Gas turbine low-emission combustion chamber using gas fuels
A gas fuel, gas turbine technology, applied in the direction of combustion chamber, continuous combustion chamber, combustion method, etc., can solve the problems of lack of adaptability of gas fuel, engine combustion chamber damage, prone to spontaneous combustion and backfire, etc., to achieve stable combustion and prevent Good effect of tempering and mixing
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Embodiment 1
[0033] Such as Figure 1-Figure 4 As shown, a gas turbine low-emission combustor using gas fuel, the head of the combustor includes a duty stage and a main combustion stage arranged in a concentric manner, and the duty stage is in the center, and the main combustion stage is arranged on the periphery of the duty stage. Adjust the duty stage, the fuel distribution of the main combustion stage and the coordination between different nozzles to achieve combustion stability and low emissions when using gaseous fuels. The duty stage includes a primary axial swirler 6 and a duty stage fuel nozzle , the primary axial swirler 6 is installed in the center hole of the head of the flame tube 12, the outer casing 14 of the flame tube is installed outside the flame tube 12, and the flame tube 12 and the outer casing 14 of the flame tube are arranged coaxially, The flame tube outer casing 14 is respectively provided with a fuel tank 24 of the No. 1 duty level and a No. 2 duty level fuel tank...
Embodiment 2
[0039] Such as Figure 5 with Image 6 As shown, the outer casing 14 of the flame tube is located at the outer ring part of the high-pressure igniter 7 and is provided with a No. The included angle between the axis of the nozzle 3 and the axial direction of the primary axial swirler 6 is 60°. Other structures and connection methods are the same as in Embodiment 1.
Embodiment 3
[0041] The installation angle between the centerline of the flame tube 12 and the engine centerline is 30°. Other structures and connection methods are the same as those in Embodiment 1 or Embodiment 2.
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