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1. 发明授权

US09017019B2 Airfoil shape for a compressor 有权
标题翻译：压缩机的翼型
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。

2. 发明申请

US20130336777A1 AIRFOIL SHAPE FOR A COMPRESSOR 有权
标题翻译：压缩机气翼形状
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。

3. 发明申请

US20100068050A1 GAS TURBINE VANE ATTACHMENT 审中-公开
标题翻译：燃气涡轮增压器附件
公开(公告)号：US20100068050A1
公开(公告)日：2010-03-18
申请号：US12209314
申请日：2008-09-12
申请人： Christian Michael Hansen , Roger Claude Beharrysingh
发明人： Christian Michael Hansen , Roger Claude Beharrysingh
IPC分类号： F01D9/04
CPC分类号： F01D25/246 , F01D9/042
摘要： Base hooks of a vane includes an approximate two times thicker radial geometry, with dimensioning and tolerancing that results in a line-line to loose fit on the forward OD hook surface and the aft ID hook surface. Tolerances thus stack up on the opposite, non-critical surfaces of the hooks (the forward ID hook surface and the aft OD hook surface). The base of the vane is curved to match that of the casing. An interface between the vane base and the casing groove includes a metal alloy liner. Also, a wear coating is provided on the vane attachment hooks. The liner protects the casing groove from wear damage, while the hook coating and the liner provide a wear coupling between the vane base and the casing that provides a barrier between the vane bases and the casing to decrease the wear rate.
摘要翻译：叶片的基座钩包括近似两倍的径向几何形状，具有尺寸和公差，导致线前端松动地配合在前面的OD钩表面和后部ID钩表面上。因此，公差因此堆叠在钩的相对的非关键表面上（前ID钩表面和后OD钩表面）。叶片的底部弯曲以匹配套管的底部。叶片基座和壳体槽之间的界面包括金属合金衬套。此外，在叶片附接钩上设置耐磨涂层。衬套保护套管槽不受磨损损伤，而钩涂层和衬套在叶片底座和壳体之间提供了一个磨损联接，在叶片底座和壳体之间提供了一个阻挡层，以降低磨损率。

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