发明名称 GAS TURBINE ENGINE OIL BUFFERING
摘要 A turbine engine includes a shaft, a fan, at least one bearing mounted on the shaft and rotationally supporting the fan, a fan drive gear system coupled to drive the fan, a bearing compartment around the at least one bearing and a source of pressurized air in communication with a region outside of the bearing compartment.
申请公布号 US2013094937(A1) 申请公布日期 2013.04.18
申请号 US201113340871 申请日期 2011.12.30
申请人 GLAHN JORN A.;SCHWARZ FREDERICK M. 发明人 GLAHN JORN A.;SCHWARZ FREDERICK M.
分类号 F01D15/12 主分类号 F01D15/12
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