FIELD: gas burning equipment. SUBSTANCE: invention is related to liquid-fuel injector 10 designed for burners of type used inside burners in gas turbines provided with premixing chamber and element 13 to form turbulence in compressed air flow generated by compressor of gas turbine. Injector 10 has body 11 terminating in tip 12 that has at least one conduit for passage of fuel and conduits of compressed air supplied by compressor of gas turbine. Fuel conduit and compressed air conduits end in proper outlet holes. Tip 12 of injector 10 terminates in middle of narrowing part 61 of premixing chamber 62. EFFECT: simplified design and raised operational reliability of injector. 15 cl, 4 dwg
