发明名称 AIRFOIL SHAPE FOR A TURBINE BUCKET
摘要 Second 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 0.05 to 0.95 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 ±0.160 inches in directions normal to the surface of the airfoil.
申请公布号 US2005079061(A1) 申请公布日期 2005.04.14
申请号 US20030681144 申请日期 2003.10.09
申请人 GENERAL ELECTRIC COMPANY 发明人 BEDDARD THOMAS BRADLEY;PESETSKY DAVID SAMUEL
分类号 F01D5/06;F01D5/14;(IPC1-7):B63H1/26 主分类号 F01D5/06
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