发明名称 |
GAS TURBINE ENGINE RAPID RESPONSE CLEARANCE CONTROL SYSTEM |
摘要 |
An active clearance control system of a gas turbine engine includes a multiple of blade outer air seal assemblies and a sync ring with a multiple of graduation sets. Each of the graduation sets is associated with one of the multiple of blade outer air seal assemblies. An active clearance control system of a gas turbine engine includes a sync ring with a multiple of graduation sets. Each of the graduation sets includes a multiple of graduations to define an associated radial position for each of a respective multiple of blade outer air seal assemblies. |
申请公布号 |
EP3049638(A4) |
申请公布日期 |
2016.10.26 |
申请号 |
EP20140860381 |
申请日期 |
2014.07.23 |
申请人 |
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发明人 |
DAVIS, TIMOTHY M.;DUGUAY, BRIAN |
分类号 |
F01D11/22;F01D11/08;F01D11/14;F02C7/28 |
主分类号 |
F01D11/22 |
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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