发明申请
- 专利标题： SEGMENTED COOLING AIR CAVITY FOR TURBINE COMPONENT
- 专利标题（中）： 用于涡轮组件的SEGMENTED冷却空气孔
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申请号： US11861662申请日： 2007-09-26
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公开(公告)号： US20090081025A1公开(公告)日： 2009-03-26
- 发明人: Paul M. Lutjen , Susan M. Tholen
- 申请人： Paul M. Lutjen , Susan M. Tholen
- 主分类号： F02C7/12
- IPC分类号： F02C7/12 ; F02C7/28 ; B29C39/00
摘要：
A component for a gas turbine engine has an airfoil with internal cooling channels for delivering air from a radially outer end of the airfoil toward a radially inner end of the airfoil. The cooling channels are separated from adjacent cooling channels by sets of at least two disconnected wall segments.
公开/授权文献
- US08128348B2 Segmented cooling air cavity for turbine component 公开/授权日：2012-03-06
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