In order to improve liquid hydrogen storage on aircraft (10), the invention proposes a liquid hydrogen tank (36) that is integrated into the fuselage (12) of the aircraft (10). At least one portion of the tank wall (38) is formed by specially adapted tank skin panels (42) and/or a pressure bulkhead (48). The parts forming the tank wall (38) are strengthened so as to contain a tank pressure (PLH2) of about 3 bar.


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    Title :

    FUSELAGE SECTION OF AN AIRCRAFT, AIRCRAFT FUSELAGE, AND AIRCRAFT


    Additional title:

    FLUGZEUGRUMPFABSCHNITT, FLUGZEUGRUMPF UND FLUGZEUG
    SECTION DE FUSELAGE D'UN AÉRONEF, FUSELAGE D'AÉRONEF ET AÉRONEF


    Contributors:

    Publication date :

    2023-01-04


    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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