发明名称 Seal means for a gas turbine engine
摘要 A pressure seal for separating elements of a gas turbine engine shroud assembly. The seal accommodates for differing rates and magnitudes of thermal expansion and is not significantly affected by eccentricities of out-of-roundness between the shroud elements. The seal is annular and has a generally Y-shaped cross section. The bifurcated or divergent elements of the seal are clamped within the base without welding.
申请公布号 US3869222(A) 申请公布日期 1975.03.04
申请号 US19730368003 申请日期 1973.06.07
申请人 FORD MOTOR COMPANY 发明人 RAHNKE, CHRISTIAN J.;VALLANCE, JAMES K.
分类号 F01D11/00;F01D25/08;F02C7/20;(IPC1-7):F01D25/12;F01D25/14;F01D25/26 主分类号 F01D11/00
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