The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 03, 2022

Filed:

Feb. 11, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Sandip Dutta, Greenville, SC (US);

James Zhang, Greenville, SC (US);

Gary Michael Itzel, Simpsonville, SC (US);

John McConnell Delvaux, Fountain Inn, SC (US);

Matthew Troy Hafner, Honea Path, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); F01D 9/04 (2006.01); F01D 25/00 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
F01D 5/186 (2013.01); F01D 5/147 (2013.01); F01D 5/187 (2013.01); F01D 5/282 (2013.01); F01D 9/041 (2013.01); F01D 25/005 (2013.01); F01D 25/12 (2013.01); F05D 2230/22 (2013.01); F05D 2230/237 (2013.01); F05D 2230/31 (2013.01); F05D 2240/122 (2013.01); F05D 2240/304 (2013.01); F05D 2250/183 (2013.01); F05D 2250/184 (2013.01); F05D 2250/185 (2013.01); F05D 2260/202 (2013.01); F05D 2260/204 (2013.01); F05D 2300/175 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A turbine component includes a root and an airfoil extending from the root to a tip opposite the root. The airfoil forms a leading edge and a trailing edge portion extending to a trailing edge. A plurality of axial cooling channels in the trailing edge portion of the airfoil are arranged to permit axial flow of a cooling fluid from an interior of the turbine component at the trailing edge portion to an exterior of the turbine component at the trailing edge portion. A method of making a turbine component includes forming an airfoil having a trailing edge portion with axial cooling channels. The axial cooling channels are arranged to permit axial flow of a cooling fluid from an interior to an exterior of the turbine component at the trailing edge portion. A method of cooling a turbine component is also disclosed.


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