发明名称 ACTIVE CLEARANCE CONTROL FOR GAS TURBINE ENGINE
摘要 A gas turbine engine includes a conduit that is configured to direct a fluid to at least one manifold that is adjacent to a turbine section. A first intake is in fluid communication with the conduit. A second intake is in fluid communication with the conduit. A valve is configured to selectively direct a fluid from at least one of the first intake and the second intake.
申请公布号 EP3126640(A4) 申请公布日期 2017.04.05
申请号 EP20150773710 申请日期 2015.03.23
申请人 United Technologies Corporation 发明人 PHILBRICK, Graham Ryan;LAGUEUX, Ken
分类号 F01D11/24;F02C7/18 主分类号 F01D11/24
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