发明申请
- 专利标题： GAS TURBINE ENGINE COMPONENT COOLING SCHEME
- 专利标题（中）： 气体涡轮发动机组件冷却方案
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申请号： US12953514申请日： 2010-11-24
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公开(公告)号： US20110070082A1公开(公告)日： 2011-03-24
- 发明人: Raymond Surace , Andrew D. Milliken
- 申请人： Raymond Surace , Andrew D. Milliken
- 主分类号： B64C27/00
- IPC分类号： B64C27/00
摘要：
A method of cooling a gas turbine engine component includes creating a cooling channel within a platform of the component, communicating cooling air into the cooling channel to cool the platform, and recycling the cooling airflow used to cool the platform by communicating the cooling airflow from the cooling channel into the airfoil to cool the airfoil.
公开/授权文献
- US08403632B2 Gas turbine engine component cooling scheme 公开/授权日：2013-03-26
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