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:
Feb. 19, 2019

Filed:

Oct. 15, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Matthew Lee Krumanaker, Blue Ash, OH (US);

Steven Robert Brassfield, Cincinnati, OH (US);

Robert Frederick Bergholz, Loveland, OH (US);

Aaron Ezekiel Smith, Montgomery, OH (US);

Weston Nolan Dooley, West Chester, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 25/12 (2006.01); F01D 5/14 (2006.01); F01D 9/04 (2006.01); F04D 29/32 (2006.01); F04D 29/54 (2006.01); F04D 29/58 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/147 (2013.01); F01D 5/18 (2013.01); F01D 9/041 (2013.01); F01D 25/12 (2013.01); F04D 29/324 (2013.01); F04D 29/542 (2013.01); F04D 29/582 (2013.01); F05D 2220/32 (2013.01); F05D 2240/303 (2013.01); F05D 2240/305 (2013.01); F05D 2240/306 (2013.01); F05D 2250/185 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01); Y02T 50/676 (2013.01);
Abstract

A turbine engine comprises an airfoil having one or more internal cooling circuits. The cooling circuits can be fed with a flow of cooling fluid from one or more cooling air inlet passages in fluid communication with the cooling circuits. The cooling circuits can provide the cooling fluid flow within the airfoil to cool the airfoil, as well as provide a cooling fluid to a plurality of film holes to create a cooling film on the external surface of the airfoil.


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