发明申请
- 专利标题: ENDWALL COMPONENT FOR A TURBINE STAGE OF A GAS TURBINE ENGINE
- 专利标题(中): 用于涡轮发动机涡轮机段的末端部件
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申请号: US13368718申请日: 2012-02-08
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公开(公告)号: US20120219401A1公开(公告)日: 2012-08-30
- 发明人: Anthony J. RAWLINSON , Peter IRELAND , Lynne H. TURNER , Ian TIBBOTT
- 申请人: Anthony J. RAWLINSON , Peter IRELAND , Lynne H. TURNER , Ian TIBBOTT
- 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: GB1103176.2 20110224
- 主分类号: F01D9/02
- IPC分类号: F01D9/02
摘要:
A component of a turbine stage of a gas turbine engine is provided, the component forming an endwall for the working gas annulus of the stage. The component has one or more internal plena behind the endwall which, in use, contain a flow of cooling air. The component further has a plurality of exhaust holes in the endwall. The holes connect the plena to a gas-washed surface of the endwall such that the cooling air effuses through the holes to form a cooling film over the gas-washed surface. Each exhaust hole has a flow cross-sectional area which is greater at an intermediate position between the entrance of the hole from the respective plenum and the exit of the hole to the gas-washed surface than it is at said exit.
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