A system includes a turbine fuel nozzle assembly (39). The turbine fuel nozzle assembly (39) includes a first fuel nozzle (12, 42, 44) including a first air inlet (62) and a second fuel nozzle (12, 42, 44) including a second air inlet (62). The turbine fue...

The present invention is directed to a staged fuel injector that includes, inter alia , a main fuel circuit for delivering fuel to a main fuel atomizer and a pilot fuel circuit for delivering fuel to a pilot fuel atomizer which is located radially inward o...