Gas turbine preevaporation combustion-chamber for combusting ethanol fuel
A technology of gas turbine and ethanol fuel, which is applied in the direction of combustion chamber, continuous combustion chamber, combustion method, etc., can solve the problem of low boiling point, volatile and high latent heat of evaporation of ethanol fuel, which is not fully applicable, gas turbine combustion chamber cannot be fully used, and pollution emission structure Strength and other issues, to achieve the effect of reducing carbon black smoke and NOx generation, simple nozzle form and structure, and low maintenance costs
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[0031] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0032] A gas turbine pre-evaporation combustor using ethanol fuel described in this embodiment adopts a single-tube cylindrical combustor structure, and is composed of a combustor casing 2 and a flame tube 6; the air flow enters the combustor from the combustor inlet 1 , into the flame tube through the opening on the pre-evaporation tube 4 and the flame tube 6; the liquid ethanol fuel is sprayed into the pre-evaporation tube 4 through the direct injection hole 28 on the ethanol supply path 3, under the action of the primary flow and the secondary swirling flow , the liquid ethanol is evaporated and mixed with air, and the mixed combustible gas enters the flame tube 6 from the outlet of the pre-evaporator tube 4; the ignition of the ethanol combustion chamber is realized by the electric spark igniter 5, and the entire ethanol combustion process...
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