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公开(公告)号:US20180080327A1
公开(公告)日:2018-03-22
申请号:US15272676
申请日:2016-09-22
Applicant: General Electric Company
Inventor: Marc Edward Blohm , Sharan Shanti
IPC: F01D5/14
CPC classification number: F01D5/141 , F04D29/324 , F04D29/544 , F05D2220/32 , F05D2230/90 , 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.
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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.
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