Patent ID: 6334309
Filing Date: 2002-01-01
Classification: F23D,F23R

Abstract:
Liquid fuel injector for burners in gas turbines, of the type used inside burners which are provided with a pre-mixing chamber (62) and an element (13) to create turbulence in the flow of compressed air obtained from the compressor of the said gas turbine, the said injector (10) comprising a body (11) which ends in a tip (12) and is provided with at least one duct (25) for passage of the fuel, and ducts (48, 58) for the inflow of compressed air from the said turbine, wherein the said duct (25) for the fuel and the said ducts (48, 58) for the compressed air end in respective outlet holes (20, 21, 22, 23), characterised in that the tip (12) of the said injector (10) ends at the median part of the converging portion (61) of the said pre-mixing chamber (62).