发明授权
- 专利标题: Cooled aerofoil blade or vane
- 专利标题(中): 冷却翼型叶片或叶片
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申请号: US12861560申请日: 2010-08-23
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公开(公告)号: US08662825B2公开(公告)日: 2014-03-04
- 发明人: Peter T. Ireland , Howoong Namgoong
- 申请人: Peter T. Ireland , Howoong Namgoong
- 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
- 代理机构: Oliff PLC
- 优先权: GB0915680.3 20090909
- 主分类号: F01D5/18
- IPC分类号: F01D5/18
摘要:
An aerofoil blade or vane suitable for the turbine of a gas turbine engine includes an extending aerofoil portion having facing wall parts interconnected by a divider member to partially define first and second cooling fluid passage portions. The first and second passage portions are interconnected in a series fluid flow relationship by a bend passage portion. The first passage portion directs cooling fluid to the bend portion and the second passage portion exhausts cooling fluid from the bend portion. The divider member provides a localised contraction of the downstream end of the first passage portion to accelerate the cooling fluid flow before it enters the bend passage portion. The divider member provides a localised progressive series narrowing and opening of the upstream end of the second passage portion in the general direction of cooling fluid flow.
公开/授权文献
- US20110058958A1 COOLED AEROFOIL BLADE OR VANE 公开/授权日:2011-03-10
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