首页> 外国专利> 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

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

机译:用于在飞机的涂装面的向后建筑结构上束缚电缆的安装系统,具有用于容纳电缆的管状格状结构,其中格状结构由可收缩管制成

摘要

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.
机译:系统(8)具有用于接收电缆(18、20、22、24)的管状格子结构,其中格子结构由诸如可收缩管的管制成。格子结构具有网状弹性部​​分,并且在不同区域具有不同的横截面。紧固元件将电缆夹紧在格子结构上,其中紧固元件在杆上连接并形成网状结构。张力元件穿过用于安装电缆的格子结构,并设有用于固定电缆的夹紧元件。还包括一种用于在飞机的涂覆表面的向后的建筑结构处束缚电缆的方法的独立权利要求。

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