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    AIRFOIL SHAPE FOR A TURBINE NOZZLE
    1.
    发明申请
    AIRFOIL SHAPE FOR A TURBINE NOZZLE 有权
    涡轮喷嘴气翼形状

    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。

    AIRFOIL SHAPE FOR A TURBINE BUCKET
    2.
    发明申请
    AIRFOIL SHAPE FOR A TURBINE BUCKET 有权
    用于涡轮马桶的气翼形状

    公开(公告)号：US20050031453A1

    公开(公告)日：2005-02-10

    申请号：US10632853

    申请日：2003-08-04

    申请人： Daniel Snook ,  Robert By ,  Bruce Smith ,  Gunnar Siden ,  Carlos Collado ,  Peter Cleveland

    发明人： Daniel Snook ,  Robert By ,  Bruce Smith ,  Gunnar Siden ,  Carlos Collado ,  Peter Cleveland

    IPC分类号： F01D5/14

    CPC分类号： F01D5/141 ,  Y10S416/02

    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 0.03 span to 0.95 span 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 the bucket 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 envelop of ±0.150 inches in directions normal to the surface of the airfoil.

    摘要翻译： 第三级涡轮机叶片具有基本上符合X，Y和Z的笛卡尔坐标值的翼型轮廓，其中X和Y值表示在表I中，其中X和Y值以英寸为单位，Z值是从0.03跨度到0.95跨度可变为Z的无量纲值 通过将Z值乘以翼型件的高度（英寸），以英寸为单位。 X和Y值是通过平滑连续的弧连接时定义每个距离Z处的翼型轮廓部分的距离。每个距离Z处的轮廓部分彼此平滑地连接以形成铲斗翼型形状。 X，Y和Z距离可以作为相同常数或数字的函数来缩放，以提供用于铲斗的放大或缩小的翼型部分。 由X，Y和Z距离给出的额定翼型在垂直于翼面表面的方向上在±0.150英寸的范围内。