18469174. GAS TURBINE ENGINE AND FUEL NOZZLE THEREFOR (General Electric Company)
GAS TURBINE ENGINE AND FUEL NOZZLE THEREFOR
Organization Name
Inventor(s)
Michael T. Bucaro of Arvada CO US
GAS TURBINE ENGINE AND FUEL NOZZLE THEREFOR
This abstract first appeared for US patent application 18469174 titled 'GAS TURBINE ENGINE AND FUEL NOZZLE THEREFOR
Original Abstract Submitted
A gas turbine engine comprising a combustion section enshrouded by a casing having at least one through passage, the combustion section comprising a dome wall and a liner at least partially defining a combustion chamber; a fuel nozzle connected to the dome wall and having a nozzle tube; and a coupling securing the fuel nozzle with casing and disposed at least partially in the at least one through passage.