发明授权
US09458729B2 Electric power supply for apparatuses supported by the rotor of an aircraft engine 有权
用于由飞机发动机的转子支撑的装置的电力供应

Electric power supply for apparatuses supported by the rotor of an aircraft engine
摘要:
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.
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