| 发明名称 |
GAS TURBINE EXHAUST NOZZLE DIVERGENT FLAP SEAL |
| 摘要 |
A seal assembly for a nozzle in a gas turbine engine includes a connector having a first hinge portion for attaching to the nozzle, a flat portion for sealing against a wall of the engine; and a first hinge for attaching the connector to the flat portion wherein the connector is adapted to rotate relative to the nozzle and the flat portion is adapted to rotate relative to the connector.
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| 申请公布号 |
US2013033005(A1) |
申请公布日期 |
2013.02.07 |
| 申请号 |
US201113196074 |
申请日期 |
2011.08.02 |
| 申请人 |
TREAT CHRISTOPHER;STENMAN CHRISTINA A. |
发明人 |
TREAT CHRISTOPHER;STENMAN CHRISTINA A. |
| 分类号 |
F01D11/00;F16J15/02 |
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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