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: US13216824申请日: 2011-08-24
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公开(公告)号: US20120057961A1公开(公告)日: 2012-03-08
- 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: GB1014802.1 20100907
- 主分类号: F01D5/22
- IPC分类号: F01D5/22 ; B23P15/04 ; 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 mainstream flow of the working gas passes through the passages formed between adjacent turbine blades. 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 has swirl directions which are co-directionally aligned with the swirl directions of the mainstream flow at the segment.
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