发明名称 Installation system for binding electrical cables at rearward building structure of coating surface of airplane, has tubular lattice structure for receiving electrical cables, where lattice structure is made of shrinkable tube
摘要 <p>The system (8) has a tubular lattice structure for receiving electrical cables (18, 20, 22, 24), where the lattice structure is made of a tube such as shrinkable tube. The lattice structure is provided with net-like elastic sections and has different cross-sections at different regions. Fastening elements clamp the electrical cables on the lattice structure, where the fastening elements are connected on bars and form a net structure. Tension elements pass through the lattice structure for installing the electrical cables and are provided with a clamping element for fixing the cables. An independent claim is also included for a method for binding electrical cables at a rearward building structure of a coating surface of an aircraft.</p>
申请公布号 DE102009060697(A1) 申请公布日期 2011.06.30
申请号 DE20091060697 申请日期 2009.12.29
申请人 AIRBUS OPERATIONS GMBH 发明人 GOEHLICH, ROBERT ALEXANDER, DR.;SAYILGAN, CIHANGIR
分类号 H02G3/34 主分类号 H02G3/34
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