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Optimization of combustion chamber geometry for natural gas engines with diesel micro-pilot-induced ignition

机译:柴油微飞行员诱导点火的天然气发动机燃烧室几何形状的优化

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摘要

Smokeless, low nitrogen oxides (NOx), and high thermal efficiency have been achieved through the lean-burn concept for natural gas engine with diesel micro-pilot-induced ignition (MPII). However, the combustion chamber is usually not specialized for natural gas combustion, and increases in the unburned hydrocarbon (HC) and carbon monoxide (CO) emissions are still a challenge for this type of engines. This paper describes optimization of the combustion chamber geometry to reduce the HC and CO emissions and improve the combustion efficiency in the MPII natural gas engine. The 3-D computational fluid dynamics (CFD) simulation model coupled with a chemical reaction mechanism is described. The temporal development of the short-pulsed diesel spray in a high pressure constant-volume vessel is measured and used to calibrate the spray model in the CFD simulation. The simulation models are validated by the experimental data of the in-cylinder pressure trace, apparent heat release rate (AHRR) and exhaust gas emissions from a single-cylinder MPII natural gas engine. To generate the various combustion chamber geometries, the bowl outline is parameterized by the two cubic Bezier curves while keeping the compression ratio constant. The available design space is explored by the multi-objective non-dominated sorting genetic algorithm II (NSGA-II) with Kriging-based meta-model. With the optimization, the HC and CO emissions are reduced by 56.47% and 33.55%, respectively, while the NOx emissions, the maximum rate of pressure rise and the gross indicated thermal efficiency that are employed as the constraints are slightly improved. Finally, the mechanism of the reduction in HC and CO emissions with the optimized combustion chamber geometry is investigated and discussed in details. (C) 2016 Elsevier Ltd. All rights reserved.
机译:通过使用柴油微飞行员诱导点火(MPII)的天然气发动机的稀薄燃烧概念,实现了无烟,低氮氧化物(NOx)和高热效率。但是,燃烧室通常不专门用于天然气燃烧,未燃烧的碳氢化合物(HC)和一氧化碳(CO)排放量的增加仍然是这类发动机的挑战。本文介绍了燃烧室几何形状的优化,以减少HC和CO排放并提高MPII天然气发动机的燃烧效率。描述了结合化学反应机理的3-D计算流体动力学(CFD)仿真模型。测量高压恒容容器中短脉冲柴油机喷雾的时间变化,并在CFD模拟中用于校准喷雾模型。通过单缸MPII天然气发动机的缸内压力曲线,表观放热率(AHRR)和废气排放的实验数据验证了仿真模型。为了产生各种燃烧室几何形状,在保持压缩比恒定的同时,通过两条三次贝塞尔曲线对碗形轮廓进行参数化。利用基于克里格元模型的多目标非支配排序遗传算法II(NSGA-II)探索了可用的设计空间。通过优化,HC和CO排放量分别减少了56.47%和33.55%,而作为限制条件的NOx排放量,最大压力升高速率和总指示热效率则得到了些微改善。最后,详细研究并讨论了通过优化燃烧室几何形状减少HC和CO排放的机理。 (C)2016 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Energy Conversion & Management》 |2016年第8期|552-563|共12页
  • 作者单位

    Shanghai Jiao Tong Univ, State Key Lab Ocean Engn, Shanghai, Peoples R China|Shanghai Jiao Tong Univ, Collaborat Innovat Ctr Adv Ship & Deep Sea Explor, Shanghai, Peoples R China;

    Shanghai Jiao Tong Univ, State Key Lab Ocean Engn, Shanghai, Peoples R China|Shanghai Jiao Tong Univ, Collaborat Innovat Ctr Adv Ship & Deep Sea Explor, Shanghai, Peoples R China;

    Shanghai Jiao Tong Univ, State Key Lab Ocean Engn, Shanghai, Peoples R China;

    Hokkaido Univ, Fac Engn, Sapporo, Hokkaido, Japan;

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

    Natural gas; Diesel micro-pilot-induced ignition; Combustion chamber geometry; HC/CO emissions; Model-based optimization;

    机译:天然气;柴油微飞行员引燃;燃烧室几何形状;HC / CO排放;基于模型的优化;

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