dual fuel gas turbine burner (DUAL FUEL GAS TURBINE COMBUSTOR)

摘要

the gas turbine burner (4) in the first combustion zone (36) and a second combustion zone (37). the burner is in a dual fuel nozzle (18) to complete, the nozzle (18) is a liquid or gas fuel in the fuel mixture to the combustion region due to i can supply. the combustion of gas fuel and the mixture is mixed in the thin section of the channels (90, 92) of the first combustion zone through the year in order to supply the gas fuel spray pin (62) and the gas or liquid fuel in the mixture and the mixture of little change in the channel (6) to the second station. the area (37) for supply to a fuel spray bar and 2 - (76). dual fuel spray bar (67). the mechanics of the construction, gas and liquid fuel to the fuel spray distribution in the set path (95, 96).the gas fuel discharge ports (78) in a spray bar's surface to form rows. the liquid fuel discharge port (84) spray bar with the a's in the spray nozzle 10 of the heat of formation.