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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

机译:飞机发动机的电导线连接装置,在管状主体和圆柱套筒之间装有导电滑环,以确保主体和套筒之间的电连续性

摘要

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.
机译:装置(116)具有管状体(136),管状体(136)包围导体(118)的端部并带有旋紧在连接器上的旋转螺母(130)。主体的一端连接到围绕导体的金属电磁屏蔽编织物(122)的一端。主体被圆柱形套筒(138)围绕,该圆柱形套筒相对于主体绕主体的纵向轴线自由旋转地安装,并且编织物固定在该套筒上。导电滑环(140)安装在主体和套筒之间,以确保主体和套筒之间的电连续性。

著录项

  • 公开/公告号FR2950201A1

    专利类型

  • 公开/公告日2011-03-18

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号FR20090004340

  • 发明设计人 DETERRE GEOFFRAY;

    申请日2009-09-11

  • 分类号H01R39/02;H02G3/02;

  • 国家 FR

  • 入库时间 2022-08-21 17:45:48

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