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Controlling n-Heptane HCCI Combustion With Partial Reforming: Experimental Results and Modeling Analysis

机译:部分重整控制正庚烷HCCI燃烧:实验结果和模型分析

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One potential method for controlling the combustion phasing of a homogeneous charge compression ignition (HCCI) engine is to vary the fuel chemistry using two fuels with different auto-ignition characteristics. Although a dual-fuel engine concept is technically feasible with current engine management and fuel delivery system technologies, this is not generally seen as a practical solution due to the necessity of supplying and storing two fuels. Onboard partial reforming of a hydrocarbon fuel is seen to be a more attractive way of realizing a dual-fuel concept, while relying on only one fuel supply infrastructure. Reformer gas (RG) is a mixture of light gases dominated by hydrogen and carbon monoxide that can be produced from any hydrocarbon fuel using an onboard fuel processor. RG has a high resistance to auto-ignition and wide flammability limits. The ratio of H_2 to CO produced depends on the reforming method and conditions, as well as the hydrocarbon fuel. In this study, a cooperative fuel research engine was operated in HCCI mode at elevated intake air temperatures and pressures, n-heptane was used as the hydrocarbon blending component because of its high cetane number and well-known fuel chemistry. RG was used as the low cetane blending component to retard the combustion phasing. Other influential parameters, such as air/fuel ratio, EGR, and intake temperature, were maintained constant. The experimental results show that increasing the RG fraction retards the combustion phasing to a more optimized value causing indicated power and fuel conversion efficiency to increase. RG reduced the first stage of heat release, extended the negative temperature coefficient delay period, and retarded the main stage of combustion. Two extreme cases of RG composition with H_2/CO ratios of 3/1 and 1/1 were investigated. The results show that both RG compositions retard the combustion phasing, but that the higher hydrogen fraction RG is more effective. A single-zone model with detailed chemical kinetics was used to interpret the experimental results. The effect of RG on combustion phasing retardation was confirmed. It was found that the low temperature heat release was inhibited by a reduction in intermediate radical mole fractions during low temperature reactions and during the early stages of the negative temperature coefficient delay period.
机译:一种控制均质充量压缩点火(HCCI)发动机燃烧阶段的潜在方法是使用两种具有不同自燃特性的燃料来改变燃料化学成分。尽管使用当前的发动机管理和燃料输送系统技术,双燃料发动机概念在技术上是可行的,但是由于需要供应和存储两种燃料,因此通常不将其视为实用的解决方案。船上碳氢化合物燃料的部分重整被认为是实现双燃料概念的一种更有吸引力的方法,同时仅依赖于一个燃料供应基础设施。重整器气体(RG)是由氢气和一氧化碳控制的轻质气体的混合物,可以使用车载燃料处理器从任何碳氢化合物燃料中产生。 RG具有很高的抗自燃性和较宽的可燃性极限。产生的H_2与CO的比例取决于重整方法和条件以及烃类燃料。在这项研究中,合作的燃料研究引擎在升高的进气温度和压力下以HCCI模式运行,正庚烷由于十六烷值高和众所周知的燃料化学性质而被用作碳氢化合物混合组分。 RG用作低十六烷值共混组分以延迟燃烧定相。其他有影响的参数(例如空燃比,EGR和进气温度)保持恒定。实验结果表明,增加RG分数会使燃烧阶段延迟到更优化的值,从而导致指示的功率和燃料转换效率增加。 RG减少了放热的第一阶段,延长了负温度系数延迟时间,并延迟了燃烧的主要阶段。研究了H_2 / CO比为3/1和1/1的RG组分的两种极端情况。结果表明,两种RG成分均阻碍了燃烧定相,但是较高的氢分数RG更有效。具有详细化学动力学的单区模型用于解释实验结果。证实了RG对燃烧相位延迟的影响。发现在低温反应期间和负温度系数延迟期的早期,中间自由基摩尔分数的减少抑制了低温放热。

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