发明名称 TURBOPROP/FAN TYPE JET ENGINE WITH CLUTCH
摘要 PROBLEM TO BE SOLVED: To maximize performance improvement by combining a jet engine and an electric motor with a gas turbine of the jet engine as a uniaxial gas turbine.SOLUTION: A turboprop or turbofan type jet engine having a gas turbine and a propeller or fan to be rotated by the gas turbine includes a clutch selectively decoupling an axis of rotation of the gas turbine from the propeller or fan and an electric motor acting on the axis of rotation of the gas turbine in the gas turbine side rather than the clutch.
申请公布号 JP2013194636(A) 申请公布日期 2013.09.30
申请号 JP20120063667 申请日期 2012.03.21
申请人 TOYOTA MOTOR CORP 发明人 IWASE SATORU
分类号 F02C7/36;B64C11/00;F01D15/10;F01D15/12;F02C3/107;F02C7/00;F02K3/06 主分类号 F02C7/36
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