发明名称 Airfoil shape for a turbine nozzle
摘要 The second 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 is a non-dimensional value from 0 to 1 convertible to Z distances in inches by multiplying the Z values of Table I by a height of the airfoil in inches. The profile sections at the Z distances are joined smoothly with one another to form a complete 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 ±0.100 inches.
申请公布号 US6722853(B1) 申请公布日期 2004.04.20
申请号 US20020301724 申请日期 2002.11.22
申请人 GENERAL ELECTRIC COMPANY 发明人 HUMANCHUK DAVID JOHN;HAFNER MATTHEW TROY;FEHLBERG JAMES B.
分类号 F01D5/14;(IPC1-7):F01D5/14 主分类号 F01D5/14
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