| 发明名称 | Oil baffle for gas turbine fan drive gear system | ||
| 摘要 | An exemplary turbine engine assembly includes a first shaft that is rotatably driven by a second shaft of a gas turbine engine, a compressor hub driven by the second shaft, the compressor hub within a compressor section of the gas turbine engine, an epicyclic gear train that is driven by the first shaft, and a common attachment point that secures the first shaft and the compressor hub to the second shaft. | ||
| 申请公布号 | US8935853(B2) | 申请公布日期 | 2015.01.20 |
| 申请号 | US201314102769 | 申请日期 | 2013.12.11 |
| 申请人 | United Technologies Corporation | 发明人 | Sheridan William G.;McCune Michael E. |
| 分类号 | B21K25/00;F02C3/04;F01D25/18;F02C7/36;F16H57/04;F16H57/08 | 主分类号 | B21K25/00 |
| 代理机构 | Carlson, Gaskey & Olds, P.C. | 代理人 | Carlson, Gaskey & Olds, P.C. |
| 主权项 | 1. A turbine engine assembly comprising: a first shaft that is rotatably driven by a second shaft of a gas turbine engine; a compressor hub driven by the second shaft, the compressor hub within a compressor section of the gas turbine engine; an epicyclic gear train that is driven by the first shaft; and a common attachment point that secures the first shaft and the compressor hub to the second shaft. | ||
| 地址 | Hartford CT US | ||