首页> 外国专利> articulation for an aircraft power distribution system unit and an aircraft power distribution system unit

articulation for an aircraft power distribution system unit and an aircraft power distribution system unit

机译:用于飞机配电系统单元的铰接和飞机配电系统单元

摘要

A hinge for an aircraft power distribution system unit is provided. The unit has a housing comprising a first housing part and a second housing part. The hinge comprises a first hinge member for connection to the first housing part of the unit; and a second hinge member for connection to the second housing part of the unit, wherein the first and the second hinge members comprise an electrically conductive material and wherein the first and the second hinge members are connectable to one another to establish an electrical connection between the first and the second hinge members and to allow relative rotation between the first and the second hinge members.
机译:提供了一种用于飞机配电系统单元的铰链。该单元具有壳体,该壳体包括第一壳体部分和第二壳体部分。铰链包括:第一铰链构件,用于连接到单元的第一壳体部分;以及第一铰链构件。第二铰链部件,其用于连接到单元的第二壳体部分,其中第一铰链部件和第二铰链部件包括导电材料,并且第一铰链部件和第二铰链部件可彼此连接以在外壳之间建立电连接。第一和第二铰链构件并允许第一和第二铰链构件之间的相对旋转。

著录项

  • 公开/公告号BR112012003082A2

    专利类型

  • 公开/公告日2016-08-16

    原文格式PDF

  • 申请/专利权人 GE AVIATION SYSTEMS LIMITED;

    申请/专利号BR20121103082

  • 发明设计人 ANDREW WORLEY;

    申请日2010-08-06

  • 分类号H01R13/04;H01R13/11;H01R25/14;H01R35/04;H02G3/18;H05K7/14;

  • 国家 BR

  • 入库时间 2022-08-21 14:27:31

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