Patent ReferencesGas turbine engine blade Turbine nozzle Bucket for the last stage of a steam turbine Bucket for the last stage of a steam turbine Turbine blade with enhanced cooling and profile optimization Patent #: 5980209 Inventors
ApplicationNo. 886406 filed on 06/22/2001US Classes:416/243, Concave surface416/223ATurbo machineExaminersPrimary: Look, Edward K.Assistant: Nguyen, Ninh H. Attorney, Agent or FirmInternational ClassF01D 005/14AbstractThe third-stage buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in inches 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.Other References
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