초록 ▼

An air fuel mixer is disclosed having a mixing duct, a shroud surrounding the upstream end of the mixing duct in which a fuel manifold is provided in flow communication with a fuel supply and control means, a set of inner and outer counter-rotating swirlers adjacent the upstream end of the mixing du

An air fuel mixer is disclosed having a mixing duct, a shroud surrounding the upstream end of the mixing duct in which a fuel manifold is provided in flow communication with a fuel supply and control means, a set of inner and outer counter-rotating swirlers adjacent the upstream end of the mixing duct for imparting swirl to an air stream, a hub separating the inner and outer annular swirlers to allow independent rotation of the air stream, and a centerbody located axially along and substantially the full length of the mixing duct. In order to inject one type of fuel into the mixing duct, fuel is supplied to the outer annular swirlers which include hollow vanes with internal cavities, wherein the internal cavities of the outer swirler vanes are in fluid communication with the fuel manifold in the shroud. The outer swirler vanes further include a plurality of fuel passages therethrough in flow communication with the internal cavities. A second fuel can be injected into the mixing duct by means of a plurality of orifices in the centerbody wall which are in flow communication with a fuel supply and control means. In this way, high pressure air from a compressor is injected into the mixing duct through the swirlers to form an intense shear region and fuel is injected into the mixing duct from the outer swirler vane passages and/or the centerbody orifices so that the high pressure air and the fuel is uniformly mixed therein so as to produce minimal formation of pollutants when a fuel/air mixture is exhausted out the downstream end of the mixing duct into the combustor and ignited.

대표청구항 ▼

An apparatus for premixing fuel and air prior to combustion in a gas turbine engine, comprising; (a) a linear mixing duct having a circular cross section defined by a wall; (b) a shroud surrounding the upstream end of said mixing duct, said shroud having contained therein a fuel manifold in flow com

An apparatus for premixing fuel and air prior to combustion in a gas turbine engine, comprising; (a) a linear mixing duct having a circular cross section defined by a wall; (b) a shroud surrounding the upstream end of said mixing duct, said shroud having contained therein a fuel manifold in flow communication with a fuel supply and control means; (c) a set of inner and outer annular counter-rotating swirlers adjacent the upstream end of said mixing duct for imparting swirl to an air stream, said outer annular swirlers including hollow vanes with internal cavities, wherein the internal cavities of said outer swirler vanes are in fluid communication with said fuel manifold, said outer swirler vanes further including a plurality of fuel passages therethrough in flow communication with said internal cavities to inject fuel into said mixing duct; (d) a hub separating said inner and outer annular swirlers to allow independent rotation of said air stream; and (e) a centerbody defined by a circular wall located axially along and substantially the full length of said mixing duct, said centerbody further comprising: (1) a plurality of orifices in said wall in flow communication with a a fuel supply and control means, wherein said orifices are located immediately downstream of said inner and outer annular swirlers to inject fuel into said mixing duct; (2) a main air passage in flow communication with an air supply; and (3) an air passage surrounding each of said fuel orifices, said air passages being in flow communication with said main air passage, wherein air from said air passages assists atomization of fuel injected through said orifices and directs fuel away from an outer annular surface of said centerbody; wherein high pressure air from a compressor is injected into said mixing duct through said swirlers to form an intense shear region and fuel is injected into said duct from at least one of said centerbody orifices and said outer swirler vane passages so that the high pressure air and the fuel is uniformly mixed therein so as to produce minimal formation of pollutants when the fuel/air mixture is exhausted out the downstream end of said mixing duct into the combustor and ignited.