Invention Grant
- Patent Title: Combustion system and method for attenuation of combustion dynamics in a gas turbine engine
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Application No.: US15681875Application Date: 2017-08-21
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Publication No.: US11181274B2Publication Date: 2021-11-23
- Inventor: Allen Michael Danis , Scott Matthew Bush , Arthur Wesley Johnson , Nicholas Ryan Overman , Kent Hamilton Lyle , Eric John Stevens
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Venable LLP
- Agent Jacqueline A. DiRamio; Michele V. Frank
- Main IPC: F23R3/36
- IPC: F23R3/36 ; F02C9/40 ; F23R3/28 ; F02C7/22 ; F02C3/20 ; F02C3/06 ; F02C7/228 ; F23R3/34 ; F02C9/28

Abstract:
The present disclosure is directed to a method of operating a combustion system to attenuate combustion dynamics. The method includes flowing, via a compressor section, an overall supply of air to the combustion system; flowing, via a fuel supply system, an overall flow of fuel to the combustion system; flowing, to a first fuel nozzle of the combustion system, a first supply of fuel defining a richer burning fuel-air mixture at the first fuel nozzle; flowing, to a second fuel nozzle of the combustion system, a second supply of fuel defining a leaner burning fuel-air mixture at the second fuel nozzle; and igniting the richer burning fuel-air mixture and the leaner burning fuel-air mixture to produce an overall fuel-air ratio at a combustion chamber of the combustion system.
Public/Granted literature
- US20190056114A1 COMBUSTION SYSTEM AND METHOD FOR ATTENUATION OF COMBUSTION DYNAMICS IN A GAS TURBINE ENGINE Public/Granted day:2019-02-21
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