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:
Jul. 05, 2022

Filed:

Mar. 06, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Shawn J. Gregg, Wethersfield, CT (US);

Dominic J. Mongillo, West Hartford, CT (US);

Michael Leslie Clyde Papple, Longueuil, CA;

Russell J. Bergman, Windsor, CT (US);

Mohammed Ennacer, St. Hubert, CA;

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 9/04 (2006.01); F01D 25/12 (2006.01); F02C 7/12 (2006.01); F04D 29/32 (2006.01); F04D 29/54 (2006.01); F04D 29/58 (2006.01);
U.S. Cl.
CPC ...
F01D 5/188 (2013.01); F01D 5/187 (2013.01); F01D 5/189 (2013.01); F01D 9/041 (2013.01); F01D 25/12 (2013.01); F02C 7/12 (2013.01); F04D 29/324 (2013.01); F04D 29/542 (2013.01); F04D 29/582 (2013.01); F05D 2220/32 (2013.01); F05D 2240/126 (2013.01); F05D 2240/30 (2013.01); F05D 2260/201 (2013.01); F05D 2260/2212 (2013.01); F05D 2260/22141 (2013.01); Y02T 50/60 (2013.01);
Abstract

A component for a gas turbine engine includes, among other things, an airfoil that extends between a leading edge and a trailing edge and a cooling circuit disposed inside of the airfoil. The cooling circuit includes at least one core cavity that extends inside of the airfoil, a baffle received within the at least one core cavity, a plurality of pedestals positioned adjacent to the at least one core cavity and a first plurality of axial ribs positioned between the plurality of pedestals and the trailing edge of the airfoil.


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