20250189132. Turbine Engine Having (General Electric)
TURBINE ENGINE HAVING A COMBUSTION SECTION WITH A FUEL NOZZLE
Abstract: a turbine engine has a compressor section, a combustion section, and a turbine section in serial flow arrangement. the combustion section has a combustion liner and dome wall collectively forming at least a portion of a combustion chamber. the dome wall has a fuel nozzle opening. the combustion section has a fuel nozzle assembly extending through the fuel nozzle opening. the fuel nozzle assembly has a gaseous fuel supply, a compressed air supply, a mixer, a fuel nozzle and a first swirler.
Inventor(s): Pradeep Naik, Clayton Stuart Cooper, Steven C. Vise, Michael A. Benjamin, Michael T. Bucaro, Sibtosh Pal, Andrew Joseph Wickersham, Karthikeyan Sampath
CPC Classification: F23R3/286 ({having fuel-air premixing devices ( takes precedence)})
Search for rejections for patent application number 20250189132
- Patent Applications
- General Electric Company
- CPC F23R3/286
- Pradeep Naik of Bengaluru IN
- Clayton Stuart Cooper of Loveland OH US
- Steven C. Vise of Loveland OH US
- Michael A. Benjamin of Cincinnati OH US
- Michael T. Bucaro of Arvada CO US
- Sibtosh Pal of Mason OH US
- Andrew Joseph Wickersham of Liberty Township OH US
- Karthikeyan Sampath of Bengaluru IN