| 发明名称 |
Gas turbine engine ring seal |
| 摘要 |
<p>A seal assembly for a gas turbine engine (10) includes an engine static structure (30). First and second members fluidly separate cavities (52, 54, 56, 58) from one another. A seal assembly (46, 48) is captured by the engine structure (30). The seal assembly (46, 48) includes a carrier (70) and a seal (82) that engages the first member (88). The second member is captured by the carrier (70).</p> |
| 申请公布号 |
EP2905428(A3) |
申请公布日期 |
2015.09.02 |
| 申请号 |
EP20150154384 |
申请日期 |
2015.02.09 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
THILL, CARSON A. ROY;BROOMER, MARK;DAVIS, TIMOTHY M.;MCGARRAH, CRAIG R.;ROGERS, MARK J.;KEENE, RUSSELL E.;SWIFT, ANTHONY B. |
| 分类号 |
F01D11/00;F01D11/04;F01D25/24;F02C3/10;F02C7/28;F16J15/08 |
主分类号 |
F01D11/00 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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