In order to enlarge a tank volume of a hydrogen powered aircraft (12), the invention proposes an aircraft tank (18) for storing cryogenic H2 which is configured as a non-circular dorsal tank. Preferably, the aircraft tank (18) is configured as a conformal fuel tank fitted to an outer contour of an aircraft fuselage (10). Further, an aircraft 12 provided with such aircraft tank 18 has been described.


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    Title :

    H2 CRYOGENIC NON CIRCULAR DORSAL TANK


    Additional title:

    KRYOGENER NICHTKREISFÖRMIGER WASSERSTOFFRÜCKENTANK
    RÉSERVOIR DORSAL NON-CIRCULAIRE D'HYDROGÈNE CRYOGÉNIQUE


    Contributors:

    Publication date :

    2025-03-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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