COMBUSTOR NOZZLE

A combustor nozzle (1220) comprising a plurality of nozzle modules (1400) is proposed. The nozzle module (1400) comprises a fuel supply pipe (1410) having an internal fuel flow path through which fuel flows from the front side to the rear side, a plurality of manifolds (1430) communicating with the fuel supply pipe (1410) and arranged in a row in a radial direction so that air inlet flow paths (1440) are respectively formed at positions therebetween, and a plurality of fuel mixers (1450) disposed along a circumferential direction at the rear side of the manifold (1430) to receive the fuel from the manifold (1430) and inject the fuel. Each of the plurality of fuel mixers (1450) comprises a mixer body (1451) having one end communicating with the manifold (1430), wherein a tip (1452) is formed at the other end of the mixer body (1451), a shroud (1460) disposed to surround an outer circumferential surface of the mixer body (1451) to guide an airflow, and at least one fuel port (1454, 1455) formed through the mixer body (1451) to inject fuel.