发明授权
- 专利标题: Rotor shroud assembly
- 专利标题(中): 转子罩组件
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申请号: US59292申请日: 1993-05-11
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公开(公告)号: US5330321A公开(公告)日: 1994-07-19
- 发明人: Michael C. Roberts , John F. Leonard
- 申请人: Michael C. Roberts , John F. Leonard
- 申请人地址: GB2 London
- 专利权人: Rolls Royce plc
- 当前专利权人: Rolls Royce plc
- 当前专利权人地址: GB2 London
- 优先权: GBX9210642.6 19920519
- 主分类号: F01D11/18
- IPC分类号: F01D11/18 ; F01D11/08
摘要:
In a gas turbine engine tip clearance between rotor blades and an encircling shroud liner is controlled by moving the shroud liner radially to match the thermal and centrifugal growth of the rotor assembly. The shroud liner segments are suspended between two axially displaced control rings located in a passageway carrying air ducted from the compressor. One control ring responds very quickly to changes in gas temperature corresponding to centrifugal growth and blade thermal growth. The other ring responds very much more slowly and corresponds to the thermal growth of the disc. The shroud liner segments are suspended from the control rings to adopt a position that constitutes the average between the growth positions of the two control rings.
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