发明名称 GAS TURBINE ENGINE FORWARD BEARING COMPARTMENT ARCHITECTURE
摘要 A gas turbine engine includes a bearing structure mounted to the front center body case structure to rotationally support a shaft driven by a geared architecture. A bearing compartment passage structure is in communication with the bearing structure through a front center body case structure.
申请公布号 EP2802747(A1) 申请公布日期 2014.11.19
申请号 EP20120865495 申请日期 2012.12.27
申请人 UNITED TECHNOLOGIES CORPORATION;MUNSELL, PETER M.;STRIPINIS, PHILIP S. 发明人 MUNSELL, PETER M.;STRIPINIS, PHILIP S.
分类号 F01D25/16;F02C7/06;F02C7/12;F02C7/28;F02C7/36;F02K3/06 主分类号 F01D25/16
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