发明名称 FIRST-STAGE HIGH PRESSURE TURBINE BUCKET AIRFOIL
摘要 The first-stage buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein Z is a perpendicular distance from a plane normal to a radius of the turbine centerline and containing the X and Y values with the Z value commencing at zero in the X, Y plane at the radially innermost aerodynamic section of the airfoil and X and Y are coordinates defining the airfoil profile at each distance Z. The X, Y and Z values may be scaled as a function of the same constant or number to provide a scaled-up or scaled-down airfoil section for the bucket.
申请公布号 KR100871195(B1) 申请公布日期 2008.12.01
申请号 KR20047000388 申请日期 2002.07.09
申请人 发明人
分类号 F01D5/14 主分类号 F01D5/14
代理机构 代理人
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