Analysis and Design of Fuel Cell Systems for Aviation
In this paper, the design of fuel cells for the main energy supply of passenger transportation aircraft is discussed. Using a physical model of a fuel cell, general design considerations are derived. Considering different possible design objectives, the trade-off between power density and efficiency...
Main Authors: | Thomas Kadyk, Christopher Winnefeld, Richard Hanke-Rauschenbach, Ulrike Krewer |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2018-02-01
|
Series: | Energies |
Subjects: | |
Online Access: | http://www.mdpi.com/1996-1073/11/2/375 |
Similar Items
-
Modelling and Designing Cryogenic Hydrogen Tanks for Future Aircraft Applications
by: Christopher Winnefeld, et al.
Published: (2018-01-01) -
Design of Fuel Cell Systems for Aviation: Representative Mission Profiles and Sensitivity Analyses
by: Thomas Kadyk, et al.
Published: (2019-04-01) -
H2-powered aviation at airports – Design and economics of LH2 refueling systems
by: J. Hoelzen, et al.
Published: (2022-05-01) -
Resource requirements for the implementation of a global H2-powered aviation
by: F. Schenke, et al.
Published: (2023-10-01) -
H2-powered aviation – Design and economics of green LH2 supply for airports
by: J. Hoelzen, et al.
Published: (2023-10-01)