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:
Aug. 11, 2026
Filed:
Jan. 21, 2025
General Electric Company, Evendale, OH (US);
Karthikeyan Sampath, Bengaluru, IN;
Maximilian Zahn, Munich, DE;
Pradeep Naik, Bengaluru, IN;
Prithiviraaj Pet T, Madurai, IN;
Pabitra Badhuk, Jhargram, IN;
Sibtosh Pal, Mason, OH (US);
Michael T. Bucaro, Arvada, CO (US);
Steven C. Vise, Loveland, OH (US);
Steven Marakovits, Mason, OH (US);
General Electric Company, Evendale, OH (US);
Abstract
A turbine engine comprising: a compressor section, a combustion section, and a turbine section in serial flow arrangement, with the combustion section comprising a combustion chamber and a fuel nozzle assembly fluidly coupled with the combustion chamber at a fuel nozzle assembly outlet, wherein the fuel nozzle assembly comprises a gaseous fuel passage defined by an inner surface of a centerbody, a plurality of annularly shaped air supply passages circumscribing the centerbody including at least a first air supply passage and a second air supply passage circumscribing the first air supply passage, at least one splitter having an annular shape circumscribing the centerbody and separating adjacent air supply passages of the plurality of air supply passages, a fuel nozzle body circumscribing the plurality of air supply passages and the at least one splitter and at least one orifice plate disposed within one of the plurality of the air supply passages.