| 发明名称 |
INTER STAGE SEAL FOR GAS TURBINE ENGINE |
| 摘要 |
A turbine section (28) of a gas turbine engine (20) includes a seal (130) that extends between a vane platform (76, 78, 80, 82) and a Blade Outer Air Seal (64). |
| 申请公布号 |
EP2998520(A1) |
申请公布日期 |
2016.03.23 |
| 申请号 |
EP20150172147 |
申请日期 |
2015.06.15 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HALL, THEODORE W.;MCCAFFREY, MICHAEL G.;MOTT, ZACHARY |
| 分类号 |
F01D11/00 |
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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