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An Experimental and Modeling Study of HCCI Combustion Using n-Heptane

机译:正庚烷燃烧HCCI的实验与模型研究

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Homogeneous charge compression ignition (HCCI) is an advanced low-temperature combustion technology being considered for internal combustion engines due to its potential for high fuel conversion efficiency and extremely low emissions of paniculate matter and oxides of nitrogen (NO_x). In its simplest form, HCCI combustion involves the auto-ignition of a homogeneous mixture of fuel, air, and diluents at low to moderate temperatures and high pressure. Previous research has indicated that fuel chemistry has a strong impact on HCCI combustion. This paper reports the preliminary results of an experimental and modeling study of HCCI combustion using n-heptane, a volatile hydrocarbon with well known fuel chemistry. A Co-operative Fuel Research (CFR) engine was modified by the addition of a port fuel injection system to produce a homogeneous fuel-air mixture in the intake manifold, which contributed to a stable and repeatable HCCI combustion process. Detailed experiments were performed to explore the effects of critical engine parameters such as intake temperature, compression ratio, air/fuel ratio, engine speed, turbocharging, and intake mixture throttling on HCCI combustion. The. influence of these parameters on the phasing of the low-temperature reaction, main combustion stage, and negative temperature coefficient delay period are presented and discussed. A single-zone numerical simulation with detailed fuel chemistry was developed and validated. The simulations show good agreement with the experimental data and capture important combustion phase trends as engine parameters are varied.
机译:均质充量压缩点火(HCCI)是一种先进的低温燃烧技术,由于其具有高燃料转化效率以及极低的颗粒物和氮氧化物(NO_x)排放潜力而被考虑用于内燃机。 HCCI燃烧以其最简单的形式涉及在低至中等温度和高压下自动点燃燃料,空气和稀释剂的均匀混合物。先前的研究表明,燃料化学性质对HCCI燃烧有很大影响。本文报告了使用正庚烷(一种具有众所周知的燃料化学性质的挥发性烃)进行的HCCI燃烧实验和模型研究的初步结果。通过添加进气口燃油喷射系统对协作式燃油研究(CFR)发动机进行了修改,以在进气歧管中产生均匀的燃油-空气混合物,这有助于稳定且可重复的HCCI燃烧过程。进行了详细的实验,以探索关键发动机参数(如进气温度,压缩比,空燃比,发动机转速,涡轮增压和进气混合物节流)对HCCI燃烧的影响。的。提出并讨论了这些参数对低温反应阶段,主燃烧阶段和负温度系数延迟时间的影响。开发并验证了具有详细燃料化学成分的单区数值模拟。仿真结果显示与实验数据吻合良好,并随着发动机参数的变化捕获了重要的燃烧阶段趋势。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2010年第2期|022801.1-022801.10|共10页
  • 作者单位

    National Research Council Canada, 1200 Montreal Road, Ottawa, ON, K1A 0R6, Canada;

    National Research Council Canada, 1200 Montreal Road, Ottawa, ON, K1A 0R6, Canada;

    National Research Council Canada, 1200 Montreal Road, Ottawa, ON, K1A 0R6, Canada;

    West Virginia University, P.O. Box 6106, Morgantown, WV, 26506;

    National Renewable Energy Laboratory, 1617 Cole Boulevard, Golden, CO 80401;

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