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.
Patent No.:
Date of Patent:
Feb. 04, 2025
Filed:
Aug. 21, 2023
Gas turbine combustor fuel nozzle assembly and combustor liner having dilution holes in arrangements
Applicant:
General Electric Company, Schenectady, NY (US);
Inventors:
Nayan Vinod Patel, Liberty Township, OH (US);
Michael A. Benjamin, Cincinnati, OH (US);
Assignee:
General Electric Company, Evendale, OH (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/06 (2006.01); F23R 3/14 (2006.01); F23R 3/34 (2006.01); F23R 3/36 (2006.01); F02C 7/22 (2006.01); F23R 3/28 (2006.01);
U.S. Cl.
CPC ...
F23R 3/34 (2013.01); F23R 3/06 (2013.01); F23R 3/14 (2013.01); F23R 3/36 (2013.01); F02C 7/22 (2013.01); F23R 3/28 (2013.01); F23R 3/346 (2013.01);
Abstract
A turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. A combustor in the combustion section can include a combustion chamber, a fuel supply fluidly coupled to the combustion chamber, and a fuel nozzle assembly. The fuel nozzle assembly can include an air flow passage and a fuel flow passage.