发明名称 Electrical lead conductors connecting device for airplane engine, has electrical conductive slip ring mounted between tubular body and cylindrical sleeve to ensure electrical continuity between body and sleeve
摘要 <p>The device (116) has a tubular body (136) enclosing ends of conductors (118) and carrying a rotating nut (130) screwed on a connector. An end of the body is connected to an end of a metallic electromagnetic shielding braid (122) surrounding the conductors. The body is surrounded by a cylindrical sleeve (138) mounted freely in rotation relative to the body around a longitudinal axis of the body, and the braid is fixed on the sleeve. An electrical conductive slip ring (140) is mounted between the body and the sleeve to ensure electrical continuity between the body and the sleeve.</p>
申请公布号 FR2950201(A1) 申请公布日期 2011.03.18
申请号 FR20090004340 申请日期 2009.09.11
申请人 SNECMA 发明人 DETERRE GEOFFRAY
分类号 H01R39/02;H02G3/02 主分类号 H01R39/02
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