| 发明名称 |
Turbine Vane With Platform Rib |
| 摘要 |
A vane for use in a gas turbine engine has an airfoil extending between a leading edge and a trailing edge, a radially outer platform and a radially inner platform. A rib is on one of the radially inner and radially outer platforms, and is adjacent the trailing edge of the airfoil. A mid-turbine frame is also disclosed. |
| 申请公布号 |
US2016194969(A1) |
申请公布日期 |
2016.07.07 |
| 申请号 |
US201414917124 |
申请日期 |
2014.09.22 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
OLS John T.;ALLEN Richard N.;PORTER Steven D.;SANCHEZ Paul K. |
| 分类号 |
F01D9/04 |
主分类号 |
F01D9/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A vane for use in a gas turbine engine comprising:
an airfoil extending between a leading edge and a trailing edge; a radially outer platform and a radially inner platform; and a rib on one of said radially inner and radially outer platforms, and said rib being adjacent said trailing edge of said airfoil. |
| 地址 |
Hartford CT US |
