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Investigation of NO_X Reduction in Fuel-Lean Reburning System with Propane

机译:丙烷贫油再燃系统中NO_X还原的研究

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摘要

In this study, the fuel-lean reburning system is considered for reducing NO emission by using an experimental and numerical approach in conjunction with a lab-scale furnace. Liquefied petroleum gas (LPG) is used as the main and reburn fuel. The goal of this work is to obtain the most optimal combustion system by employing the fuel-lean reburning system to reduce environmental pollution. The amount of reburn fuel and injection location of rebum fuel are considered as experimental parameters. There are very few studies that have focused on how the reburning process is affected by changes in the flow field that are induced by combustion. It is important to study the effect of the combustion condition on the reburning process in order to control fuel-lean reburning. A computational fluid dynamics (CFD) model is used to provide understanding of the complex combustion phenomena. The validation of die predicted results is carefully conducted by comparing the predicted results with the measured data such as species concentration and temperature distribution inside the furnace region. The measured results show that the fuel-lean reburning method leads to 50% NO reduction by using a ratio of reburn fuel to total fuel of 0.13 and by achieving complete combustion without any additional oxidizer. In addition, predicted results indicate that the recirculation flow into the furnace region is carefully considered in order to enhance the reburning efficiency.
机译:在这项研究中,贫油再燃系统被认为是通过结合实验室规模的炉子使用实验和数值方法来减少NO排放的。液化石油气(LPG)用作主要燃料和再燃燃料。这项工作的目的是通过采用贫燃料再燃系统来减少环境污染,从而获得最佳的燃烧系统。再燃燃料的量和再燃燃料的喷射位置被认为是实验参数。很少有研究集中于再燃烧过程如何受到燃烧引起的流场变化的影响。重要的是研究燃烧条件对再燃过程的影响,以控制贫油再燃。计算流体动力学(CFD)模型用于提供对复杂燃烧现象的理解。通过将预测结果与测量数据(例如炉膛区域内的物质浓度和温度分布)进行比较,可以仔细地进行模具预测结果的验证。测量结果表明,通过使用再燃燃料与总燃料的比率为0.13并通过完全燃烧而无需任何其他氧化剂,贫燃料再燃方法可减少50%的NO。此外,预测结果表明,要认真考虑进入炉区的再循环流,以提高再燃效率。

著录项

  • 来源
    《Energy & fuels》 |2011年第maraaapra期|p.905-915|共11页
  • 作者

    Hak Young Kim; Seung Wook Baek;

  • 作者单位

    School of Mechanical, Aerospace and System Engineering, Division of Aerospace Engineering, Korea Advanced Institute of Science and Technology, 373-1 Gusong-Dong, Yusung-Gu, Daejon 305-701, Korea;

    School of Mechanical, Aerospace and System Engineering, Division of Aerospace Engineering, Korea Advanced Institute of Science and Technology, 373-1 Gusong-Dong, Yusung-Gu, Daejon 305-701, Korea;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    S: swirl number; O: van angle; D: nozzle diameter; D_h: van hub diameter; rff: reburn fuel fraction; et al;

    机译:S:旋流数;O:范角;D:喷嘴直径;D_h:轮毂直径;rff:再燃燃料分数;等;

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