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
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