und Raumfahrt e.V. 2013. This paper presents an overall methodology for the development and assessment of multifunctional fuel cell system architectures in the context of More-Electric- Aircraft. A system design method which assists all stages of the system design process is being introduced. Starting with the required functions, it supports the task to design a fuel cell system, which is assessed based on reference flight missions. This paper focusses on the sizing and optimization procedure as part of the overall system design method. The developed procedure makes use of so-called behavior models, which own the property of being self-sizing. Highlighting its advantages, this approach is compared to a ‘‘classical’’ one. Finally, a showcase application of the overall system design method illustrates its capability.
Subjects
Fuel cell system
More-Electric-Aircraft
Optimization
Self-sizing models
System engineering
DDC Class
620: Ingenieurwissenschaften
More Funding Information
Deutschland, Bundesministerium für Bildung und Forschung, BMBF Spitzencluster
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