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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

Inactive Publication Date: 2018-12-21
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Through the analysis, it can be known that the above-mentioned nozzles increase the swirl flow channel along the radial or axial direction, although it can improve the uniformity of fuel / air mixing, but the structure is a bit complicated, the flow resistance is large, and there is no specific prevention of spontaneous combustion, tempering and oscillating combustion. measures

Method used

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  • Gas-fuel low-pollution combustion chamber lean premixing swirl nozzle and full-ring combustion chamber
  • Gas-fuel low-pollution combustion chamber lean premixing swirl nozzle and full-ring combustion chamber
  • Gas-fuel low-pollution combustion chamber lean premixing swirl nozzle and full-ring combustion chamber

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specific Embodiment

[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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Abstract

The invention relates to a gas-fuel low-pollution combustion chamber lean premixing swirl nozzle and a full-ring combustion chamber. The gas-fuel low-pollution combustion chamber lean premixing swirlnozzle comprises an axial swirler, a fuel pipeline, fuel injection holes, a premixing section, an outlet convergence section and wall surface diffusion small holes, the plurality of fuel injection holes are located in a fuel boss at the tail end of the fuel pipeline, fuel sprayed by the fuel injection holes and the swirl air are uniformly mixed in the premixing section, the combustion equivalent ratio of the swirl nozzle ranges from 0.55 to 0.75, it is guaranteed that the temperature of a combustion region is relatively low and no local hot spots exist, so that the generation of nitrogen oxideis effectively reduced; a fuel / air mixture is accelerated to flow through the outlet convergence section, so that the backfire risk is reduced; the wall temperature and the boundary layer fuel / air ratio can be reduced through the wall surface diffusion small holes, so that the spontaneous combustion and backfire risks are reduced; in an actual combustion chamber, a multi-point lean premixing combustion chamber head is formed by reasonably arranging a certain number of swirl nozzles with the same size, and the main mold fuel staged supply is adopted so that the low-pollution emission level ofthe combustion chamber in the full working condition range can be realized.

Description

technical field [0001] The invention belongs to the field of gas turbine combustors, and relates to a gas fuel low-pollution combustor lean premix swirl nozzle and a full-ring combustor, in particular to a low-pollution combustor lean premix swirl nozzle solution suitable for gas fuel. Background technique [0002] In recent years, with the frequent occurrence of smog weather all over the country, people have gradually realized that the ecological environment problem has become an important issue affecting the survival of human society. Because the main elements of traditional energy fuels such as coal and petroleum are carbon, oxygen, hydrogen, nitrogen and sulfur, a large amount of harmful gases SOx and NOx will be produced after combustion, and a large amount of unburned particulate matter (PM2. 5, the chief culprit of smog), causing great pollution to the environment, so it is urgent to find clean energy. The main elements of natural gas, shale gas and other gases are c...

Claims

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Application Information

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IPC IPC(8): F23R3/38F23R3/58F23R3/52
CPCF23R3/38F23R3/52F23R3/58
Inventor 索建秦孙付军梁红侠于涵李乐黎明石腾
Owner NORTHWESTERN POLYTECHNICAL UNIV