An aircraft engine including: a stator; a main shaft; a first rotor; a second rotor; a transmission mechanism; a first electrical apparatus supported by the first rotor and a second electrical apparatus supported by the second rotor; at least one first field winding supported by the stator; a control unit configured to circulate direct electric current in the first field winding; at least one first armature winding supported by the first rotor and connected to the first electrical apparatus and at least one second armature winding supported by the second rotor and connected to the second electrical apparatus.
ALIMENTATION ELECTRIQUE DES EQUIPEMENTS PORTES PAR LE ROTOR D'UN MOTEUR D'AERONEF
ELECTRIC POWER FEED FOR THE SYSTEMS CARRIED BY TURBOSHAFT ROTOR
STROMVERSORGUNG FÜR DIE VOM TRIEBWERKSROTOR GETRAGENEN GERÄTE
2016-04-06
Patent
Electronic Resource
French
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