发明名称 Airfoil shape for a turbine bucket and turbine incorporating same
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 to 1 convertible to Z distances in inches by multiplying the Z' values by the height of the airfoil in inches and adding the radius of the airfoil base. 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, 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 envelope of ±0.0.060 inches in directions normal to the surface of the airfoil.
申请公布号 US2009035145(A1) 申请公布日期 2009.02.05
申请号 US20070882373 申请日期 2007.08.01
申请人 GENERAL ELECTRIC COMPANY 发明人 DELONG JON ROBERT;BIELEK CRAIG ALLEN;HAYES TOMMY DEE;LAGRANGE BENJAMIN ARNETTE;JOHNSON SCOTT F.
分类号 F01D5/14 主分类号 F01D5/14
代理机构 代理人
主权项
地址