| 发明名称 |
GAS TURBINE ENGINE RING SEAL |
| 摘要 |
A seal assembly for a gas turbine engine includes an engine static structure. First and second members fluidly separate cavities from one another. A seal assembly is captured by the engine structure. The seal assembly includes a carrier and a seal that engages the first member. The second member is captured by the carrier. |
| 申请公布号 |
US2015226132(A1) |
申请公布日期 |
2015.08.13 |
| 申请号 |
US201514611920 |
申请日期 |
2015.02.02 |
| 申请人 |
United Technologies Corporation |
发明人 |
Roy Thill Carson A.;Broomer Mark;Davis Timothy M.;McGarrah Craig R.;Rogers Mark J.;Keene Russell E.;Swift Anthony B. |
| 分类号 |
F02C7/28;F01D25/24;F02C3/04 |
主分类号 |
F02C7/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A seal assembly for a gas turbine engine comprising:
engine static structure; first and second members fluidly separate cavities from one another; and a seal assembly captured by the engine structure, the seal assembly includes a carrier and a seal that engages the first member, and the second member captured by the carrier. |
| 地址 |
Hartford CT US |
