| 发明名称 |
COMBUSTOR SEAL SYSTEM FOR A GAS TURBINE ENGINE |
| 摘要 |
A system for providing a seal between a combustor and a turbine vane. The system includes a flange configured to extend radially from the combustor, and a seal. The flange includes a flange surface configured to face in an axial direction toward a surface of the vane. The seal is configured to be axially loaded between the flange surface and the surface of the vane. |
| 申请公布号 |
US2015226131(A1) |
申请公布日期 |
2015.08.13 |
| 申请号 |
US201314430334 |
申请日期 |
2013.09.30 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Low Kevin Joseph;Wong Joey |
| 分类号 |
F02C7/28;F02C3/107 |
主分类号 |
F02C7/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for providing a seal between a combustor and a turbine vane, the system comprising:
a flange configured to extend radially from the combustor, the flange including a flange surface configured to face in an axial direction toward a surface of the vane; and a seal configured to be axially loaded between the flange surface and the surface of the vane. |
| 地址 |
Hartford CT US |
