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In order to conclude the second component to the first component which

机译:为了将第二部分归纳为第一部分

摘要

PROBLEM TO BE SOLVED: To provide a lightning-resistant fastener and a cap which improves workability and quality stability with lightening resistance assured and thereby enables a reduction in the manufacturing cost of an aircraft body, and to provide a method of mounting the lightning-resistant fastener.;SOLUTION: By forming a hole 32 in a cap 30 and by forming a screw groove 32a in the hole 32, the cap 30 is surely and easily positioned and mounted on a fastener member 24, and the cap 30 is surely prevented from falling even after the mounting. Moreover, locking portions 60 prevent the cap 30 from loosening from the fastener member 24. Assuring the lightning-resistant performance, this structure enables the improvement of the workability, the suppression of the manufacturing cost, and the mounting of the cap 30 with stable quality without relying on a worker. It is desirable to form the cap 30 of a resin for mass-production and reduction in weight etc.;COPYRIGHT: (C)2012,JPO&INPIT
机译:解决的问题:提供一种防雷的紧固件和帽盖,其在确保了防雷的同时提高可加工性和质量稳定性,从而能够降低飞机的制造成本,并提供一种安装该防雷的方法解决方案:通过在盖30上形成孔32并在孔32上形成螺纹槽32a,盖30被可靠且容易地定位并安装在紧固件构件24上,并且可靠地防止了盖30的松动。即使安装后也会掉落。此外,锁定部分60防止帽30从紧固件构件24上松开。确保耐雷击性能,该结构使得能够以稳定的质量改善可加工性,抑制制造成本以及帽30的安装。不用依靠工人理想的是形成用于大量生产和减轻重量等的树脂盖30。版权所有:(C)2012,JPO&INPIT

著录项

  • 公开/公告号JP5535843B2

    专利类型

  • 公开/公告日2014-07-02

    原文格式PDF

  • 申请/专利权人 三菱航空機株式会社;

    申请/专利号JP20100205341

  • 发明设计人 西村 渉;

    申请日2010-09-14

  • 分类号B64C1/00;F16B37/14;

  • 国家 JP

  • 入库时间 2022-08-21 16:14:09

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