Patent ID: 9203220
Filing Date: 2015-12-01
Classification: B60R,H02G

Abstract:
1. An installation assembly for bridging a cable harness between two aircraft structure elements of an aircraft, the installation assembly comprising: an elongated connecting rod having two end sections for attaching the connecting rod onto two adjacent aircraft structure elements; and at least one cable guidance element having at least one receiving section for receiving a cable harness and an attachment section for circumferentially surrounding the connecting rod, wherein locking means are provided to form a connection between the attachment section and the connecting rod, wherein a polygonal cross section of the connecting rod corresponds to a recess of the attachment section in order to form a positive locking engagement between the at least one cable guidance element and the connecting rod, and wherein the U-shaped recess corresponds to a clip element snapped in the opening of the U-shaped recess in order to form a clip connection.