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 US9410483(B2) 申请公布日期 2016.08.09
申请号 US201514640251 申请日期 2015.03.06
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Munsell Peter M.;Stripinis Philip S.
分类号 F02C7/06;F02C7/12;F02C7/28;F01D25/16;F02K3/06;F02C7/36 主分类号 F02C7/06
代理机构 Carlson, Gaskey & Olds P.C. 代理人 Carlson, Gaskey & Olds P.C.
主权项 1. A gas turbine engine comprising: a front center body case structure; a geared architecture at least partially supported by said front center body case structure; a bearing structure mounted to said front center body case structure to rotationally support a shaft driven by said geared architecture; a bearing compartment passage structure in communication with said bearing structure through said front center body case structure, wherein said bearing compartment passage structure includes a hollow front center body strut; and a conditioning device in fluid communication with said bearing compartment passage structure.
地址 Hartford CT US