Ge Aviation Systems Limited

John Michael Brett

Adrian John Hughes

Christopher Andrew Leivers

John Oliver Collins

Lewis Hughes

An avionics power management panel and door assembly where the panel includes a cabinet including a set of walls at least partially defining an interior with an open face and door assembly includes a central panel a front panel that includes a set of rows with apertures formed between two adjacent rows and where the set of rows have a crimped profile.

Avionics power management panel and door assembly

An avionics power management panel and power panel controller assembly where the panel includes a cabinet including a set of walls at least partially defining an interior with a printed circuit board. The power panel controller assembly can be provided in the interior and can include a chassis housing one or more power panel control modules adapted to couple to the printed circuit board via one or more complementary PCB connectors.

Power management panel and controller assembly

An apparatus and method managing a circuit breaker in a power distribution system unit. The power distribution system unit can include a housing with an internal bus structure, a door assembly which includes at least one plug received in a socket. A snubber plate is positioned at the socket and includes an aperture through which the plug can be received.

Power distribution system with snubber plate

An apparatus for distributing power from a power source to a set of power outputs using a power distribution rack includes a manifold having a set of bus bar channels in a wall, a set of electronic cards, and a set of bus bars received in the set of bus bar channels and coupling a power source to the electronic cards, wherein the electronic cards route the power from the power source to the power outputs.

Power distribution rack assembly

One aspect of the present invention provides a housing for housing electrical equipment in an aircraft. The housing comprises one or more panels defining an enclosed space for housing electrical equipment in an aircraft. The housing also comprises at least one electrical busbar for providing electric power to the electrical equipment, wherein the at least one electrical busbar is configured to provide structural support for the housing.

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Tewkesbury, United Kingdom

John Michael Brett