发明名称 Aircraft nut and bolt assembly system - detects alteration in distance between datum points on nut when tightening
摘要 <p>The nut and bolt assembly system is for use with a load-indicating nut ensuring that the bolt has been pulled down to the correct degree. A tightening torque is applied to the nut simultaneously with a detector for the alteration in distance between two datum points on the nut body. Torque continues to be exerted until the detector has reacted to an alteration of a predetermined value in the distance concerned, and which in turn can be arranged to initiate a visual or audible signal. Where a power-operated spanner is used, the signal can cut off the power to it.</p>
申请公布号 FR2388643(A1) 申请公布日期 1978.11.24
申请号 FR19770012766 申请日期 1977.04.27
申请人 GKN FASTENERS LTD 发明人
分类号 B25B23/147;(IPC1-7):25B21/00 主分类号 B25B23/147
代理机构 代理人
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