发明名称 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.
申请公布号 US2010108806(A1) 申请公布日期 2010.05.06
申请号 US20090590045 申请日期 2009.10.30
申请人 SEARETE LLC, A LIMITED LIABILITY CORPORATION OF THE STATE OF DELAWARE 发明人 CHAN ALISTAIR K.;HYDE RODERICK A.;ISHIKAWA MURIEL Y.;JUNG EDWARD K.Y.;KARE JORDIN T.;MYHRVOLD NATHAN P.;TEGREENE CLARENCE T.;WEAVER THOMAS A.;WOOD, JR. LOWELL L.;WOOD VICTORIA Y.H.
分类号 B64D31/00 主分类号 B64D31/00
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