Ge Aviation Systems Limited

David Graham Ettridge

Xiaochuan Jia

Keval Mehta

Thomas David Oliver Pocock

Systems and methods for controlling power distribution are provided. More particularly, in one embodiment, a method can include monitoring a first plurality of electrical characteristics for each power source of a plurality of power sources. The plurality of power sources can include a first generator, a second generator, an auxiliary power source, and an external power source. The method can include monitoring a second plurality of electrical characteristics for each bus of a plurality of buses. The plurality of buses can include a first electrical bus, a second electrical bus, and an electrical tie bus. The method can further include selectively controlling a power distribution of the plurality of power sources among the plurality of buses based, at least in part, on the first and second pluralities of electrical characteristics.

Multi-source power distribution system

A turbofan engine includes a turbine engine having a rotatable fan and a generator. The generator further includes a main machine, an exciter, and a generator control unit for controlling the excitation of the main machine. A rotor assembly is located within one of the blades, and a stator assembly that is along a rotational path of the rotor assembly whereby the operation of the turbine engine rotates the fan, which rotates the rotor assembly along its rotational path past the stator assembly to generate electricity.

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Bishops Cleeve, United Kingdom

David Graham Ettridge