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Experimental investigation of combustion characteristics in a multi-staging vortex combustor firing rice husk

机译:多级涡流燃烧器燃烧稻壳的燃烧特性实验研究

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The paper described the combustion characteristics in a multi-staging vortex combustor by using rice husk as fuel. Effects of the operating conditions namely: equivalence ratio (Φ=0.8, 1.0 and 1.2) and secondary air ratio (λ=0.0, 0.15 and 0.25) on combustion characteristics (temperature distribution, fly ash and gas emission) were experimentally studied. In the experiments, the conventional vortex combustor consisted of two straight concentric cylindrical pipes, combustion chamber (outer chamber) and exhaust pipe (inner chamber). The variable size of middle section of the combustor was designed to be adjustable from 1.0D (conventional vortex combustor), to 0.75D and 0.5D as desired. The changes of the middle chamber size lead to multi-staging vortex inside the combustor. In the experiments, the rice husk was fed into the combustor at constant mass flow rate of 0.3 kg/min. Test results revealed that the mean temperature distribution for the multi-staging vortex combustor with middle chamber size of 0.5D was higher than those of 0.75D and 1.0D. The experimental results showed the maximum temperature of about 1176 ℃ in the vortex chamber with the middle chamber of 0.5D at equivalence ratio, Φ=0.8 and no secondary air injection, λ=0.0. Measurements of gas emissions from cyclone collector consisted of O_2=2.5%, CO_2= 17.3%, and CO=270 ppm, respectively.
机译:本文以稻壳为燃料,描述了多级涡流燃烧室的燃烧特性。实验研究了当量比(Φ= 0.8、1.0和1.2)和二次空气比(λ= 0.0、0.15和0.25)对燃烧特性(温度分布,飞灰和气体排放)的影响。在实验中,传统的涡流燃烧器由两根同心的直圆柱管组成,即燃烧室(外室)和排气管(内室)。燃烧器中间部分的可变尺寸设计为可根据需要从1.0D(常规涡流燃烧器)调整到0.75D和0.5D。中间腔室尺寸的变化导致燃烧器内部的多级涡旋。在实验中,将稻壳以恒定质量流量0.3 kg / min送入燃烧室。测试结果表明,中间室尺寸为0.5D的多级涡流燃烧室的平均温度分布高于0.75D和1.0D的平均温度分布。实验结果表明,涡流室内的最高温度约为1176℃,中间室为0.5D,当量比Φ= 0.8,无二次空气注入,λ= 0.0。来自旋风分离器的气体排放的测量值分别由O_2 = 2.5%,CO_2 = 17.3%和CO = 270 ppm组成。

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