发明名称 MOVABLE AIR SEAL FOR GAS TURBINE ENGINE
摘要 A blade tip clearance control system for an engine case of a gas turbine engine according to one disclosed non-limiting embodiment of the present disclosure includes an air seal segment within the engine case. A drive link extends through the engine case, the drive link mounted to the air seal segment.
申请公布号 US2016047266(A1) 申请公布日期 2016.02.18
申请号 US201414779602 申请日期 2014.03.28
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Powell Brad
分类号 F01D11/22 主分类号 F01D11/22
代理机构 代理人
主权项 1. A blade tip clearance control system for an engine case of a gas turbine engine comprising: an air seal segment within the engine case; and a drive link that extends through the engine case, said drive link mounted to said air seal segment.
地址 Hartford CT US
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