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:
Nov. 12, 2019

Filed:

Jun. 06, 2016
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 9/02 (2006.01); F01D 25/12 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/147 (2013.01); F01D 5/282 (2013.01); F01D 9/02 (2013.01); F01D 25/12 (2013.01); F05D 2220/30 (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 2260/20 (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. Radial cooling channels in the trailing edge portion of the airfoil permit radial flow of a cooling fluid through the trailing edge portion. Each radial cooling channel has a first end at a lower surface at a root edge of the trailing edge portion or at an upper surface at a tip edge of the trailing edge portion and a second end opposite the first end at the lower surface or the upper surface. A method of making a turbine component and a method of cooling a turbine component are also disclosed.


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