发明名称 Airfoil shape for a turbine bucket
摘要 Third stage turbine buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z values are non-dimensional values from 0.03 span to 0.95 span convertible to Z distances in inches by multiplying the Z values by the height of the airfoil in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form the bucket airfoil shape. The X, Y and Z distances may be scalable as a function of the same constant or number to provide a scaled up or scaled down airfoil section for the bucket. The nominal airfoil given by the X, Y and Z distances lies within an envelop of ±0.150 inches in directions normal to the surface of the airfoil.
申请公布号 US6857855(B1) 申请公布日期 2005.02.22
申请号 US20030632853 申请日期 2003.08.04
申请人 GENERAL ELECTRIC COMPANY 发明人 SNOOK DANIEL DAVID;BY ROBERT ROMANY;SMITH BRUCE LOREN;SIDEN GUNNAR LEIF;COLLADO CARLOS ALBERTO;CLEVELAND PETER GAINES
分类号 F01D5/14;(IPC1-7):F01D5/14 主分类号 F01D5/14
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