Gas-fuel low-pollution combustion chamber lean premixing swirl nozzle and full-ring combustion chamber
A swirl nozzle and gas fuel technology, applied in combustion chambers, continuous combustion chambers, combustion methods, etc., can solve problems such as complex structures and large flow resistance, and achieve reduced NOx emissions, improved mixing uniformity, and low pollution emission levels Effect
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[0039] Such as Figure 1-3 As shown, the embodiment of the present invention provides a lean premixed swirl nozzle structure suitable for low-pollution combustors of gas fuel gas turbines, including an axial swirler 4, a swirler outer wall 2, a swirler inner wall 6, fuel Pipeline 7, fuel boss 9, fuel injection hole 8, swirl flow channel 5, premixing section 10, exit converging section 11, wall surface divergence small hole 3 and swirl nozzle outlet 12. The swirl channel 5 is surrounded by an axial swirler 4, an inner wall 6 of the swirler and an outer wall 2 of the swirler. The blades of the axial swirler 4 are curved blades, and the number of blades is 6-20. The blade angle is 30°-60°. The premixing section 10 is located between the swirl channel 5 and the outlet converging section 11, the ratio of the length L of the premixing section to the diameter D of the nozzle is 0.7-1.2, and the diameter D of the nozzle is 25mm-40mm. The fuel pipeline 7 is located inside the inner w...
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