公开(公告)号：US08961119B2

公开(公告)日：2015-02-24

申请号：US13526941

申请日：2012-06-19

申请人： Matthew John McKeever ,  Gang Liu

发明人： Matthew John McKeever ,  Gang Liu

IPC分类号： F01D9/02

CPC分类号： F01D5/141 ,  F04D29/544 ,  F05D2250/74

摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in scalable Table 1 wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined smoothly with one another to form a complete airfoil shape.

摘要翻译： 具有基本上按照可伸缩表1中提出的X，Y和Z的笛卡尔坐标值的标称翼型分布的制品，其中X，Y和Z的笛卡尔坐标值是通过乘以可转换成尺寸距离的无量纲值 X，Y和Z的笛卡尔坐标值为数，其中X和Y是当通过连续弧连接时在每个Z高度处限定翼型轮廓部分的坐标，每个Z高度处的翼型轮廓部分平滑地与 彼此形成一个完整的翼型。

公开(公告)号：US20130336780A1

公开(公告)日：2013-12-19

申请号：US13526941

申请日：2012-06-19

申请人： Matthew John McKeever ,  Gang Liu

发明人： Matthew John McKeever ,  Gang Liu

IPC分类号： F03B11/02

CPC分类号： F01D5/141 ,  F04D29/544 ,  F05D2250/74

摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in scalable Table 1 wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined smoothly with one another to form a complete airfoil shape.

摘要翻译： 具有基本上按照可伸缩表1中提出的X，Y和Z的笛卡尔坐标值的标称翼型分布的制品，其中X，Y和Z的笛卡尔坐标值是通过乘以可转换成尺寸距离的无量纲值 X，Y和Z的笛卡尔坐标值为数，其中X和Y是当通过连续弧连接时在每个Z高度处限定翼型轮廓部分的坐标，每个Z高度处的翼型轮廓部分平滑地与 彼此形成一个完整的翼型。

公开(公告)号：US20130336777A1

公开(公告)日：2013-12-19

申请号：US13526863

申请日：2012-06-19

申请人： Matthew John McKeever ,  Gang Liu ,  Umesh Garg ,  Ryan Wesley Murphy ,  Edward Charles Schurr ,  Michael James Dutka ,  Govindarajan Rengarajan ,  Paul Griffin Delvernois ,  Ya-Tien Chiu ,  Roger Claude Beharrysingh ,  Marc Edward Blohm ,  SenthilKumar Narendran

发明人： Matthew John McKeever ,  Gang Liu ,  Umesh Garg ,  Ryan Wesley Murphy ,  Edward Charles Schurr ,  Michael James Dutka ,  Govindarajan Rengarajan ,  Paul Griffin Delvernois ,  Ya-Tien Chiu ,  Roger Claude Beharrysingh ,  Marc Edward Blohm ,  SenthilKumar Narendran

IPC分类号： F03B11/02

CPC分类号： F04D29/542 ,  F01D5/141 ,  F01D5/142 ,  F01D9/02 ,  F04D29/544 ,  F05D2250/74

摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLES 1-11, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

摘要翻译： 具有基本上按照可伸缩表格中阐述的X，Y和Z的笛卡尔坐标值的标称翼型分布的制品，该可伸缩表从由表1-11组成的表组中选择，其中笛卡尔坐标值 X，Y和Z是通过将X，Y和Z的笛卡尔坐标值乘以数的可转换为尺寸距离的无量纲值，并且其中X和Y是当通过连续弧连接时限定翼型轮廓截面的坐标 在每个Z高度处，每个Z高度处的翼型轮廓部分彼此连接以形成完整的翼型形状。

公开(公告)号：US09017019B2

公开(公告)日：2015-04-28

申请号：US13526863

申请日：2012-06-19

申请人： Matthew John McKeever ,  Gang Liu ,  Umesh Garg ,  Ryan Wesley Murphy ,  Edward Charles Schurr ,  Michael James Dutka ,  Govindarajan Rengarajan ,  Paul Griffin Delvernois ,  Ya-Tien Chiu ,  Roger Claude Beharrysingh ,  Marc Edward Blohm ,  SenthilKumar Narendran

发明人： Matthew John McKeever ,  Gang Liu ,  Umesh Garg ,  Ryan Wesley Murphy ,  Edward Charles Schurr ,  Michael James Dutka ,  Govindarajan Rengarajan ,  Paul Griffin Delvernois ,  Ya-Tien Chiu ,  Roger Claude Beharrysingh ,  Marc Edward Blohm ,  SenthilKumar Narendran

IPC分类号： F01D9/02 ,  F04D29/54 ,  F01D5/14

CPC分类号： F04D29/542 ,  F01D5/141 ,  F01D5/142 ,  F01D9/02 ,  F04D29/544 ,  F05D2250/74

摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLES 1-11, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

