Turbine engine fuel nozzles and methods of assembling the same

摘要

A method for assembling a fuel nozzle for a turbine engine is provided. The method includes coupling a one-piece housing to a one-piece venturi wherein the housing defines an annular fuel nozzle tip and the venturi defines a fuel chamber within the fuel nozzle tip. The method further includes coupling a one-piece swirler to the venturi such that the swirler extends radially inward from the venturi.