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:
Oct. 06, 2026

Filed:

Jul. 07, 2025
Applicant:

General Electric Company, Evendale, OH (US);

Inventors:

Gerardo Antonio Salazar Lois, West Chester, OH (US);

Steven Marakovits, Mason, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23R 3/60 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F23R 3/007 (2013.01); F23R 3/60 (2013.01); F23R 2900/03044 (2013.01);
Abstract

A gas turbine engine generally defines an axial direction and includes a combustor assembly. The combustor assembly includes a plurality of liner tiles defining at least part of a combustion chamber that extends between a forward end and an aft end generally along the axial direction. A combustor liner support assembly is positioned on a cold side of the plurality of liner tiles and defines a rail extending radially toward the combustion chamber. A retainer assembly includes a bushing where at least one liner tile of the plurality of liner tiles is floatably coupled to the rail via the bushing.


Find Patent Forward Citations

Salazar Lois, Gerardo. (2026). Combustor assembly for a gas turbine engine (U.S. Patent No. 12753921). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12753921

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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