| 发明名称 |
GAS TURBINE ENGINE STATOR VANE PLATFORM COOLING |
| 摘要 |
An airfoil component for a gas turbine engine includes a platform joined to an airfoil. The platform includes a flow path surface that extends between spaced apart lateral surfaces. The airfoil extends from the flow path surface. A contoured surface adjoins the flow path surface and one of the lateral surfaces. |
| 申请公布号 |
US2016003074(A1) |
申请公布日期 |
2016.01.07 |
| 申请号 |
US201414769208 |
申请日期 |
2014.03.10 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Chlus Wieslaw A.;Thomen Seth J. |
| 分类号 |
F01D9/04;F01D9/02 |
主分类号 |
F01D9/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An airfoil component for a gas turbine engine comprising:
a platform joined to an airfoil, the platform includes a flow path surface extending between spaced apart lateral surfaces, the airfoil extends from the flow path surface, and a contoured surface adjoins the flow path surface and one of the lateral surfaces. |
| 地址 |
Hartford CT US |
