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:
Aug. 24, 2021

Filed:

Jan. 07, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Dennis M. Moura, South Windsor, CT (US);

Carey Clum, East Hartford, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/06 (2006.01); F02C 7/30 (2006.01); F01D 25/12 (2006.01); F23R 3/00 (2006.01); F23R 3/50 (2006.01); F01D 25/32 (2006.01); F02C 7/18 (2006.01);
U.S. Cl.
CPC ...
F02C 7/30 (2013.01); F01D 25/12 (2013.01); F01D 25/32 (2013.01); F02C 7/18 (2013.01); F23R 3/002 (2013.01); F23R 3/005 (2013.01); F23R 3/06 (2013.01); F23R 3/50 (2013.01); F05D 2220/32 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01); F05D 2260/221 (2013.01); F05D 2260/607 (2013.01); F23R 2900/00004 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03044 (2013.01);
Abstract

A gas turbine engine component assembly is provided. The gas turbine engine component assembly comprising: a first component having a first surface and a second surface opposite the first surface wherein the first component includes a cooling hole extending from the second surface to the first surface through the first component; a second component having a first surface and a second surface, the first surface of the first component and the second surface of the second component defining a cooling channel therebetween in fluid communication with the cooling hole for cooling the second surface of the second component; and a deflector forming a passageway with the second surface of the first component, the passageway configured to direct airflow into the cooling channel in a lateral direction parallel to the second surface of the second component such that a cross flow is generated in the cooling channel.


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