发明申请
US20100108806A1 Hybrid propulsive engine including at least one independently rotatable propeller/fan 审中-公开
混合推进发动机包括至少一个独立旋转的螺旋桨/风扇

Hybrid propulsive engine including at least one independently rotatable propeller/fan
摘要:
One aspect relates to a method of reducing noise for an aircraft. The method includes determining a mode of operation of the aircraft or the engine. The method also includes controlling a hybrid jet engine, based on the mode of operation, to at least partially use electrically generated torque to generate thrust.
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