发明名称 |
CAP, FASTENING STRUCTURE USING THE SAME, AND AIRCRAFT HAVING THIS FASTENING STRUCTURE |
摘要 |
PROBLEM TO BE SOLVED: To provide a cap capable of improving safety by suppressing the occurrence of sparks therein even when any lightening shock current runs through a fastener, and to provide a fastening structure using the same, and an aircraft having the fastening structure.SOLUTION: The cap 27 is mounted to cover a piercing part of a stringer 11 in a fastener 15 for coupling the upper outer sheet 3 of an aircraft with the stringer 11 located inside the upper outer sheet 3. An outer surface 33 in contact with the internal space of the upper outer sheet 3 is constituted of a curved surface, and formed of a conductive material. |
申请公布号 |
JP2011195114(A) |
申请公布日期 |
2011.10.06 |
申请号 |
JP20100066927 |
申请日期 |
2010.03.23 |
申请人 |
MITSUBISHI HEAVY IND LTD;YAMAMOTO KAZUO |
发明人 |
KAMIHARA NOBUYUKI;MURAKAMI KOICHI;YAMAMOTO KAZUO |
分类号 |
B64C1/00;F16B37/14 |
主分类号 |
B64C1/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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