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Experimental investigation of pilot-fuel combustion in dual-fuel engines, Part 1: Thermodynamic analysis of combustion phenomena

机译:双燃料发动机试验燃料燃烧的实验研究,第1部分:燃烧现象的热力学分析

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摘要

The pilot-fuel auto-ignition and combustion in compressed methane/air mixtures are investigated. Experiments were performed in an optically accessible rapid compression-expansion machine featuring quiescent charge conditions and a single-hole coaxial diesel injector mounted on the cylinder periphery. It enabled thermodynamic analysis of the pilot-fuel combustion without these phenomena being masked by the rapid premixed-flame propagation like in the engine test rigs with turbulent charge. The aim of this study is to elucidate the first-order influences of charge and pilot-fuel parameters on the ignition delay and transition into the premixed flame propagation. For this purpose, a comprehensive measurement matrix including variations of the premixed fuel equivalence ratio, charge temperature, and oxygen content as well as the variation of pilot injection duration is tested. The heat release rate (HRR) metrics describing the pilot-fuel combustion duration, peak HRR, and cumulative HRR during the pilot-fuel combustion are derived. Correlations of the HRR metrics to the ignition delay, pilot-fuel mixing state at ignition and the volume of the pilot-fuel jet are investigated. Methane is found to increase the ignition delay and prolong the pilot-fuel combustion duration. This effect is amplified for pilot-injection strategies with leaner pilot-fuel mixtures at ignition or in the case of reduced charge oxygen content. Despite the reduced pilot-fuel reactivity the co-combustion of entrained methane leads to higher peak-HRR, except in the reduced charge oxygen cases, where the excessively reduced mixture reactivity with the introduction of methane leads even to a reduced peak-HRR.The phenomenology of the dual-fuel combustion process is described in Part 1, whereas Part 2 of this work aims at improving the understanding of the underlying processes by application of advanced optical diagnostic methods.
机译:研究了压缩甲烷/空气混合物中的试验燃料自燃和燃烧。在光学可接近的快速压缩 - 膨胀机中进行实验,该膨胀条件具有静止电荷条件和安装在汽缸周边上的单孔同轴柴油喷射器。它能够使导燃燃料燃烧的热力学分析,没有这些现象被发动机试验台中的快速预混火焰传播掩盖,如发动机试验台,具有湍流电荷。本研究的目的是阐明充电和试验 - 燃料参数对点火延迟和过渡到预混火焰繁殖的一流影响。为此目的,测试包括预混合燃料等效比,电荷温度和氧含量的变化以及导频注射持续时间的变化的综合测量矩阵。衍生出在试验 - 燃料燃烧期间的导燃燃烧持续时间,峰值HRR和累积HRR的热释放率(HRR)度量。研究了HRR指标对点火延迟的相关性,点火时的试验燃料混合状态以及导燃料射流的体积。发现甲烷增加点火延迟并延长导燃料燃料燃烧持续时间。对于在点火时的稀释燃料混合物或在减少电荷氧含量的情况下,这种效果被扩增。尽管导燃料反应性降低,但夹带的甲烷的共燃烧导致较高的峰-HRR,除了减少的电荷氧案例外,在引入甲烷引入的情况下过度降低的混合物反应性均匀于降低的峰-HRR。第1部分中描述了双燃料燃烧过程的现象学,而本工作的第2部分旨在通过应用先进的光学诊断方法改善对底层过程的理解。

著录项

  • 来源
    《Fuel》 |2019年第1期|115642.1-115642.16|共16页
  • 作者单位

    Paul Scherrer Inst Energy & Environm Div Forsch Str 111 CH-5232 Villigen Switzerland;

    Paul Scherrer Inst Energy & Environm Div Forsch Str 111 CH-5232 Villigen Switzerland;

    Univ Appl Sci & Arts Northwestern Switzerland Inst Thermal & Fluid Engn Sch Engn Klosterzelgstr 2 CH-5210 Windisch Switzerland;

    Swiss Fed Inst Technol Inst Energy Technol Lab Aerothermochem & Combust Syst Sonneggstr 3 CH-8092 Zurich Switzerland;

    IFP Energies Nouvelles Inst Carnot IFPEN Transports Energie 1 & 4 Ave Bois Preau F-92852 Rueil Malmaison France;

  • 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

    Dual-fuel engines; Natural-gas engines; Combustion mode transition; Autoignition; Tracer-PLIF; Combustion phenomenology;

    机译:双燃料发动机;天然气发动机;燃烧模式过渡;自燃;Tracer-PLIF;燃烧现象学;

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