A hydrogen aircraft includes: an airframe including a fuselage and a wing; at least one propulsion system fixed to the airframe; a pressurized chamber disposed inside the fuselage; a pressure bulkhead that is disposed at a rear part of the pressurized chamber and has strength to withstand pressurization of the pressurized chamber; a hydrogen tank that is disposed in an accommodation section and stores liquid hydrogen, the accommodation section being installed behind the pressure bulkhead, outside the pressurized chamber, and inside the fuselage; and a supply line that supplies the liquid hydrogen stored in the hydrogen tank to the propulsion system.


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    Titel :

    HYDROGEN AIRCRAFT


    Weitere Titelangaben:

    WASSERSTOFFFLUGZEUG
    AÉRONEF À HYDROGÈNE


    Beteiligte:
    KONDO YOSHITAKA (Autor:in) / TOYODA TAKAHIRO (Autor:in) / NAKAGAWA TAKESHI (Autor:in) / KUMADA KENTA (Autor:in) / UENO YOSUKE (Autor:in) / NOMURA KAZUKI (Autor:in)

    Erscheinungsdatum :

    25.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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