公开(公告)号：US09234428B2

公开(公告)日：2016-01-12

申请号：US13613922

申请日：2012-09-13

申请人： Randall Richard Good ,  Bradley Taylor Boyer ,  Xiaoyong Fu ,  Aaron Ezekiel Smith ,  Jacob C. Perry, II

发明人： Randall Richard Good ,  Bradley Taylor Boyer ,  Xiaoyong Fu ,  Aaron Ezekiel Smith ,  Jacob C. Perry, II

IPC分类号： F01D5/14 ,  F01D5/18

CPC分类号： F01D5/14 ,  F01D5/187

摘要： Turbine bucket nominal internal core profiles and core insert external profiles are provided. In one embodiment, a turbine bucket includes an airfoil, platform, shank and dovetail. The bucket has a nominal internal core profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1 wherein the Z values are non-dimensional values from 0 to 1 convertible to Z distances in inches by multiplying the Z values by a height of the bucket in inches, and wherein X and Y are non-dimensional values which, when connected by smooth continuing arcs, define internal core profile sections at each distance Z along the bucket, the profile sections at the Z distances being joined smoothly with one another to form said bucket internal core profile.

摘要翻译： 提供涡轮桶标称内芯型材和芯插件外部型材。 在一个实施例中，涡轮机桶包括翼型件，平台，柄和燕尾榫。 铲斗具有基本上根据表1所示的X，Y和Z的笛卡尔坐标值的标称内部芯轮廓，其中Z值是从0到1的无量纲值，可以通过将Z值乘以Z 以铲斗的高度为英寸，其中X和Y为无量纲值，当通过平滑连续的圆弧连接时，沿着铲斗在每个距离Z处限定内芯轮廓部分，Z距离处的轮廓部分被连接 彼此平滑地形成所述桶内芯轮廓。

公开(公告)号：US06739839B1

公开(公告)日：2004-05-25

申请号：US10403696

申请日：2003-03-31

申请人： Theresa A. Brown ,  Majid Ahmadi ,  Eugene Clemens ,  Jacob C. Perry, II ,  Allyn K. Holiday ,  Richard A. Delehanty ,  Ariel Caesar Prepena Jacala

发明人： Theresa A. Brown ,  Majid Ahmadi ,  Eugene Clemens ,  Jacob C. Perry, II ,  Allyn K. Holiday ,  Richard A. Delehanty ,  Ariel Caesar Prepena Jacala

IPC分类号： F01D514

CPC分类号： F01D5/141 ,  F05D2220/76 ,  F05D2240/301 ,  Y10S416/02

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.

摘要翻译： 第一级铲斗具有基本上符合表I中列出的X，Y和Z的笛卡尔坐标值的翼型，其中Z是与垂直于涡轮机中心线的半径并且包含X和Y值的平面的垂直距离 其中Z值在翼型的径向最内部空气动力学部分的X，Y平面处开始为零，X和Y是在每个距离Z处限定翼型轮廓的坐标.X，Y和Z值可以被缩放为函数 相同的常数或数量，以提供用于铲斗的放大或缩小的翼型部分。

公开(公告)号：US06722851B1

公开(公告)日：2004-04-20

申请号：US10385438

申请日：2003-03-12

申请人： Robert Alan Brittingham ,  Edward Durell Benjamin ,  Jacob C. Perry, II

发明人： Robert Alan Brittingham ,  Edward Durell Benjamin ,  Jacob C. Perry, II

IPC分类号： F01D514

CPC分类号： F01D5/147 ,  F01D5/141 ,  F05D2250/20 ,  F05D2250/70 ,  F05D2260/202 ,  Y10S416/02

摘要： First stage turbine buckets have internal core 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 to 1 convertible to Z distances in inches by multiplying the Z values by the height of the bucket in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define internal core profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete internal core profile. 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 internal core profile. The nominal internal core profile given by the X, Y and Z distances lies within an envelope of ±0.039 inches in directions normal to any internal core surface location.

摘要翻译： 第一级涡轮机叶片具有基本上根据表I所示的X，Y和Z的笛卡尔坐标值的内部芯轮廓，其中X和Y值以英寸为单位，Z值是从0到1可转换成Z距离的无量纲值 以英寸乘以Z值乘以桶的高度（英寸）。 X和Y值是当通过光滑连续弧连接时，在每个距离Z处限定内部芯轮廓部分的距离。每个距离Z处的轮廓部分彼此平滑地连接以形成完整的内部芯轮廓。 X，Y和Z距离可以是可扩展的，作为相同常数或数字的函数，以提供按比例放大或缩小的内核配置文件。 由X，Y和Z距离给出的标称内芯型材在垂直于任何内芯表面位置的方向上在±0.039英寸的包络内。

公开(公告)号：US20140069110A1

公开(公告)日：2014-03-13

申请号：US13613922

申请日：2012-09-13

申请人： Randall Richard Good ,  Bradley Taylor Boyer ,  Xiaoyong Fu ,  Aaron Ezekiel Smith ,  Jacob C. Perry, II

发明人： Randall Richard Good ,  Bradley Taylor Boyer ,  Xiaoyong Fu ,  Aaron Ezekiel Smith ,  Jacob C. Perry, II

IPC分类号： F01D5/14

CPC分类号： F01D5/14 ,  F01D5/187

摘要： Turbine bucket nominal internal core profiles and core insert external profiles are provided. In one embodiment, a turbine bucket includes an airfoil, platform, shank and dovetail. The bucket has a nominal internal core profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1 wherein the Z values are non-dimensional values from 0 to 1 convertible to Z distances in inches by multiplying the Z values by a height of the bucket in inches, and wherein X and Y are non-dimensional values which, when connected by smooth continuing arcs, define internal core profile sections at each distance Z along the bucket, the profile sections at the Z distances being joined smoothly with one another to form said bucket internal core profile.

摘要翻译： 提供涡轮桶标称内芯型材和芯插件外部型材。 在一个实施例中，涡轮机桶包括翼型件，平台，柄和燕尾榫。 铲斗具有基本上根据表1所示的X，Y和Z的笛卡尔坐标值的标称内部芯轮廓，其中Z值是从0到1的无量纲值，可以通过将Z值乘以Z 以铲斗的高度为英寸，其中X和Y为无量纲值，当通过平滑连续的圆弧连接时，沿着铲斗在每个距离Z处限定内芯轮廓部分，Z距离处的轮廓部分被连接 彼此平滑地形成所述桶内芯轮廓。