发明名称 Stator assembly for a gas turbine engine
摘要 A coolable stator assembly is positioned outwardly of an array of rotor blades in a high by pass turbofan gas turbine engine as disclosed. The stator assembly includes case tied air seals positioned by rails and a shield which extends circumferentially about the rails and the rail connector section extending between the rails. Various constructions details for improving the control of clearances and circumferential temperature gradients in the rails are developed. In one particular embodiment, cooling air tubes are employed with the shield.
申请公布号 US4826397(A) 申请公布日期 1989.05.02
申请号 US19880212827 申请日期 1988.06.29
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SHOOK, PAUL S.;KANE, DANIEL E.
分类号 F01D11/10;F01D11/24;(IPC1-7):F04D15/00;F04D29/00 主分类号 F01D11/10
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