The objective of the present invention is to provide: a fuel tank that can prevent an increase in weight and can have reduced cost and working time during a production process, a main wing; an aircraft fuselage; an aircraft, and a mobile body. The fuel tank is provided with a structural member that uses a carbon-fiber-reinforced plastic of which the reinforcing material (15) contains carbon fibers and the matrix (17) contains plastic. The matrix (17) is imparted electrical conductivity. Also, a cut surface (11a) That is of the structural member and that is formed by the strcutural member being cut may be exposed within the fuel tank where a fuel is housed.


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    Titel :

    FUEL TANK, MAIN WING, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOBILE BODY


    Weitere Titelangaben:

    KRAFTSTOFFTANK, HAUPTFLÜGEL, FLUGZEUGRUMPF, FLUGZEUG UND MOBILER KÖRPER
    RÉSERVOIR DE CARBURANT, AILE PRINCIPALE, FUSELAGE D'AÉRONEF, AÉRONEF ET CORPS MOBILE


    Beteiligte:
    KAMIHARA NOBUYUKI (Autor:in) / YAMASHITA MASAYUKI (Autor:in) / ABE TOSHIO (Autor:in) / KAMINO YUICHIRO (Autor:in)

    Erscheinungsdatum :

    2023-03-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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