Method and apparatus for combustion gas turbine

A PREMIX COMPRESSED AIR AND GAS FUEL 5C 18A IS INTRODUCED AND BURNED IN A HEAD OF BURNING ROOM 13 THE BURNING UNIT 2 OF 3 GAS TURBINE AND HOME BURNING AT A TEMPERATURE OF LOW AND WITH FLAME POOR FLAME IS CARRIED OUT IN A COMBUSTION CHAMBER REAR 15 FOLLOWING THE HEAD OF BURNING ROOM 13, SO AS TO PREVENT THE FORMATION OF A HIGH TEMPERATURE FLAME THAT TREND TO PROMOTE THE FORMATION OF NITROGEN OXIDES .