发明名称 Seal and airfoil tip clearance control
摘要 <p>A turbine section includes a housing (31) and a blade outer air seal (42) to be mounted on the housing. A flex beam (34) mounts the blade outer air seal (42) onto the housing (31), with the flex beam (34) being supported on the housing (31), but free to move relative to the housing (31). A pressure air chamber (30) is formed on an opposed side of the flex beam (34) from the blade outer air seal (42). A source of pressurized air is delivered into the chamber (30) to cause the flex beam (34) to move the blade outer air seal (42) toward and away from a central axis of the housing (31).</p>
申请公布号 EP2392780(A2) 申请公布日期 2011.12.07
申请号 EP20110168277 申请日期 2011.05.31
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 WAGNER, JOEL H.
分类号 F01D11/22 主分类号 F01D11/22
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