发明名称 Rotatable vane seal
摘要 Means for preventing the wasteful leakage of cooling air within the turbine section of a gas turbine engine is disclosed. A segmented shroud radially separates the flow path for the working medium gases from cooling air supply chambers which are disposed radially outward of the flow path. Rotatable vanes penetrate the shroud and extend into the medium flow path to control the flow of medium gases through the turbine. A ring, which is split, is urged against the vane and the adjacent shroud segments in operative response to a spring member to prevent the excess leakage of cooling air therebetween.
申请公布号 US3995971(A) 申请公布日期 1976.12.07
申请号 US19750583141 申请日期 1975.06.02
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 WHITE, LOREN HAWDON
分类号 F01D17/16;(IPC1-7):F01D17/16;F01D17/14 主分类号 F01D17/16
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