STRUCTURE FOR AIRCRAFT, METHOD OF MANUFACTURING STRUCTURE FOR AIRCRAFT AND METHOD OF MAKING DESIGN INFORMATION OF STRUCTURE FOR AIRCRAFT
    1.
    发明申请
    STRUCTURE FOR AIRCRAFT, METHOD OF MANUFACTURING STRUCTURE FOR AIRCRAFT AND METHOD OF MAKING DESIGN INFORMATION OF STRUCTURE FOR AIRCRAFT 有权
    飞机结构,制造飞机结构的方法及制作飞机结构设计信息的方法

    公开(公告)号:US20160244182A1

    公开(公告)日:2016-08-25

    申请号:US15048671

    申请日:2016-02-19

    CPC classification number: B64D45/02 B64C1/12 B64C3/26 B64C3/34 B64D37/32

    Abstract: 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.

    Abstract translation: 根据一个实施方案,用于飞机的结构包括第一结构构件,联接到第一结构构件的第二结构构件,紧固件和导电物体。 紧固件将第一结构构件连接到第二结构构件。 紧固件插入形成在第一结构构件与第二结构构件重叠的部分中的插入孔中。 紧固件与插入孔中的第一和第二结构构件电接触不接触。 导电性物体嵌入到第一和第二结构构件的至少任一个内部。 导电物体通过形成将电流引导到第一和第二结构构件中的至少一个内部的电流通道,从而防止紧固件与第一和第二结构构件中的每一个之间的火花。

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