The purpose of the present invention is to provide: a structural material for structures which is capable of attaining reductions in working time and cost in production steps and of preventing an increase in weight; a fuel tank; a main wing; and an aircraft. A rib (11) as the structural material for structures is characterized by comprising a carbon-fiber-reinforced plastic wherein the reinforcement comprises carbon fibers and the matrix comprises a plastic, and the surface of the carbon-fiber-reinforced plastic was coated with a low-viscosity surface-protective material (18) having conductivity imparted thereto.


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    Titel :

    STRUCTURAL MATERIAL FOR STRUCTURE, FUEL TANK, MAIN WING, AND AIRCRAFT


    Beteiligte:
    KAMIHARA NOBUYUKI (Autor:in) / ABE TOSHIO (Autor:in) / OKUDA AKIHISA (Autor:in) / IKADA AKIRA (Autor:in) / YAMASHITA MASAYUKI (Autor:in) / KISHIMOTO KAZUAKI (Autor:in) / KAMINO YUICHIRO (Autor:in)

    Erscheinungsdatum :

    01.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / C08J Verarbeitung , WORKING-UP



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