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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
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.
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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
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。
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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
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。
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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.
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公开(公告)号：US20130336778A1
公开(公告)日：2013-12-19
申请号：US13526893
申请日：2012-06-19
申请人： Michael James Dutka , Pinak Pani Gogoi , Christopher Edward LaMaster , Venkata Siva Prasad Chaluvadi , Pradeep Mahadevappa
发明人： Michael James Dutka , Pinak Pani Gogoi , Christopher Edward LaMaster , Venkata Siva Prasad Chaluvadi , Pradeep Mahadevappa
IPC分类号： F04D29/44
CPC分类号： F04D29/563 , F04D29/544
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 1-2, 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： 具有基本上根据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，该可缩放表从由表1-2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。
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公开(公告)号：US08926287B2
公开(公告)日：2015-01-06
申请号：US13526893
申请日：2012-06-19
申请人： Michael James Dutka , Pinak Pani Gogoi , Christopher Edward LaMaster , Venkata Siva Prasad Chaluvadi , Pradeep Mahadevappa
发明人： Michael James Dutka , Pinak Pani Gogoi , Christopher Edward LaMaster , Venkata Siva Prasad Chaluvadi , Pradeep Mahadevappa
IPC分类号： F01D5/14
CPC分类号： F04D29/563 , F04D29/544
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 1-2, 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： 具有基本上根据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，该可缩放表从由表1-2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。
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公开(公告)号：US08714908B2
公开(公告)日：2014-05-06
申请号：US12940341
申请日：2010-11-05
IPC分类号： F04D29/58
CPC分类号： F01D11/001 , F04D29/164 , F04D29/563
摘要： A method and system for improving performance of a compressor section of a gas turbine by diverting leakage air flowing from high pressure downstream of a stator vane assembly to low pressure upstream of the stator vane assembly from disrupting design flow patterns at a leading edge of stator vanes. A cover is provided at a forward face of an inner shroud assembly to prevent the leakage air from impinging on the leading edge. The cover may be provided at an outlet channel of a flow diverter mounted on the forward face of the inner shroud assembly.
摘要翻译： 一种用于通过将定子叶片组件的下游从高压流出的泄漏空气从定子叶片组件的上游转向低压的方式改进燃气轮机的压缩机部分的性能的方法和系统，从而破坏定子叶片的前缘处的设计流动模式 。 在内护罩组件的前表面处设置盖，以防止泄漏空气撞击前缘。 盖可以设置在安装在内护罩组件的前表面上的分流器的出口通道处。
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