Patent · US Active

Device for laying a cable harness in an aircraft

US8590846B2 · kind B2 · utility

5Cited by
27References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 27, 2010
Grant dateNov 26, 2013
Priority date
Expiry dateMar 3, 2031

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB60R16/0222
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

Abstract

A device for bridging a cable harness between two aircraft structure elements of an aircraft includes an elongated connecting rod having a plurality of radial snap-in holes and configured to bridge a space between the two aircraft structure elements and affix to at least one of the two aircraft structure elements. The device also includes 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 resiliently held radially directed locking pin, wherein the locking pin corresponds to one of the plurality of the radial snap-in holes so as to form a clip connection and a positive locking engagement between the at least one attachment section and the connecting rod.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.