Abstract Systems and methods for distributing in an aircraft are provided. More particularly,
in one embodiment, a system can include one or more gas turbine engines configured to …

An aircraft hybrid electrical system includes an electric power generating system in signal
communication with a thermal combustion engine, a secondary power system in signal …

A system includes a first generator configured to output a first plurality of AC signals; a
second generator configured to output a second plurality of AC signals; a first set of rectifiers …

4, 233652 4,275,858 4, 287907 4, 299361 4.326, 189 4,330,827 4332032 4,335,745
4,340,791 4, 347901 4,351.394 4,372.212 4,413,322 4,472,780 4, 476395 4, 482018 4 …

Multiple position switches and specifically in-line multiple position switches where a user
has definitive points of on and off switching which are used to turn multiple redundant …

Abstract Systems and methods for dual voltage power generation are provided. Aspects
include a generator having an input connected to an engine to receive rotational energy …

Abstract Systems and methods for distributing in an aircraft are provided. More particularly,
in one embodiment, a system can include one or more gas turbine engines configured to …

An architecture for an aircraft comprises two air-condition ing systems, two converters, each
intended to supply one of the air-conditioning systems, and at least one first electric machine …