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Electrical lead for engine of airplane, has tubular protection structure comprising telescopic part whose length is adjustable between predetermined values, where length of electric conductor is equal to large length of structure

机译:飞机发动机的电线具有管状保护结构,该结构包括伸缩部分,伸缩部分的长度在预定值之间可调,其中电导体的长度等于较大的结构长度

摘要

The lead (10) has an electric conductor (12) surrounded by a tubular protection structure (14), where the protection structure has an telescopic part (16) whose length is adjustable between predetermined values. Length of the conductor is equal to large length of the structure. The conductor is totally housed in the structure or partially housed in a conductor storing case (34). The telescopic part has coaxial cylindrical bodies (24, 26) surrounding the conductor and fixed to the protection structure by gluing.
机译:引线(10)具有被管状保护结构(14)围绕的电导体(12),其中保护结构具有伸缩部分(16),其长度可在预定值之间调节。导体的长度等于结构的大长度。导体完全被容纳在结构中或部分地被容纳在导体存储盒(34)中。伸缩部分具有同轴圆柱体(24、26),其围绕导体并通过胶粘固定在保护结构上。

著录项

  • 公开/公告号FR2950749A1

    专利类型

  • 公开/公告日2011-04-01

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号FR20090004599

  • 发明设计人 DETERRE GEOFFRAY;

    申请日2009-09-25

  • 分类号H02G3/06;B64D33;

  • 国家 FR

  • 入库时间 2022-08-21 17:45:50

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