Airbus Operations Gmbh

Paul O'Shaughnessy

Anthony John Bryant

James Bird

Scott Palmer

Javier Ruiz-De-Pablo

Christopher Bills

An aircraft system has a first structure, and a second structure coupled to the first structure and movable between first and second positions relative to the first structure. The aircraft system has an electrical connector for providing an electrical connection running between respective components housed within the first and second structures. The electrical connector has a cable harness housed within the first structure, and a connector body coupled to an end of the cable harness. The connector body extends through an aperture formed in the first structure, and the connector body is coupled to the second structure such that movement of the second structure between the first and second positions relative to the first structure causes the connector body to move through the aperture.

Aircraft systems and electrical connectors

A cable routing system is disclosed including a routing fixture and an exit fitting. The routing fixture defines a channel for a cable. The channel is engaged by the exit fitting and a cable in the channels exits through an exit channel defined by the exit fitting. The exit channel is directed away from the channel in the routing fixture. The resulting assembly allows low profile cable runs that can conform to a structural surface and in which cables can be broken out easily, without a requirement to cut the cable. A clamp may be provided to further secure the exit fitting to the routing fixture. A method of installation involves installing a cable into a routing channel before installing the exit fitting. The cable routing system can be used in an aircraft, including space constrained areas such as within an aircraft wing.

Aircraft cable routing system and method of installation thereof

A cable routing system is disclosed having dielectric, or insulating, liner which is installed within a cable routing channel, or raceway, to subdivide the channel into at least two secondary channels. This can achieve more efficient use of space and enable more flexible placement of cables within the channels while meeting safety requirements. Installation of cables into the channel can include inserting the cables into the dielectric liner before the installation of the dielectric liner into the cable routing channel. The cable routing system can be used in an aircraft, including within space-constrained areas of the aircraft such as inside a wing.

Growing community of inventors

Bristol, United Kingdom

Paul O'Shaughnessy