| 发明名称 |
Flexible seal for gas turbine engine system |
| 摘要 |
A system includes a gas turbine engine, a nozzle structure located adjacent to the gas turbine engine, a flexible annular seal linking the gas turbine engine and the nozzle structure, the flexible annular seal having a plurality of corrugate sections, and a reinforcement member positioned between two of the plurality of corrugate sections. |
| 申请公布号 |
US8647048(B2) |
申请公布日期 |
2014.02.11 |
| 申请号 |
US201113173954 |
申请日期 |
2011.06.30 |
| 申请人 |
ROBERTS STEVEN D.;MONAHAN RICHARD W.;PIMENTA DAVID C.;UNITED TECHNOLOGIES CORPORATION |
发明人 |
ROBERTS STEVEN D.;MONAHAN RICHARD W.;PIMENTA DAVID C. |
| 分类号 |
F02C7/28;F01D11/00;F02K1/80 |
主分类号 |
F02C7/28 |
| 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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