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1. 发明授权

US08807950B2 Turbine nozzle airfoil profile 有权
标题翻译：涡轮喷嘴翼型
公开(公告)号：US08807950B2
公开(公告)日：2014-08-19
申请号：US13304728
申请日：2011-11-28
申请人： Craig Allen Bielek , Veeraporn Kullatham , Mary Holloway
发明人： Craig Allen Bielek , Veeraporn Kullatham , Mary Holloway
IPC分类号： F01D5/14
CPC分类号： F01D5/142 , F05D2250/74
摘要： The present application provides a turbine nozzle including an airfoil shape. The airfoil shape may have a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances in inches by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in inches. The X and Y values are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The airfoil profile sections at Z distances may be joined smoothly with one another to form a complete airfoil shape.
摘要翻译：本申请提供了一种包括翼型形状的涡轮喷嘴。翼型可以具有基本上根据表1所示的X，Y和Z的笛卡尔坐标值的标称轮廓.X，Y和Z的笛卡尔坐标值是0％至100％的无量纲值可转换为通过将X，Y和Z的笛卡尔坐标值乘以翼型件的高度（英寸），以英寸为单位的尺寸距离。 X和Y值是以英寸为单位的距离，当通过平滑连续的弧连接时，在每个距离Z处限定翼型轮廓部分.Z距离处的翼型轮廓部分可以彼此平滑地连接以形成完整的翼型形状。

2. 发明申请

US20130136607A1 TURBINE NOZZLE AIRFOIL PROFILE 有权
标题翻译：涡轮喷嘴气翼型材
公开(公告)号：US20130136607A1
公开(公告)日：2013-05-30
申请号：US13304728
申请日：2011-11-28
申请人： Craig Allen Bielek , Veeraporn Kullatham , Mary Holloway
发明人： Craig Allen Bielek , Veeraporn Kullatham , Mary Holloway
IPC分类号： F01D5/14
CPC分类号： F01D5/142 , F05D2250/74
摘要： The present application provides a turbine nozzle including an airfoil shape. The airfoil shape may have a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances in inches by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in inches. The X and Y values are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The airfoil profile sections at Z distances may be joined smoothly with one another to form a complete airfoil shape.
摘要翻译：本申请提供了一种包括翼型形状的涡轮喷嘴。翼型可以具有基本上根据表1所示的X，Y和Z的笛卡尔坐标值的标称轮廓.X，Y和Z的笛卡尔坐标值是0％至100％的无量纲值可转换为通过将X，Y和Z的笛卡尔坐标值乘以翼型件的高度（英寸），以英寸为单位的尺寸距离。 X和Y值是以英寸为单位的距离，当通过平滑连续的弧连接时，在每个距离Z处限定翼型轮廓部分.Z距离处的翼型轮廓部分可以彼此平滑地连接以形成完整的翼型形状。

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