发明申请
- 专利标题: AIRFOIL SHAPE FOR A TURBINE NOZZLE
- 专利标题(中): 涡轮喷嘴气翼形状
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申请号: US10630750申请日: 2003-07-31
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公开(公告)号: US20050025618A1公开(公告)日: 2005-02-03
- 发明人: Brian Arness , Robert By , Gunnar Siden , Poornathresan Krishnakumar , Bruce Smith , Peter Selent
- 申请人: Brian Arness , Robert By , Gunnar Siden , Poornathresan Krishnakumar , Bruce Smith , Peter Selent
- 主分类号: F01D9/02
- IPC分类号: F01D9/02 ; F01D5/14 ; F01D1/02
摘要:
The third stage nozzle has an airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein X and Y values are in inches and define airfoil profile sections at each distance Z and Z are non-dimensional values within a range from 0.1 to 0.9 convertible to Z distances in inches by multiplying the Z values of Table I within said range by a height of the airfoil in inches. The profile sections at the Z distances are joined smoothly with one another to form the nozzle airfoil shape. The X and Y distances may be scalable to provide a scaled-up or scaled-down airfoil for the nozzle. The nominal airfoil given by the X, Y and Z distances lies within an envelope of ±0.160 inches.
公开/授权文献
- US06866477B2 Airfoil shape for a turbine nozzle 公开/授权日:2005-03-15
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