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.


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    Titel :

    COOLING ARCHITECTURE FOR HYDROGEN FUEL CELL-POWERED AIRCRAFT


    Weitere Titelangaben:

    KÜHLARCHITEKTUR FÜR EIN MIT WASSERSTOFFBRENNSTOFFZELLEN BETRIEBENES FLUGZEUG
    ARCHITECTURE DE REFROIDISSEMENT POUR AÉRONEF ALIMENTÉ PAR PILE À COMBUSTIBLE À HYDROGÈNE


    Beteiligte:
    TEJPAL RITISH (Autor:in)

    Erscheinungsdatum :

    2024-03-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



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