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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ТОПЛИВНЫЙ БАК, ОСНОВНЫЕ КРЫЛЬЯ, КОРПУС ЛЕТАТЕЛЬНОГО АППАРАТА, ЛЕТАТЕЛЬНЫЙ АППАРАТ И ТРАНСПОРТНОЕ СРЕДСТВО


    Erscheinungsdatum :

    27.04.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    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