多喷嘴燃烧器高温空气中低NOx煤气燃烧模拟

Yaxin Su, Bingtao Zhao
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引用次数: 3

摘要

采用多喷嘴燃烧器对工业炉内的煤气高温空气燃烧进行了数值模拟。炉体为800mm×800mm× 1400mm的矩形腔体。壁中央有一个直径为10mm的圆形燃料射流。5个圆形气流以不同的跨角均匀分布在燃油射流周围。选择基于b函数的概率密度函数(PDF)燃烧模型,结合标准k-e模型模拟燃气燃烧。采用离散坐标法对辐射进行了模拟。采用热NOx模型对NOx排放进行了模拟。本文讨论了燃料射流与空气射流之间的距离对燃烧特性的影响。结果表明,由于射流的相互作用,炉内存在再循环区。烟气的再循环改变了炉内燃料和氧气的局部分布,进而影响了炉内NOx的局部生成。当空气与燃油射流之间的距离增大时,可以有效延缓燃油与空气的混合,在空气与燃油射流之间出现明显的再循环区,降低了局部氧浓度。在低氧区和燃烧区燃烧更多的燃料,火焰体积都增加,使温度分布更加均匀,局部高温得到抑制。当空气和燃料射流之间的无因次距离为2.5时,在含氧量为15%的情况下,NOx的最小排放量为45 ppm
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Modeling of Low NOx Combustion of Coal Gas with High Temperature Air from a Multi-jet Burner
Numerical simulation was carried out on the High Temperature Air Combustion of coal gas in an industrial furnace with a multi-jet burner. The furnace was a rectangular chamber of 800mm×800mm× 1400mm. A circular fuel jet of a diameter of 10mm is at the center of the wall. 5 circular air jets equably distributed around the fuel jet with different straddle angles. A PDF (Probability Density Function) combustion model based on a b function was selected to simulate the gas combustion combined with the standard k-e model. The radiation was simulated by a Discrete Ordinates method. The NOx emission was simulated by thermal NOx model. The effect of the distance between the fuel and air jets on the combustion characteristics was discussed in this paper. The results showed that there was the recirculation zone in the furnace due to the interaction of the jets. The recirculation of the flue-gas changed the local distribution of the fuel and oxygen in the furnace and then influenced the local NOx generation. When the distance between the air and fuel jets increased, the mixing of the fuel and air could be effectively delayed and an obvious recirculation zone appeared between the air jets and fuel jet that reduced the local oxygen concentration. More fuel would be burnt in the low oxygen region and combustion zone and the flame volume were both increased which made the temperature distribution became more equable and local high temperature was suppressed. When the dimensionless distance between the air and fuel jets was 2.5, a minimum NOx emission of 45 ppm was achieved at 15% O2
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