-
公开(公告)号：US10415595B2
公开(公告)日：2019-09-17
申请号：US15272546
申请日：2016-09-22
Applicant: General Electric Company
Inventor： Lakshmanan Valliappan , Ramesh Kempanna Babu
Abstract: A system is provided, including an airfoil. The airfoil includes a first suction portion of a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z of a suction side as set forth in TABLE I to a maximum of three decimal places, wherein the X and Y values of the suction side are coordinate values that couple together to define suction side sections of the first suction portion of the nominal airfoil profile at each Z coordinate value, the suction side sections of the first suction portion of the nominal airfoil profile are coupled together to define the first suction portion, the airfoil includes an airfoil length along a Z axis, the first suction portion comprises a first portion length along the Z axis, the first portion length is less than or equal to the airfoil length, and the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances.
-
公开(公告)号：US09546555B2
公开(公告)日：2017-01-17
申请号：US13717265
申请日：2012-12-17
Applicant: General Electric Company
Inventor： Rohit Chouhan , Holly Renae Davis , Lakshmanan Valliappan
CPC classification number: F01D5/225 , F01D5/16 , F05D2260/96 , Y02T50/671 , Y02T50/673
Abstract: A rotatable blade for use in a turbomachine includes an airfoil portion having a leading edge, a trailing edge a radially-inner end and a radially-outer end; a root section at to the radially-inner end of the airfoil portion, and a part-span shroud located on the airfoil portion between the root section and the radially-outer end. The part-span shroud decreases in width and thickness from decreasing in width and thickness from the airfoil portion to a contact surface adapted to engage a mating contact surface on a part-span shroud of an adjacent blade.
Abstract translation: 用于涡轮机的可旋转叶片包括具有前缘的翼型部分，后缘具有径向内端和径向外端; 位于翼型部分的径向内端的根部，以及位于根部与径向外端之间的翼型部分上的部分跨度护罩。 部分跨度的宽度和厚度从宽度和厚度从翼型部分减小到适于接合邻近叶片的部分跨度护罩上的配合接触表面的接触表面。
-
公开(公告)号：US10436214B2
公开(公告)日：2019-10-08
申请号：US15272577
申请日：2016-09-22
Applicant: General Electric Company
Inventor： Lakshmanan Valliappan , Ramesh Kempanna Babu , Sagar Kamble
Abstract: A system is provided, including an airfoil. The airfoil includes a first suction portion of a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z of a suction side as set forth in TABLE I to a maximum of three decimal places, wherein the X and Y values of the suction side are coordinate values that couple together to define suction side sections of the first suction portion of the nominal airfoil profile at each Z coordinate value, the suction side sections of the first suction portion of the nominal airfoil profile are coupled together to define the first suction portion, the airfoil includes an airfoil length along a Z axis, the first suction portion comprises a first portion length along the Z axis, the first portion length is less than or equal to the airfoil length, and the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances.
-
Patent Agency Ranking
公开(公告)号：US20180080474A1
公开(公告)日：2018-03-22
申请号：US15272546
申请日：2016-09-22
Applicant: General Electric Company
Inventor： Lakshmanan Valliappan , Ramesh Kempanna Babu
CPC classification number: F04D29/544 , F02C3/04 , F04D29/324 , F05D2250/74 , Y02T50/673
Abstract: A system is provided, including an airfoil. The airfoil includes a first suction portion of a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z of a suction side as set forth in TABLE I to a maximum of three decimal places, wherein the X and Y values of the suction side are coordinate values that couple together to define suction side sections of the first suction portion of the nominal airfoil profile at each Z coordinate value, the suction side sections of the first suction portion of the nominal airfoil profile are coupled together to define the first suction portion, the airfoil includes an airfoil length along a Z axis, the first suction portion comprises a first portion length along the Z axis, the first portion length is less than or equal to the airfoil length, and the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances.
-
公开(公告)号：US20180080464A1
公开(公告)日：2018-03-22
申请号：US15272577
申请日：2016-09-22
Applicant: General Electric Company
Inventor： Lakshmanan Valliappan , Ramesh Kempanna Babu , Sagar Kamble
CPC classification number: F04D29/384 , F01D5/14 , F04D29/324 , F04D29/544 , F05D2220/32 , F05D2220/3216 , F05D2240/123 , F05D2240/124 , F05D2240/305 , F05D2240/306 , F05D2250/74 , Y02T50/673
Abstract: A system is provided, including an airfoil. The airfoil includes a first suction portion of a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z of a suction side as set forth in TABLE I to a maximum of three decimal places, wherein the X and Y values of the suction side are coordinate values that couple together to define suction side sections of the first suction portion of the nominal airfoil profile at each Z coordinate value, the suction side sections of the first suction portion of the nominal airfoil profile are coupled together to define the first suction portion, the airfoil includes an airfoil length along a Z axis, the first suction portion comprises a first portion length along the Z axis, the first portion length is less than or equal to the airfoil length, and the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances.
-
公开(公告)号：US20150063997A1
公开(公告)日：2015-03-05
申请号：US14013661
申请日：2013-08-29
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Sunil Rajagopal , Moorthi Subramaniyan , Lakshmanan Valliappan
CPC classification number: F01D5/141 , F01D5/145 , F05D2240/122 , F05D2240/304 , F05D2250/184 , Y02T50/673
Abstract: An airfoil includes a radially inner edge extending in a radial direction of the airfoil to a radially outer edge. Also included is a leading edge extending in an axial direction of the airfoil to a trailing edge. Further included is a trailing edge geometry comprising at least one wave segment having simultaneous curvature in at least two directions.
Abstract translation: 翼型件包括沿翼型件的径向方向延伸到径向外边缘的径向内边缘。 还包括沿翼型的轴向方向延伸到后缘的前缘。 还包括后缘几何形状，其包括至少一个在至少两个方向具有同时曲率的波段。
-
公开(公告)号：US09951790B2
公开(公告)日：2018-04-24
申请号：US14845398
申请日：2015-09-04
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Lakshmanan Valliappan , Sharan Shanti , Penchala Kumar Mittadodla
CPC classification number: F04D29/544 , F01D5/141 , F04D29/324 , F05B2240/301 , F05D2240/301 , F05D2250/74
Abstract: 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 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.
-
公开(公告)号：US20170067482A1
公开(公告)日：2017-03-09
申请号：US14845398
申请日：2015-09-04
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Lakshmanan Valliappan , Sharan Shanti , Penchala Kumar Mittadodla
IPC: F04D29/54
CPC classification number: F04D29/544 , F01D5/141 , F04D29/324 , F05B2240/301 , F05D2240/301 , F05D2250/74
Abstract: 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 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.
-
-
-
-
-
-
-
Search Results
8
records
(took 0.025 seconds)
