发明申请
- 专利标题: GAS TURBINE ENGINE COMPONENT
- 专利标题(中): 气体涡轮发动机部件
-
申请号: US13408251申请日: 2012-02-29
-
公开(公告)号: US20120251295A1公开(公告)日: 2012-10-04
- 发明人: Lynne H. TURNER , Peter T. IRELAND , Ian TIBBOTT , Anthony J. RAWLINSON
- 申请人: Lynne H. TURNER , Peter T. IRELAND , Ian TIBBOTT , Anthony J. RAWLINSON
- 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: GB1105105.9 20110328
- 主分类号: F01D5/18
- IPC分类号: F01D5/18
摘要:
A component of a gas turbine engine is provided. The component includes an external wall which, in use, is exposed on one surface thereof to working gas flowing through the engine. The component further includes effusion cooling holes formed in the external wall. In use, cooling air blows through the cooling holes to form a cooling film on the surface of the external wall exposed to the working gas. The component further includes an air inlet arrangement which receives the cooling air for distribution to the cooling holes. The component further includes a plurality of metering feeds and a plurality of supply plena. The metering feeds meter the cooling air from the air inlet arrangement to respective of the supply plena, which in turn supply the metered cooling air to respective portions of the cooling holes.
信息查询