Electromechanical flight control system and method for rotocraft

Flight control systems and methods for rotorcraft are provided. The flight control system includes a user input device and a motor in operable communication with the user input device. The motor includes a plurality of winding sets and an armature coupled to the plurality of winding sets. The armatu...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HANLON, CASEY, KERN, JAMES I
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS DYNAMO-ELECTRIC MACHINES ELECTRICITY GENERATION HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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