TURBINE ENGINE FUEL NOZZLES

摘要

A fuel nozzle (100) for a turbine engine (10) is provided. The fuel nozzle includes a one-piece housing (124) coupled to a one-piece venture (128). The housing includes an annular fuel nozzle tip and a plurality of openings configured to discharge air radially outward from the fuel nozzle tip. The venturi is coupled to the housing and defines a fuel chamber within the fuel nozzle tip. A one-piece swirler (136) is coupled to and extends radially inward from the venturi. The swirler facilitates enhancing mixing of the fuel and air within the fuel chamber.