20250207780. Turbine Engine Having (General Electric)
TURBINE ENGINE HAVING A COMBUSTION SECTION WITH A FUEL NOZZLE ASSEMBLY
Abstract: a turbine engine has a compression 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 combustion section has a fuel nozzle assembly. the fuel nozzle assembly has a compressed air tube, and a body. the body defining a gaseous fuel channel exhausting into the combustion chamber.
Inventor(s): Pradeep Naik, Clayton Stuart Cooper, Sibtosh Pal, Michael T. Bucaro, Michael A. Benjamin, Steven C. Vise, Karthikeyan Sampath, Andrew Joseph Wickersham
CPC Classification: F23R3/286 ({having fuel-air premixing devices ( takes precedence)})
Search for rejections for patent application number 20250207780
- Patent Applications
- General Electric Company
- CPC F23R3/286
- Pradeep Naik of Bengaluru IN
- Clayton Stuart Cooper of Loveland OH US
- Sibtosh Pal of Mason OH US
- Michael T. Bucaro of Arvada CO US
- Michael A. Benjamin of Cincinnati OH US
- Steven C. Vise of Loveland OH US
- Karthikeyan Sampath of Bengaluru IN
- Andrew Joseph Wickersham of Liberty Township OH US