发明名称 |
Shroud assembly and method of machining the same |
摘要 |
A method of machining an inner surface (56) of a shroud assembly (42) extending generally circumferentially around a central axis of a gas turbine aircraft engine. The method includes determining pre-machined radial clearances (60) during flight between tips (26) of rotor blades (20) in the engine and the inner surface (56) of the shroud assembly (42) at each of a plurality of circumferentially spaced locations around the shroud assembly (42). The inner surface (56) of the shroud assembly (42) is machined based on the pre-machined radial clearances (60) to provide a generally uniform post-machined radial clearance (60) during flight between the tips (26) of the rotor blades (20) and the inner surface (56) of the shroud assembly (42) at each of the circumferentially spaced locations around the shroud assembly (42). <IMAGE> |
申请公布号 |
EP1233148(B1) |
申请公布日期 |
2012.10.17 |
申请号 |
EP20020251042 |
申请日期 |
2002.02.15 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
STOW, JONATHAN JAMES |
分类号 |
F01D9/04;F01D11/08;F01D5/00;F01D9/02;F01D11/14;F01D11/18;F01D11/24;F01D21/04;F01D25/26 |
主分类号 |
F01D9/04 |
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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