发明名称 |
AIR TRANSFER BUSHING |
摘要 |
PURPOSE: To provide a gas turbine engine having an air transfer assembly with a replaceable temperature control air transfer tube. CONSTITUTION: An air transfer assembly 10 transfers temperature control air 21 from an annular plenum 20 to an annular manifold 30 through an air transfer tube 15 interposed therebetween. The air transfer tube prevents temperature control air leakage while it is permitted to slide between a limit set by an air transfer bushing assembly and a limit set by a manifold cup 75 formed in the annular manifold. An air transfer bushing 35 is removable and is installed in an aperture in an outer support 25. The manifold cup is formed in the annular manifold.
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申请公布号 |
JPH05214959(A) |
申请公布日期 |
1993.08.24 |
申请号 |
JP19920172170 |
申请日期 |
1992.06.30 |
申请人 |
GENERAL ELECTRIC CO <GE> |
发明人 |
BINSENTO MARION DORERATSUPU;HARORUDO REI HANSERU |
分类号 |
F02C7/18;F01D5/18;F01D9/02;F01D9/04;F01D9/06;F01D11/00;F02C9/18 |
主分类号 |
F02C7/18 |
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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