According to one implementation, a structure for an aircraft includes a first structural member, a second structural member coupled to the first structural member, a fastener and a conductive object. The fastener couples the first structural member to the second structural member. The fastener is inserted into an insertion hole formed in a portion where the first structural member is overlapped with the second structural member. The fastener is in electrically non-contact with the first and second structural members in the insertion hole. The conductive object is embedded inside at least either one of the first and second structural members. The conductive object prevents a spark between the fastener and each of the first and second structural members by forming a current pathway that leads current, flowing inside the at least either one of the first and second structural members, to the other structural member.


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    Titel :

    STRUCTURE FOR AIRCRAFT, METHOD OF MANUFACTURING STRUCTURE FOR AIRCRAFT AND METHOD OF MAKING DESIGN INFORMATION OF STRUCTURE FOR AIRCRAFT


    Beteiligte:
    KAWASHIMA AI (Autor:in) / AKIBA KOUSABUROU (Autor:in) / KOMABA YASUEKI (Autor:in) / HIROMATSU YOSHIAKI (Autor:in) / NISHI TAKAYUKI (Autor:in) / FUJITA HIROYASU (Autor:in)

    Erscheinungsdatum :

    2016-08-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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