FIELD: electricity.
SUBSTANCE: aircraft power supply circuit includes on-board power distribution network (17) for electric devices (5b) located in or near the aircraft engine, and power supply generator (27) integrated in the aircraft engine to supply AC power to deicing system (5a). Power supply generator is connected to electromechanical drive of thrust reverser (5c) via rectifier to supply DC power to the mentioned drive.
EFFECT: reduced technical requirements to rectifier.
7 cl, 1 dwg
Authors
Dates
2014-07-20—Published
2011-06-06—Filed