A combined premixer for gas turbine
A gas turbine, combined technology, applied in the direction of combustion chamber, combustion method, combustion equipment, etc., can solve the problems of unstable combustion of full premixed combustion, unstable combustion of premixed nozzles, easy tempering, etc., and achieve the benefit of gas dispersion The effect of mixing, design difficulty and production difficulty is low, and stability is improved
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Embodiment 1
[0036] Such as Figure 1-4 As shown, this embodiment designs a combined premixer for gas turbines, the purpose of which is to avoid the problems of easy tempering and flameout in the starting state of the premixer by increasing diffusion combustion. The combined premixer in this embodiment includes components such as a premixing nozzle and a connecting body 3 .
[0037] The premix nozzle is connected to a connection body 3 for fixing the premix nozzle to the combustor head of the gas turbine.
[0038] The premixing nozzle includes an outer casing 13, swirl vanes 11 and a central cone 12; a premixing channel is arranged in the outer casing 13, and the central cone 12 is arranged at the center of the premixing channel; the premixing channel is used for gas Pre-mixing with air; a plurality of swirl blades 11 for air swirl are arranged between the central cone 12 and the outer shell 13, and an air inlet 133 is arranged on the air intake side of the pre-mixing channel, and the pre...
Embodiment 2
[0042] Such as Figure 1-4 As shown, this embodiment designs a combined premixer for gas turbines. The purpose is to use the combination of premixing nozzles to solve the problems of difficult installation and maintenance, production and design of existing premixers. The combined premixer in this embodiment can be combined on the structure in Example 1, and can also be a combination of a new structure.
[0043] The combined premixer in this embodiment includes components such as a premixing nozzle and a connecting body 3 .
[0044] A plurality of premixing nozzles are connected side by side on the connecting body 3, and the connecting body 3 is used to fix each premixing nozzle to the head of the combustion chamber of the gas turbine.
[0045] The premixing nozzle includes an outer casing 13, swirl vanes 11 and a central cone 12; a premixing passage is provided in the outer casing 13, and the central cone 12 is arranged at the center of the premixing passage; the premixing pa...
Embodiment 3
[0049] Such as Figure 1-4 As shown, this embodiment designs a combined premixer for gas turbines, the purpose of which is to use the way of spraying gas from the position of the swirl blade 11 of the gas small hole 43 to improve the mixing degree of the premixed gas. In this embodiment The combined type premixer in can be combined on the structure in embodiment 1 or 2, also can be to adopt new structure.
[0050] The combined premixer in this embodiment includes components such as a premixing nozzle and a connecting body 3 .
[0051] A plurality of premixing nozzles are connected side by side on the connecting body 3, and the connecting body 3 is used to fix each premixing nozzle to the head of the combustion chamber of the gas turbine.
[0052] The premixing nozzle includes an outer casing 13, swirl vanes 11 and a central cone 12; a premixing passage is provided in the outer casing 13, and the central cone 12 is arranged at the center of the premixing passage; the premixing...
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