发明名称 |
Shielded electrical harness, in particular for an airplane engine |
摘要 |
<p>The harness has conductive elements with connectors/branches at its ends, where each element has an electrically conducting wire (20) mounted in a tubular structure (22) of protection and shield. The structure has a sheath (28) with ringed structure, surrounding a metallic tubular braid (26) of the shield. An end of the sheath is fixed to a cylindrical end fitting (30) of thermo-retractable material. The end fitting fixes the sheath on the connector, and locks and fixes an end of the braid on a cylindrical piece (32) of the connector by intermediate of a metallic band (36).</p> |
申请公布号 |
EP1858116(B1) |
申请公布日期 |
2009.10.28 |
申请号 |
EP20070290601 |
申请日期 |
2007.05.11 |
申请人 |
SNECMA |
发明人 |
DETERRE, GEOFFRAY;HENRIOUX, PASCAL;LORAND, ANTHONY;PELISSON, PASCAL |
分类号 |
H01R4/72;H01R13/646;H01R13/658 |
主分类号 |
H01R4/72 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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