发明名称 Integrated wiring for composite structures
摘要 A wire for integration with an airplane composite structure material includes a conductive core surrounded by an isolation layer for substantially isolating the conductive core from the composite structure material. The isolation layer includes braided fibers, and the braided fibers include a material having at least substantially similar properties as the composite structure material.
申请公布号 US7414189(B2) 申请公布日期 2008.08.19
申请号 US20050163001 申请日期 2005.09.30
申请人 THE BOEING COMPANY 发明人 GRIESS KENNETH H.
分类号 H01B7/00 主分类号 H01B7/00
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