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:
Feb. 24, 2026

Filed:

Mar. 14, 2023
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventor:

Dibesh D. Joshi, South Windsor, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F02C 7/24 (2006.01); F02C 7/30 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F02C 7/24 (2013.01); F02C 7/30 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/231 (2013.01); F05D 2260/95 (2013.01);
Abstract

A combustor for a gas turbine engine, including: a heat shield panel attached to a combustor liner, the combustor liner having a plurality of primary apertures extending through the combustor liner and the heat shield panel having a plurality of apertures extending therethrough; an intermediary layer located between the combustor liner and the heat shield panel, the intermediary layer being spaced from the combustor liner and the intermediary layer being spaced from the heat shield panel, the intermediary layer including a plurality of secondary apertures extending through the intermediary layer, the plurality of apertures, the plurality of primary apertures and the plurality of secondary apertures each being in fluid communication with each other; and a plurality of pins extending upwardly and away from a surface of the intermediary layer towards a surface of the combustor liner.


Find Patent Forward Citations

Quick Actions:

Joshi, Dibesh. (2026). Apparatus and method for air particle capture in a gas turbine engine (U.S. Patent No. 12560323). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12560323

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