发明名称 Aeroengine starter/generator arrangement
摘要 An open-rotor gas turbine engine comprising a starter/generator, a first spool and a second spool, the second spool is of a lower pressure than the first spool; wherein the starter/generator is connected to the first and second spools via first and second clutches respectively. The method of operating the open-rotor engine comprises the step of supplying power to the starter/generator to drive the first spool via the first clutch to start the engine and, once the engine is self-propelling, a step of driving the starter/generator from the second spool via the second clutch to generate electricity.
申请公布号 US2010133832(A1) 申请公布日期 2010.06.03
申请号 US20090588810 申请日期 2009.10.28
申请人 ROLLS-ROYCE PLC 发明人 BUTT DAVID C.
分类号 H02P9/06;F02C6/04;F02C7/36;F02K3/00;F16D27/12;F16D41/08 主分类号 H02P9/06
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