发明名称 Airfoil shape for a turbine nozzle
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 the 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.
申请公布号 US6866477(B2) 申请公布日期 2005.03.15
申请号 US20030630750 申请日期 2003.07.31
申请人 GENERAL ELECTRIC COMPANY 发明人 ARNESS BRIAN PETER;BY ROBERT ROMANY;SIDEN GUNNAR LEIF;KRISHNAKUMAR POORNATHRESAN;SMITH BRUCE LOREN;SELENT PETER CHRISTOPHER
分类号 F01D9/02;F01D5/14;(IPC1-7):F01D9/04 主分类号 F01D9/02
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