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. 13, 2023

Filed:

Jul. 30, 2021
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Steven Douglas Johnson, Milford, OH (US);

Jonathan Russell Ratzlaff, Loveland, OH (US);

Craig Alan Gonyou, Blanchester, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/08 (2006.01); F01D 25/12 (2006.01); F01D 9/06 (2006.01); F02C 7/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/085 (2013.01); F01D 9/065 (2013.01); F01D 25/12 (2013.01); F02C 7/185 (2013.01); F05D 2240/35 (2013.01); F05D 2260/213 (2013.01); F05D 2260/2212 (2013.01); F05D 2260/232 (2013.01); F05D 2260/607 (2013.01);
Abstract

A gas turbine engine includes a combustion section, a turbine section, and a compressor section. The combustion section includes a combustor casing, a combustor, a cooling duct, and an outer duct. The combustor casing defines at least in part a diffuser cavity and a fluid inlet. The combustor disposed is in the diffuser cavity. The cooling duct is in fluid communication with the fluid inlet in the combustor casing and is configured to transport a flow of cooled air. The outer duct surrounds at least a portion of the cooling duct and extends along a portion of an entire length of the cooling duct. The outer duct defines a gap with the cooling duct and is configured to transport a flow of buffer air. The turbine section is disposed downstream from the combustion section. The cooling duct is in fluid communication with the turbine section.


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