| 发明名称 |
GAS TURBINE ENGINE VANE-TO-TRANSITION DUCT SEAL |
| 摘要 |
A vane seal assembly for a gas turbine engine comprises of a case including a first connector. A notch in the case adjoins the groove. A vane having a second connector mates with the first connector. A seal assembly is provided between the vane and the case to provide a sealed cavity adjoining the notch. |
| 申请公布号 |
US2014366556(A1) |
申请公布日期 |
2014.12.18 |
| 申请号 |
US201414296657 |
申请日期 |
2014.06.05 |
| 申请人 |
United Technologies Corporation |
发明人 |
Banks Anton G.;Hazzard Robert L. |
| 分类号 |
F01D11/00 |
主分类号 |
F01D11/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A vane seal assembly for a gas turbine engine comprising:
a case including a first connector, and a notch in the case that adjoins the groove; a vane having a second connector mating with the first connector; a seal assembly provided between the vane and the case to provide a sealed cavity adjoining the notch. |
| 地址 |
Hartford CT US |
