发明名称 CLEARANCE CONTROL ASSEMBLY
摘要 A clearance control assembly for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a clearance control ring to position a blade outer air seal assembly radially relative to a blade tip. The clearance control ring is compression fit to the blade outer air seal assembly.
申请公布号 EP3030755(A1) 申请公布日期 2016.06.15
申请号 EP20140833899 申请日期 2014.08.07
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 TATMAN, NEIL L.;RIOUX, PHILIP ROBERT
分类号 F01D11/18;F01D25/24 主分类号 F01D11/18
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