A fuel tank including a structural member that uses carbon-fiber-reinforced plastic including a reinforcing material containing carbon fiber and a matrix containing a plastic, the structural member being formed by laminating a conductive sheet between prepregs of the carbon-fiber-reinforced plastic, and being formed with a fastening hole in which a bolt is fastened, and a cut surface of the structural member formed by cutting the structural member being exposed within an internal area in which fuel is stored.


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    Titel :

    FUEL TANK, MAIN WINGS, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOVING BODY


    Beteiligte:
    KAMIHARA NOBUYUKI (Autor:in) / KISHIMOTO KAZUAKI (Autor:in) / ABE TOSHIO (Autor:in) / KAMINO YUICHIRO (Autor:in)

    Erscheinungsdatum :

    2016-02-25


    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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