A composite structure includes a composite member and a fastener. The composite member has a through hole. The fastener is inserted in the through hole and couples the composite member and another part to each other. The composite member includes an electrically-conductive composite member provided at least in part or all of a through-hole portion. The through-hole portion is a portion, of the composite member, having the through hole. The electrically-conductive composite member has a thickness that is greater in a portion, of the electrically-conductive composite member, included in the through-hole portion than in a portion, of the electrically-conductive composite member, other than the through-hole portion.


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    Titel :

    COMPOSITE STRUCTURE, AIRCRAFT, AND LIGHTNING CURRENT GUIDING METHOD


    Weitere Titelangaben:

    VERBUNDSTRUKTUR, FLUGZEUG UND BLITZSTROMFÜHRUNGSVERFAHREN
    STRUCTURE COMPOSITE, AÉRONEF ET PROCÉDÉ DE GUIDAGE DE COURANT DE FOUDRE


    Beteiligte:
    TAJIRI KEISUKE (Autor:in) / HIRAKI MEGUMI (Autor:in)

    Erscheinungsdatum :

    2023-02-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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