发明名称 FLOW DIRECTING ASSEMBLY FOR A GAS TURBINE ENGINE
摘要 <p>A non-rotating flow directing assembly for a gas turbine engine is disclosed. The flow directing assembly is formed of a circumferentially segmented inner case supported by an annular sleeve. The inner case is formed of a plurality of arcuate segments extending axially continuously through the engine. A method of assembling the circumferentially continuous annular sleeve about an axially continuous rotor is also disclosed. In an alternate embodiment the inner case is formed of several pluralities of arcuate segments.</p>
申请公布号 CA1162148(A) 申请公布日期 1984.02.14
申请号 CA19810376278 申请日期 1981.04.27
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BRODELL, ROBERT F.;COMEAU, ROGER J.;MONSARRAT, WILLIAM G.
分类号 F01D25/24;F01D25/26;(IPC1-7):F01D1/04 主分类号 F01D25/24
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