摘要翻译： 具有基本上按照可伸缩表格中阐述的X，Y和Z的笛卡尔坐标值的标称翼型分布的制品，该可伸缩表从由表1-11组成的表组中选择，其中笛卡尔坐标值 X，Y和Z是通过将X，Y和Z的笛卡尔坐标值乘以数的可转换为尺寸距离的无量纲值，并且其中X和Y是当通过连续弧连接时限定翼型轮廓截面的坐标 在每个Z高度处，每个Z高度处的翼型轮廓部分彼此连接以形成完整的翼型形状。

公开(公告)号：US08936441B2

公开(公告)日：2015-01-20

申请号：US13526920

申请日：2012-06-19

申请人： Matthew John McKeever ,  Ryan Wesley Murphy

发明人： Matthew John McKeever ,  Ryan Wesley Murphy

IPC分类号： F01D5/14

CPC分类号： F01D5/141 ,  F04D29/544 ,  F05D2250/74

摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in scalable Table 1 wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

摘要翻译： 具有基本上按照可伸缩表1中提出的X，Y和Z的笛卡尔坐标值的标称翼型分布的制品，其中X，Y和Z的笛卡尔坐标值是通过乘以可转换成尺寸距离的无量纲值 X，Y和Z的笛卡尔坐标值为数，其中X和Y是当通过连续弧连接时在每个Z高度处限定翼型轮廓部分的坐标，每个Z高度处的翼型轮廓部分与一个 另一个形成一个完整的翼型。

公开(公告)号：US20140030098A1

公开(公告)日：2014-01-30

申请号：US13556323

申请日：2012-07-24

申请人： Michael James Dutka ,  John Duong ,  Ya-Tien Chiu ,  Alexander David Shrum ,  Kelvin Rono Aaron ,  Christopher Edward LaMaster ,  San-Dar Gau ,  Franco Monteleone ,  Paul Griffin Delvernois ,  Matthew John McKeever ,  Govindarajan Rengarajan ,  Jeremy Peter Latimer ,  Marc Edward Blohm ,  Eric Richard Bonini ,  Venkata Siva Prasad Chaluvadi ,  Jamie Dean Lumpkin ,  Thomas Robbins Tipton

发明人： Michael James Dutka ,  John Duong ,  Ya-Tien Chiu ,  Alexander David Shrum ,  Kelvin Rono Aaron ,  Christopher Edward LaMaster ,  San-Dar Gau ,  Franco Monteleone ,  Paul Griffin Delvernois ,  Matthew John McKeever ,  Govindarajan Rengarajan ,  Jeremy Peter Latimer ,  Marc Edward Blohm ,  Eric Richard Bonini ,  Venkata Siva Prasad Chaluvadi ,  Jamie Dean Lumpkin ,  Thomas Robbins Tipton

IPC分类号： F01D5/30 ,  F01D5/14

CPC分类号： F01D5/3038 ,  F04D29/322 ,  F05D2250/74

摘要： An article of manufacture has a first component configured for use with a turbomachine. The first component is configured for attachment to a second component, and reduces the possibility of attachment with an undesired third component by modification of a. characteristic of the first component. This modification is matched by a complementary characteristic of the second component. The first component has a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table selected from the group consisting of TABLES 1-11. Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying by a number. X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height. The airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

摘要翻译： 制造品具有配置成与涡轮机一起使用的第一部件。 第一部件被配置为附接到第二部件，并且通过修改a来减少与不希望的第三部件的连接的可能性。 第一部分的特征。 该修改由第二组件的互补特性匹配。 第一部件具有基本上根据从由表1-11组成的组中选择的可缩放表格中阐述的X，Y和Z的笛卡尔坐标值的标称翼型分布。 X，Y和Z的笛卡尔坐标值是通过乘以数字可转换为尺寸距离的无量纲值。 X和Y是当通过连续弧连接时在每个Z高度处限定翼型轮廓部分的坐标。 每个Z高度处的翼型轮廓部分彼此连接以形成完整的翼型形状。

公开(公告)号：US20130336798A1

公开(公告)日：2013-12-19

申请号：US13526832

申请日：2012-06-19

申请人： Michael James Dutka ,  John Duong ,  Ya-Tien Chiu ,  Alexander David Shrum ,  Kelvin Rono Aaron ,  Christopher Edward LaMaster ,  San-Dar Gau ,  Franco Monteleone ,  Paul Griffin Delvernois ,  Matthew John McKeever ,  Govindarajan Rengarajan ,  Jeremy Peter Latimer ,  Marc Edward Blohm ,  Eric Richard Bonini ,  Venkata Siva Prasad Chaluvadi

发明人： Michael James Dutka ,  John Duong ,  Ya-Tien Chiu ,  Alexander David Shrum ,  Kelvin Rono Aaron ,  Christopher Edward LaMaster ,  San-Dar Gau ,  Franco Monteleone ,  Paul Griffin Delvernois ,  Matthew John McKeever ,  Govindarajan Rengarajan ,  Jeremy Peter Latimer ,  Marc Edward Blohm ,  Eric Richard Bonini ,  Venkata Siva Prasad Chaluvadi

