The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in quality management to be reduced, and weight increases to be prevented. The fuel tank comprises a structural member that uses a carbon fiber reinforced plastic (CFRP) (15) including a reinforcing material containing carbon fiber and a matrix containing plastic. The structural member is formed by laminating conductive sheets (17) between prepregs of the carbon fiber reinforced plastic (CFRP) (15), and being formed with a fastening hole (22) in which a bolt is fastened.


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    Titel :

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


    Weitere Titelangaben:

    KRAFTSTOFFTANK, HAUPTTRAGFLÄCHEN, FLUGZEUGRUMPF, FLUGZEUG UND BEWEGLICHER KÖRPER
    RÉSERVOIR À CARBURANT, AILES PRINCIPALES, FUSELAGE D'AÉRONEF, AÉRONEF ET CORPS MOBILE


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

    Erscheinungsdatum :

    2018-08-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B60K Anordnung oder Einbau von Antriebseinheiten oder von Kraft- bzw. Drehmomentübertragungen in Fahrzeugen , ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



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