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    • 6. 发明公开
    • Installation assembly for bridging a cable harness or the like between two aircraft structure elements
    • 用于桥接线束或两架飞机结构元件之间等安装装置
    • EP2787586A1
    • 2014-10-08
    • EP13162545.1
    • 2013-04-05
    • Airbus Operations GmbH
    • Robrecht, VolkerRaguse, TillStoevesand, Daniel
    • H02G3/32
    • H02G3/00B60R16/02H02G3/32H02G3/36H02G3/38
    • The invention relates to an installation assembly for bridging a cable harness between two aircraft structure elements (1a, 1b) of an aircraft, die assembly comprising an elongated connecting rod (4) having two end sections (2a, 2b) for attaching the connecting rod (4) onto two adjacent aircraft structure elements (1a, 1b), at least one cable guidance element (5, 5') having at least one receiving section (6) for receiving a cable harness (7) and an attachment section (8) for circumferentially surrounding the connecting rod (4), wherein locking means are provided to form a connection between the attachment section (8) and the connecting rod (4), wherein a polygonal cross section of the connecting rod (4) corresponds to a recess (9) of the attachment section (8) in order to form a positive locking engagement between the cable guidance element (5) and the connecting rod (4).
    • 本发明在安装组件涉及桥接两个飞机结构元件之间的电缆束(1A,1B)的飞行器的,该组件包括细长的连杆(4),其具有两个端部(2A,2B)用于安装连杆 (4)到具有至少一个用于容纳电缆束(6),接收部的两个相邻的飞机结构元件(1A,1B),至少一个线缆引导元件(5,5“)(7)和(安装部8 )为沿周向围绕所述连接杆(4),worin锁定装置被提供,以形成连接部分(8)和连接杆(4)之间的连接,worin连杆的多边形的横截面(4)对应于一个 凹部(9),以便形成电缆导向元件(5)和所述连接杆之间的正锁定接合所述附接部(8)的(4)。