A hydrogen storage tank for a hydrogen aircraft includes an outer tank, an inner tank, a first strap, and a second strap. The inner tank is disposed inside the outer tank with a space therebetween, and has a shape having a longitudinal direction. The first strap includes a first end and a second end. The first end is connected to an inner surface of the outer tank, and the second end is connected to an outer surface of the inner tank. The second strap includes a third end and a fourth end. The third end is connected to the inner surface of the outer tank, and the fourth end is connected to the outer surface of the inner tank. The first strap and the second strap extend along the longitudinal direction of the inner tank, and in the longitudinal direction, a distance between the second end and the fourth end is shorter than a distance between the first end and the third end.


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    Titel :

    HYDROGEN STORAGE TANK FOR HYDROGEN AIRCRAFT


    Weitere Titelangaben:

    WASSERSTOFFSPEICHERTANK FÜR EIN WASSERSTOFFFLUGZEUG
    RÉSERVOIR DE STOCKAGE D'HYDROGÈNE POUR AÉRONEF À HYDROGÈNE


    Beteiligte:
    KADOOKA KEISUKE (Autor:in) / MAKI KOSHIRO (Autor:in)

    Erscheinungsdatum :

    30.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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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