发明名称 キャップ、これを用いた締結構造およびこの締結構造を有する航空機
摘要 <p>There is provided a cap capable of achieving enhanced safety by inhibiting the occurrence of sparks thereinside even if a lightning current has flowed through a fastener, a fastening structure using the same, and an aircraft including the fastening structure. A cap (27) according to the present invention is attached so as to cover a portion of a fastener (15) that couples an upper skin (3) of an aircraft and a stringer (11) located inside the upper skin (3), the portion projecting through the stringer (11), wherein an outer surface (33) of the cap that comes into contact with an interior space of the upper skin (3) is a curved surface, and the cap is made of a conductive material.</p>
申请公布号 JP5619446(B2) 申请公布日期 2014.11.05
申请号 JP20100066927 申请日期 2010.03.23
申请人 发明人
分类号 B64C1/00;B64D45/02;F16B37/14 主分类号 B64C1/00
代理机构 代理人
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