Patent ID: 9670846
Date: 2017-06-06
CPC Classifications: F02C,F05D,F23D,F23R

Claim:
1. A fuel nozzle for use with a flow of air and a flow of fuel in a gas turbine engine, comprising: a fuel nozzle body; a plurality of elongated mixing tubes positioned within and extending through the fuel nozzle body in an annular array, wherein each of the elongated mixing tubes comprise a fuel inlet and an air inlet, wherein the fuel inlet is positioned downstream from and perpendicular to the air inlet, wherein the flow of fuel and the flow of air mix within the elongated mixing tubes; a turbulated mixing zone comprising alternating areas of greater diameter and lesser diameter extending along an axial length of an inner surface of each the elongated mixing tubes to promote mixing of the flow of air and the flow of fuel; and a constricted tip disposed at an air-fuel outlet of each of the elongated mixing tubes.