发明名称 AIRFOIL SHAPE FOR A TURBINE BUCKET
摘要 Fourth 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 to 1 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 a complete airfoil shape. The X and Y 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 US2005013695(A1) 申请公布日期 2005.01.20
申请号 US20030621460 申请日期 2003.07.18
申请人 HYDE SUSAN MARIE;BY ROBERT ROMANY;SCHAEFFER JON CONRAD;SIMS CALVIN LEVY;BOISCLAIR MICHAEL ERNEST 发明人 HYDE SUSAN MARIE;BY ROBERT ROMANY;SCHAEFFER JON CONRAD;SIMS CALVIN LEVY;BOISCLAIR MICHAEL ERNEST
分类号 F01D5/18;F01D5/00;F01D5/14;(IPC1-7):B63H1/26 主分类号 F01D5/18
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