| 发明名称 |
SEAL ASSEMBLY IN A GAS TURBINE ENGINE |
| 摘要 |
A gas turbine engine seal assembly (160) including: a rigid seal (58) cooperatively configured with a structure (14, 42) of a gas turbine engine to define a leakage path (102, 130) including a flow-controlling section (106, 134); and a compliant seal (162, 164) positioned in the leakage path. |
| 申请公布号 |
US2016273374(A1) |
申请公布日期 |
2016.09.22 |
| 申请号 |
US201514660969 |
申请日期 |
2015.03.18 |
| 申请人 |
Siemens Energy, Inc. |
发明人 |
Mitchell David J. |
| 分类号 |
F01D11/00;F01D9/02;F01D9/04 |
主分类号 |
F01D11/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine seal assembly comprising:
a rigid seal cooperatively configured with a structure of a gas turbine engine to define a leakage path there between comprising a flow-controlling section; and a compliant seal positioned in the leakage path. |
| 地址 |
Orlando FL US |
