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 |