发明名称 AUXILIARY OIL PUMP FOR GAS TURBINE ENGINE GEAR REDUCTION
摘要 A gas turbine engine has a turbine driving a gear reduction. The gear reduction drives a fan drive shaft assembly to, in turn, drive a fan rotor at a reduced speed relative to the turbine. A generator generates current upon rotation of the fan drive assembly. The generator supplies electric current to an electric motor driven pump. The electric motor driven pump delivers lubricant to components within the gear reduction.
申请公布号 WO2015065720(A1) 申请公布日期 2015.05.07
申请号 WO2014US60824 申请日期 2014.10.16
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CIGAL, BRIAN P.;VALVA, CHRISTOPHER M.
分类号 F02C7/06;F01D25/20;F16H57/04 主分类号 F02C7/06
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