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:
Nov. 18, 2025

Filed:

May. 20, 2024
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventor:

Raymond Surace, Newington, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F02K 1/82 (2006.01); F23R 3/60 (2006.01); F23R 3/06 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F02K 1/822 (2013.01); F23R 3/60 (2013.01); F23R 3/007 (2013.01); F23R 3/06 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/03044 (2013.01);
Abstract

A gas turbine engine combustor panel assembly includes a shell defining an outer periphery of a combustion chamber. The shell has an outer skin with a first plurality of holes and a combustor panel, which includes a first end including a second plurality of holes on an inner face, which extend through the inner face to an outer face and are configured to allow fluid flow from the first plurality of holes to the combustion chamber. The combustor panel further includes a second end comprising a dovetail interface section extending axially from a central axis and from a panel wall of the combustor panel. The assembly further includes a plurality of dovetail tail connectors configured to extend along a central axis and interface with the second end of the combustor panel to connect the combustor panel to the shell.


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