Patent ID: 7505665
Filing Date: 2009-03-17
Classification: B64C,B64D,H02G

Abstract:
1. A cable holder for an aircraft, comprising: a base element; and a cable holder module; wherein the base element has a mount for mounting to a structure of the aircraft; wherein the cable holder module is designed for receiving at least one cable; wherein the base element and the cable holder module are separably connected to one another so as to inhibit any relative movement between one another; wherein the mount comprises at least one first pin that is designed for insertion into a first recess in a surface of the aircraft structure; wherein the at least one first pin is provided with a corrugation; wherein said cable holder module has at least one snap-in tab for an engagement with said base element, in such a way that said cable holder module is held on said base element when said at least one snap-in tab is engaged with said base element; wherein said cable holder module is provided a longitudinally located groove, and a longitudinally located protrusion in the middle of the groove for holding each cable; at least a first pin, a second pin are provided on the mount; wherein the length of said first pin and the thickness of said base element are the same, and the length of said second pin is longer than the thickness of said base element; said second pin is provided with a corrugation for insertion into a first recess in a surface of the aircraft structure; and at least two slot-like cable tie openings for each corresponding cable holders on the top surface of said base element.