IPC分类号： F04D29/38

CPC分类号： F04D29/324 ,  F01D5/141 ,  F05D2250/74

摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLES 1-11, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

公开(公告)号：US20130336779A1

公开(公告)日：2013-12-19

申请号：US13526920

申请日：2012-06-19

申请人： Matthew John McKeever ,  Ryan Wesley Murphy

发明人： Matthew John McKeever ,  Ryan Wesley Murphy

IPC分类号： F03B11/02

CPC分类号： F01D5/141 ,  F04D29/544 ,  F05D2250/74

摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in scalable Table 1 wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

摘要翻译： 具有基本上按照可伸缩表1中提出的X，Y和Z的笛卡尔坐标值的标称翼型分布的制品，其中X，Y和Z的笛卡尔坐标值是通过乘以可转换成尺寸距离的无量纲值 X，Y和Z的笛卡尔坐标值为数，其中X和Y是当通过连续弧连接时在每个Z高度处限定翼型轮廓部分的坐标，每个Z高度处的翼型轮廓部分与一个 另一个形成一个完整的翼型。

公开(公告)号：US09175693B2

公开(公告)日：2015-11-03

申请号：US13526832

申请日：2012-06-19

申请人： Michael James Dutka ,  John Duong ,  Ya-Tien Chiu ,  Alexander David Shrum ,  Kelvin Rono Aaron ,  Christopher Edward LaMaster ,  San-Dar Gau ,  Franco Monteleone ,  Paul Griffin Delvernois ,  Matthew John McKeever ,  Govindarajan Rengarajan ,  Jeremy Peter Latimer ,  Marc Edward Blohm ,  Eric Richard Bonini ,  Venkata Siva Prasad Chaluvadi

发明人： Michael James Dutka ,  John Duong ,  Ya-Tien Chiu ,  Alexander David Shrum ,  Kelvin Rono Aaron ,  Christopher Edward LaMaster ,  San-Dar Gau ,  Franco Monteleone ,  Paul Griffin Delvernois ,  Matthew John McKeever ,  Govindarajan Rengarajan ,  Jeremy Peter Latimer ,  Marc Edward Blohm ,  Eric Richard Bonini ,  Venkata Siva Prasad Chaluvadi

IPC分类号： F01D5/14 ,  F01D5/16 ,  F04D29/32

CPC分类号： F04D29/324 ,  F01D5/141 ,  F05D2250/74

摘要： An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLES 1-11, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

公开(公告)号：US09145777B2

公开(公告)日：2015-09-29

申请号：US13556323

申请日：2012-07-24

申请人： Michael James Dutka ,  John Duong ,  Ya-Tien Chiu ,  Alexander David Shrum ,  Kelvin Rono Aaron ,  Christopher Edward LaMaster ,  San-Dar Gau ,  Franco Monteleone ,  Paul Griffin Delvernois ,  Matthew John McKeever ,  Govindarajan Rengarajan ,  Jeremy Peter Latimer ,  Marc Edward Blohm ,  Eric Richard Bonini ,  Venkata Siva Prasad Chaluvadi ,  Jamie Dean Lumpkin ,  Thomas Robbins Tipton

发明人： Michael James Dutka ,  John Duong ,  Ya-Tien Chiu ,  Alexander David Shrum ,  Kelvin Rono Aaron ,  Christopher Edward LaMaster ,  San-Dar Gau ,  Franco Monteleone ,  Paul Griffin Delvernois ,  Matthew John McKeever ,  Govindarajan Rengarajan ,  Jeremy Peter Latimer ,  Marc Edward Blohm ,  Eric Richard Bonini ,  Venkata Siva Prasad Chaluvadi ,  Jamie Dean Lumpkin ,  Thomas Robbins Tipton

IPC分类号： F01D5/30 ,  F04D29/34 ,  F04D29/32

CPC分类号： F01D5/3038 ,  F04D29/322 ,  F05D2250/74

摘要： An article of manufacture has a first component configured for use with a turbomachine. The first component is configured for attachment to a second component, and reduces the possibility of attachment with an undesired third component by modification of a characteristic of the first component. This modification is matched by a complementary characteristic of the second component. The first component has a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table selected from the group consisting of TABLES 1-11. Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying by a number. X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height. The airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

摘要翻译： 制造品具有配置成与涡轮机一起使用的第一部件。 第一部件被配置为附接到第二部件，并且通过修改第一部件的特性来减少与不需要的第三部件的连接的可能性。 该修改由第二组件的互补特性匹配。 第一部件具有基本上根据从由表1-11组成的组中选择的可缩放表格中阐述的X，Y和Z的笛卡尔坐标值的标称翼型分布。 X，Y和Z的笛卡尔坐标值是通过乘以数字可转换为尺寸距离的无量纲值。 X和Y是当通过连续弧连接时在每个Z高度处限定翼型轮廓部分的坐标。 每个Z高度处的翼型轮廓部分彼此连接以形成完整的翼型形状。