发明申请
- 专利标题: AIRFOIL CORE SHAPE FOR A TURBINE NOZZLE
- 专利标题(中): 用于涡轮喷嘴的气翼芯形
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申请号: US12138580申请日: 2008-06-13
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公开(公告)号: US20090324415A1公开(公告)日: 2009-12-31
- 发明人: Edward Durell Benjamin, JR. , David John Humanchuk , Daniel David Snook
- 申请人: Edward Durell Benjamin, JR. , David John Humanchuk , Daniel David Snook
- 申请人地址: US NY Schenectady
- 专利权人: GENERAL ELECTRIC COMPANY
- 当前专利权人: GENERAL ELECTRIC COMPANY
- 当前专利权人地址: US NY Schenectady
- 主分类号: F01D5/14
- IPC分类号: F01D5/14
摘要:
An article of manufacture includes an object having an airfoil core shape. The airfoil core shape has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in TABLE 1 where X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances are joined smoothly with one another to form a complete airfoil core shape.
公开/授权文献
- US08057169B2 Airfoil core shape for a turbine nozzle 公开/授权日:2011-11-15
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