A power system includes a liquid hydrogen fuel source including a fuel tank (14) containing a volume of hydrogen fuel (12). The fuel tank includes two or more vacuum insulation layers (52), and a liquid insulation material (54) positioned between the two or more vacuum insulation layers. A first power generator (22a) located fluidly downstream of the hydrogen fuel source. The first power generator utilizes a flow of hydrogen fuel from the volume of hydrogen fuel to generate electrical or mechanical power.


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    Title :

    AUXILLARY POWER GENERATION AND COOLING SYSTEMS ON LIQUID HYDROGEN FUELED AIRCRAFT


    Additional title:

    HILFSSTROMERZEUGUNGS- UND KÜHLSYSTEME AN MIT FLÜSSIGEM WASSERSTOFF ANGETRIEBENEN FLUGZEUGEN
    SYSTÈMES DE PRODUCTION D'ÉNERGIE AUXILIAIRE ET DE REFROIDISSEMENT SUR AÉRONEF ALIMENTÉ EN HYDROGÈNE LIQUIDE


    Contributors:

    Publication date :

    2024-02-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F17C Behälter zum Aufnehmen oder Speichern verdichteter, verflüssigter oder verfestigter Gase , VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES



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