An aircraft electrical supply circuit including: a power distribution network, onboard the aircraft, for electrical devices located in an engine of the aircraft or near the engine; and a power supply generator built into the engine of the aircraft to supply AC voltage power to a deicing or anti-icing system. The power supply generator is connected to a thrust reverser electromechanical actuator by a rectifier for supplying DC voltage power to the actuator.
Power supply circuit for an aircraft de-icing system
2016-01-12
Patent
Elektronische Ressource
Englisch
NTIS | 1978
NTRS | 1978
|British Library Conference Proceedings | 1994
|NTIS | 1971