发明名称 ATTACHMENT AVOIDANCE FASTENER
摘要 PROBLEM TO BE SOLVED: To provide an attachment avoidance fastener, surely preventing peel-off of an insulating cap while the airplane is flying to improve the lightening attachment preventing effect to the fastener and the reliability. SOLUTION: This attachment avoidance fastener 1 joints a shell plate 10 of the airplane and a structural member 11 positioned on the inner side of the shell plate 10. An insulator layer 5 is fused to cover one end face of a head 3, and is made to mesh mechanically with an engaging portion 7 formed on the one end face. The peripheral edge part of the engaging portion 7 is rounded along the circumferential direction. COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2011102122(A) 申请公布日期 2011.05.26
申请号 JP20110029237 申请日期 2011.02.14
申请人 MITSUBISHI HEAVY IND LTD 发明人 KASHIWAGI MASAHIRO;KAMINO YUICHIRO;OGURI KAZUYUKI;TARUMI TAKEYASU;BESSHO MASAHIRO;YAMAKOSHI HIDEO;ISHIKAWA NAOMOTO
分类号 B64C1/00;B64D45/02;F16B33/06;F16B41/00 主分类号 B64C1/00
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