作者: Stephen J. Bradbrook
DOI:
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摘要: A system and method for variable drive of a propeller or fan gas turbine engine. The engine has combustor arranged to be driven by combustion product from the combustor. comprises primary shaft transmission torque said propeller; an electric generator turbine; motor output generator. clutch is mounted between rotor operable mechanically disconnect so that can any combination and/or motor. invention may applied turboprop turbofan having gearing particularly suited unmanned aerial vehicle proulsion.