| 发明名称 |
GAS TURBINE ENGINE BLADE OUTER AIR SEAL THERMAL CONTROL SYSTEM |
| 摘要 |
A clearance control system for a gas turbine engine is provided. The system includes an inner axial wall that extends between a forward wall and an aft wall. The system also includes an outer axial wall that extends parallel to the inner axial wall to pivotally receive a full hoop thermal control ring. |
| 申请公布号 |
EP3055514(A4) |
申请公布日期 |
2016.11.02 |
| 申请号 |
EP20140859618 |
申请日期 |
2014.08.05 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BLANEY, KEN F.;LUTJEN, PAUL M. |
| 分类号 |
F01D11/16;F01D11/08;F01D11/18;F01D25/28;F02C7/20;F16J15/44 |
主分类号 |
F01D11/16 |
| 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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