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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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