发明申请
- 专利标题: TURBINE STAGE SHROUD SEGMENT
- 专利标题(中): 涡轮级SHROUD SEGMENT
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申请号: US13177151申请日: 2011-07-06
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公开(公告)号: US20120027576A1公开(公告)日: 2012-02-02
- 发明人: Ian TIBBOTT , Peter IRELAND , Anthony J. RAWLINSON , Lynne H. TURNER
- 申请人: Ian TIBBOTT , Peter IRELAND , Anthony J. RAWLINSON , Lynne H. TURNER
- 申请人地址: GB 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: GB London
- 优先权: GB1012783.5 20100730
- 主分类号: F01D25/14
- IPC分类号: F01D25/14 ; B23P15/00 ; F01D25/12
摘要:
A shroud segment for a turbine stage of a gas turbine engine forms an endwall for the working gas annulus of the stage. The segment also provides a close clearance to the tips of a row of turbine blades which sweep across the segment. In use a leakage flow of the working gas passes through the clearance gap between the blade tips and the segment. The segment has a plurality of cooling holes and respective air feed passages for the cooling holes. The cooling holes are distributed over that part of the gas-washed surface of the segment which is swept by the blade tips. The cooling holes deliver, in use, cooling air which spreads over the gas-washed surface. The feed passages are configured such that the delivered air opposes the leakage flow of the working gas.
公开/授权文献
- US08714918B2 Turbine stage shroud segment 公开/授权日:2014-05-06
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