| 发明名称 |
Turbine blade damper and seal |
| 摘要 |
An integral damper and seal 46 for a turbine blade in a gas turbine engine includes a damper portion 54 which contacts the platform and at least one sealing portion 56, angled radially inward from the damper portion, which makes contact with and seals against the platform. <IMAGE> |
| 申请公布号 |
EP0851097(A2) |
申请公布日期 |
1998.07.01 |
| 申请号 |
EP19970310512 |
申请日期 |
1997.12.23 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HOUSTON, DAVID P.;GONSOR, MICHAEL;PELLAND, NATALI A.;AIREY, DAVID |
| 分类号 |
F01D5/26;F01D5/30;F01D11/00 |
主分类号 |
F01D5/26 |
| 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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