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:
Jun. 23, 2020

Filed:

May. 27, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Curtis Walton Stover, West Chester, OH (US);

Jonathan Michael Rausch, West Chester, OH (US);

Satoshi Atsuchi, Rexford, NY (US);

Gulcharan Singh Brainch, West Chester, OH (US);

Robert David Briggs, West Chester, OH (US);

Ronald Scott Bunker, Placitas, NM (US);

Ambarish Jayant Kulkarni, Niskayuna, NY (US);

Michael Alan Meade, West Chester, OH (US);

Byron Andrew Pritchard, Cincinnati, OH (US);

Robert Proctor, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F01D 11/08 (2006.01); F01D 25/12 (2006.01); F01D 9/04 (2006.01); F01D 5/18 (2006.01); F23R 3/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F01D 5/189 (2013.01); F01D 9/041 (2013.01); F01D 11/08 (2013.01); F01D 25/12 (2013.01); F23R 3/002 (2013.01); F23R 3/005 (2013.01); F05D 2240/81 (2013.01); F05D 2250/38 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01); F05D 2260/22141 (2013.01); F05D 2260/607 (2013.01); F23R 2900/03042 (2013.01); F23R 2900/03043 (2013.01); F23R 2900/03044 (2013.01); F23R 2900/03045 (2013.01); Y02T 50/673 (2013.01); Y02T 50/676 (2013.01);
Abstract

Gas turbine engine components are provided which utilize an insert to provide cooling air along a cooled surface of an engine component. The insert provides cooling holes or apertures which face the cool side surface of the engine component and direct cooling air onto that cool side surface. The apertures may be formed in arrays and directed at an oblique or a non-orthogonal angle to the surface of the insert and may be at an angle to the surface of the engine component being cooled. An engine component assembly is provided with counterflow impingement cooling, comprising an engine component cooling surface having a cooling fluid flow path on one side and a second component adjacent to the first component. The second component may have a plurality of openings forming an array wherein the openings extend through the second component at a non-orthogonal angle to the surface of the second component.


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