Generator for gas turbine engine having main dc bus...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 41/00 (2006.01) F02C 7/32 (2006.01) H02J 3/02 (2006.01) H02K 7/18 (2006.01) H02M 7/02 (2006.01)

Patent

CA 2638961

An aircraft electrical system includes a generator that supplies electrical AC power to a plurality of accessories associated with a gas turbine engine. The generator also supplies power to an aircraft DC bus in parallel to the supply to the accessory bus.

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