A system and method to converting mechanical rotational energy of an aircraft input shaft of a transmission to electrical energy. The system includes an alternator having an inductor carried by the aircraft transmission and a magnet carried by the aircraft input shaft. The input shaft rotates the magnet in relation to the inductor, which in turn converts the mechanical rotational energy to electrical energy.
BRUSHLESS ALTERNATOR FOR HELICOPTER TRANSMISSION INSTALL
ALTERNATEUR SANS BALAI POUR TRANSMISSION D'HELICOPTERE
2016-03-22
Patent
Electronic Resource
English
SAE Technical Papers | 1998
|British Library Conference Proceedings | 1998
|AN EXCITED FIELD BRUSHLESS FLYWHEEL ALTERNATOR FOR OUTBOARD ENGINES
SAE Technical Papers | 1961
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