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:
Mar. 19, 2019

Filed:

Oct. 26, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Zachary John Snider, Simpsonville, SC (US);

Gregory Thomas Foster, Greer, SC (US);

Joseph Anthony Weber, Simpsonville, SC (US);

James Fredric Wiedenhoefer, Clifton Park, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/06 (2006.01); F01D 5/18 (2006.01); F01D 25/08 (2006.01); F01D 5/14 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F01D 9/065 (2013.01); F01D 5/147 (2013.01); F01D 5/186 (2013.01); F01D 5/187 (2013.01); F01D 9/041 (2013.01); F01D 9/06 (2013.01); F01D 25/08 (2013.01); F05D 2220/32 (2013.01); F05D 2240/122 (2013.01); F05D 2240/123 (2013.01); F05D 2240/124 (2013.01); F05D 2240/305 (2013.01); F05D 2240/306 (2013.01); F05D 2260/202 (2013.01); F05D 2260/204 (2013.01);
Abstract

A turbine airfoil for a rotating blade or stationary nozzle vane includes an airfoil body including a leading edge and a trailing edge. A coolant supply passage extends within the airfoil body, and a coolant return passage extends within the airfoil body. A first trench is in an external surface of the airfoil body, the first trench extending to the trailing edge and being in fluid communication with the coolant supply passage. A second trench is in the external surface of the airfoil body, the second trench extending to the trailing edge and being in fluid communication with the coolant return passage and the first trench. A cover seats in the airfoil body and encloses the trenches to form coolant passages with the airfoil body. In embodiments, two coolant passages to and back from the trailing edge may be used to allow for a recycling flow.


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