Patent ID: 8590846
Filing Date: 2013-11-26
Classification: B60R,H02G

Abstract:
1. A device for bridging a cable harness between two aircraft structure elements of an aircraft, the device comprising: an elongated connecting rod having a plurality of radial snap-in holes disposed in an outer circumferential wall of the connecting rod and configured to at least partially bridge a space between the two aircraft structure elements and to affix to at least one of the two aircraft structure elements; and a cable guiding element having at least one receiving section for receiving the cable harness and at least one attachment section circumferentially surrounding the connecting rod, the attachment section having a locking pin disposed radially relative to the connecting rod in a resilient manner so as to snap into and form a positive locking engagement with a corresponding one of the plurality of radial snap-in holes via axial insertion of the connecting rod into the at least one attachment section, wherein each of the plurality of snap-in holes is a radial through-hole at an end region of the rod.