公开(公告)号：US20070177981A1

公开(公告)日：2007-08-02

申请号：US11340577

申请日：2006-01-27

申请人： Thomas Vandeputte ,  John Greene ,  Peter Selent ,  Linda Farral ,  Sze Bun Chan ,  Brian Arness

发明人： Thomas Vandeputte ,  John Greene ,  Peter Selent ,  Linda Farral ,  Sze Bun Chan ,  Brian Arness

IPC分类号： B64C27/46

CPC分类号： F01D5/141 ,  F05D2240/128 ,  F05D2250/74 ,  Y10S416/02

摘要： First stage stator vanes for a turbine comprised airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in inches in Table I, which define a plurality of radially spaced profile sections forming the nominal profile. The Z coordinate values for each profile section are radial distances from the turbine axis to a portion of the surface of revolution about the axis containing the profile section. The X and Y values for each profile section are coordinate values which, when connected by smooth continuing arcs define the airfoil profile section along the surface of revolution portion. The radially spaced profile sections are joined smoothly with one another to form the nominal airfoil profile.

摘要翻译： 用于涡轮机的第一级定子叶片包括基本上按照表I中以英寸为单位的X，Y和Z的笛卡尔坐标值的翼型分布，其定义了形成标称轮廓的多个径向间隔的轮廓部分。 每个轮廓截面的Z坐标值是从涡轮机轴线到围绕围绕轮廓部分的轴线的旋转表面的一部分的径向距离。 每个轮廓截面的X和Y值是坐标值，当通过平滑的连续弧连接时，沿着旋转部分的表面限定翼型轮廓部分。 径向隔开的轮廓部分彼此平滑地连接以形成标称翼型轮廓。

公开(公告)号：US20050025618A1

公开(公告)日：2005-02-03

申请号：US10630750

申请日：2003-07-31

申请人： Brian Arness ,  Robert By ,  Gunnar Siden ,  Poornathresan Krishnakumar ,  Bruce Smith ,  Peter Selent

发明人： Brian Arness ,  Robert By ,  Gunnar Siden ,  Poornathresan Krishnakumar ,  Bruce Smith ,  Peter Selent

IPC分类号： F01D9/02 ,  F01D5/14 ,  F01D1/02

CPC分类号： F01D5/142 ,  F01D5/141

摘要： The third stage nozzle has an airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein X and Y values are in inches and define airfoil profile sections at each distance Z and Z are non-dimensional values within a range from 0.1 to 0.9 convertible to Z distances in inches by multiplying the Z values of Table I within said range by a height of the airfoil in inches. The profile sections at the Z distances are joined smoothly with one another to form the nozzle airfoil shape. The X and Y distances may be scalable to provide a scaled-up or scaled-down airfoil for the nozzle. The nominal airfoil given by the X, Y and Z distances lies within an envelope of ±0.160 inches.

摘要翻译： 第三级喷嘴具有基本上根据表I中列出的X，Y和Z的笛卡尔坐标值的翼型分布，其中X和Y值以英寸为单位，并且在每个距离Z和Z是非尺寸值，限定翼型剖面部分 在0.1至0.9的范围内，通过将表I的Z值乘以所述范围内的翼型高度（英寸），以英寸计算Z距离。 在Z距离处的轮廓部分彼此平滑地连接以形成喷嘴翼型形状。 X和Y距离可以是可缩放的，以为喷嘴提供放大或缩小的翼型。 由X，Y和Z距离给出的额定翼型在±0.160英寸的范围内。