稀薄预混涡流燃烧器中沼气燃烧的数值分析

Dániel Füzesi, V. Józsa
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引用次数: 1

摘要

现代燃烧技术以精瘦预混燃烧器为重点,实现高热效率、宽工作范围、低污染物排放的稳态运行。相应的应用范围从锅炉到燃气轮机。本文用CFD方法对30 kW燃烧功率的紊流燃烧器进行了初步分析。参考燃料为天然气,测试了四种沼气,这些沼气被模拟为不同成分的CH4、CO2和H2的混合物。尽管燃烧是稳定的,但由于不稳定流动结构的显著存在,稳定解是不合适的。由于在这种情况下的燃烧是由体积反应主导的,因此可以在壁面附近施加一个粗边界层。然而,剪切主导的流动需要使用至少k-ω的SST湍流粘度模型。采用比例自适应仿真方法计算暂态工况。在燃料中,由于混合管入口中心存在钝体,天然气燃烧表现出闪回现象。然而,其程度较低,在实际燃烧器中加入一些中央吹扫空气将解决这一问题。所有火焰形状均为V形和W形,这意味着燃烧室加载的最佳条件。尽管进口总质量流量随着燃料热值的降低而增加,但天然气燃烧在流场中表现出最高的速度和温度。总的来说,含有CH4-CO2的燃料的少量氢稀释作为一种极好的燃烧稳定剂,没有闪回或太强烈的热释放率。因此,目前所分析的燃烧器可以在低热值燃料上运行,而无需修改设计或在燃烧室上暴露局部高热负荷。由于这是一个初步的研究,验证和实际相关性的评价将在后续的工作中讨论。
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Numerical analysis of biogas combustion in a lean premixed swirl burner
Modern combustion technology focuses on lean premixed burners to achieve high thermal efficiency, wide operating range, and low pollutant emissions for steady-state operation. The corresponding applications range from boilers to gas turbines. The present paper is a preliminary analysis of a turbulent laboratory test burner with 30 kW combustion power by using CFD. The reference fuel was natural gas and four biogases were tested which were modeled as a mixture of CH4, CO2, and H2 in various compositions. Even though the combustion is steady, the steady solution was inappropriate due to the notable presence of unsteady flow structures. Since the combustion in the present case is dominated by volumetric reactions, a coarse boundary layer could be applied near the wall. However, the shear-dominated flow required the use of at least k-ω SST turbulent viscosity model. The transient cases were calculated by using Scale Adaptive Simulation. Among the fuels, natural gas combustion showed flashback due to the bluff body present at the center in the mixing tube inlet. Nevertheless, its extent was low and some central purge air in the real burner will solve this problem. All the flame shapes were V and W, meaning an optimal condition for combustion chamber loading. Even though the overall mass flow rates at the inlet are increasing with the decreasing heating value of the fuel, natural gas combustion showed the highest velocity and temperature in the flow field. Overall, a small hydrogen dilution of the CH4-CO2 containing fuel acted as an excellent combustion stabilizer without flashback or too intense heat release rate. As a consequence, the presently analyzed burner can run on low calorific value fuels without design modifications or exposing locally high thermal load on the combustion chamber. Since it is an initial study, validation and the evaluation of practical relevance will be discussed in subsequent works.
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