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. 11, 2024

Filed:

Mar. 21, 2023
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Perumallu Vukanti, Bengaluru, IN;

Sibtosh Pal, Mason, OH (US);

Pradeep Naik, Bengaluru, IN;

R Narasimha Chiranthan, Bengaluru, IN;

Ajoy Patra, Bengaluru, IN;

Michael T. Bucaro, Arvada, CO (US);

Aritra Chakraborty, Bengaluru, IN;

Arijit Sinha Roy, Bengaluru, IN;

Pabitra Badhuk, Bengaluru, IN;

Bhavya Naidu Panduri, Bengaluru, IN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/06 (2006.01);
U.S. Cl.
CPC ...
F23R 3/06 (2013.01);
Abstract

A gas turbine engine includes a compressor section, a combustor section, and a turbine section in fore-to-aft serial flow arrangement and defines an engine centerline. The combustor section includes a combustor liner at least partially defining a combustor chamber and a dome wall, coupled to the combustor liner, and defining a forward end of the combustion chamber. A first fuel nozzle is located on the dome wall and fluidly coupled to the combustion chamber. A first set of compressed air openings emit compressed air into the combustion chamber along a first flow path and a second set of compressed air openings emit compressed air into the combustion chamber along a second flow path. The first and second flow paths intersect at an intersection point to form a sheet of air.


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