초록 ▼

A gas turbine engine (12) including a water injection system (56) for providing a flow of water (60) to only a pilot diffusion combustion zone (20) of a dual-mode combustor (10) and not to a pre-mixed combustion zone (18) of the combustor. The selective reduction of peak flame temperature in the pil

A gas turbine engine (12) including a water injection system (56) for providing a flow of water (60) to only a pilot diffusion combustion zone (20) of a dual-mode combustor (10) and not to a pre-mixed combustion zone (18) of the combustor. The selective reduction of peak flame temperature in the pilot flame zone provides a maximum reduction in the production of oxides of nitrogen with a minimum consumption of water. The pilot fuel fraction of the combustor may be increased prior to the initiation of the pilot water injection flow. The flow rate of the pilot injection water may be varied as a function of the power level of the gas turbine, and further as a function of the humidity of the ambient air (36).

대표청구항 ▼

1. A gas turbine engine having a dual-mode combustor comprising: a pre-mixed combustion zone disposed downstream of a first fuel delivery element; a diffusion combustion zone disposed downstream of a second fuel delivery element; a water injection apparatus for selectively injecting water into

1. A gas turbine engine having a dual-mode combustor comprising: a pre-mixed combustion zone disposed downstream of a first fuel delivery element; a diffusion combustion zone disposed downstream of a second fuel delivery element; a water injection apparatus for selectively injecting water into only the diffusion combustion zone and not the pre-mixed combustion zone for controlling combustion temperature in the diffusion flame zone; a fuel system for supplying fuel through said fuel delivery elements to said pre-mixed combustion zone and said diffusion combustion zone, a pilot fuel fraction being a ratio of a fuel flow rate provided to the pilot diffusion combustion zone divided by a sum of the fuel flow rate provided to the pilot diffusion combustion zone plus a fuel flow rate provided to the pre-mixed combustion zone; and a controller operatively connected to the fuel system and comprising logic for increasing the pilot fuel fraction prior to initiating the operation of the water injection apparatus to selectively inject water into only the diffusion combustion zone. 2. The gas turbine engine of claim 1, further comprising: a pilot fuel nozzle disposed in the dual-mode combustor for providing a flow of fuel to the diffusion combustion zone; and the water injection apparatus comprising a water conduit connected to the pilot fuel nozzle for selectively delivering a flow of water to the diffusion combustion zone and not the pre-mixed combustion zone. 3. The gas turbine engine of claim 1, further comprising a sensor for providing a signal responsive to a level of humidity in ambient air provided to the gas turbine engine, the water injection apparatus being responsive to the signal to control a flow rate of the water injected into only the diffusion combustion zone as a function of the level of humidity. 4. A method for controlling combustion of a fuel in a gas turbine engine having a pre-mixed zone of combustion downstream of a first fuel delivery element and a pilot diffusion zone of combustion downstream of a second fuel delivery element, the method comprising selectively injecting a fluid other than the fuel into only the pilot diffusion combustion zone and not the pre-mixed combustion zone, the fluid being injected into the pilot diffusion combustion zone only when the gas turbine engine is operating above a predetermined power level. 5. A method for controlling combustion of a fuel in a gas turbine engine having a pre-mixed zone of combustion downstream of a first fuel delivery element and a pilot diffusion zone of combustion downstream of a second fuel delivery element, the method comprising selectively injecting a fluid other than the fuel into only the pilot diffusion combustion zone and not the pre-mixed combustion zone, the fluid being injected into the pilot diffusion combustion zone only when the gas turbine engine is operating at a steady-state power level and not in a power transient condition. 6. A method for controlling combustion of a fuel in a gas turbine engine having a pre-mixed zone of combustion downstream of a first fuel delivery element and a pilot diffusion zone of combustion downstream of a second fuel delivery element, the method comprising selectively injecting a fluid other than the fuel into only the pilot diffusion combustion zone and not the pre-mixed combustion zone, and increasing a pilot fuel fraction of the combustor by a predetermined increment above a baseline value prior to initiating the selective injection of fluid into only the pilot diffusion combustion zone. 7. The method of claim 6, further comprising calculating the predetermined increment as a function of an operating power level of the combustor.