| 发明名称 |
MODULATED TURBINE VANE COOLING |
| 摘要 |
A vane structure includes a baffle movably mounted within an aperture, the baffle movable to control a cooling flow between a first cooling cavity and a second cooling cavity. |
| 申请公布号 |
US2014271101(A1) |
申请公布日期 |
2014.09.18 |
| 申请号 |
US201213630681 |
申请日期 |
2012.09.28 |
| 申请人 |
Slavens Thomas N.;Pietraszkiewicz Edward F.;Martin Thomas J.;Zelesky Mark F.;Gautschi Steven B.;Devore Matthew A.;Staroselsky Alexander |
发明人 |
Slavens Thomas N.;Pietraszkiewicz Edward F.;Martin Thomas J.;Zelesky Mark F.;Gautschi Steven B.;Devore Matthew A.;Staroselsky Alexander |
| 分类号 |
F01D25/12 |
主分类号 |
F01D25/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A vane structure for a gas turbine engine comprising:
an airfoil section which defines an aperture, a first cooling cavity in communication with said aperture and a second cooling cavity in communication with said aperture; and a baffle movably mounted within said aperture, said baffle movable to control a cooling flow between said first cooling cavity and said second cooling cavity. |
| 地址 |
Vernon CT US |
