A cooling architecture for an integrated hydrogen-electric engine having a radiator and a hydrogen fuel cell includes a t and a manifold. The turbine is disposed in fluid communication with the hydrogen fuel cell. The turbine is configured to compress a predetermined amount of air and direct a first portion of the predetermined amount of the compressed air to the fuel cell for generating electricity that powers the integrated hydrogen-electric engine. The manifold is disposed in fluid communication with the turbine and positioned to direct a second portion of the predetermined amount of compressed air to the radiator for removing heat from the radiator.
COOLING ARCHITECTURE FOR HYDROGEN FUEL CELL-POWERED AIRCRAFT
KÜHLARCHITEKTUR FÜR EIN MIT WASSERSTOFFBRENNSTOFFZELLEN BETRIEBENES FLUGZEUG
ARCHITECTURE DE REFROIDISSEMENT POUR AÉRONEF ALIMENTÉ PAR PILE À COMBUSTIBLE À HYDROGÈNE
2024-03-13
Patent
Elektronische Ressource
Englisch
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