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Similarity Analysis of the Chemical Kinetic Mechanism on the Ignition Delay in Shock Tubes and Homogeneous Charge Compression Ignition (HCCI) Engines

机译:减震管和均匀电荷压缩点火点火延迟的化学动力学机制的相似性分析(HCCI)发动机

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The chemical kinetic mechanism determines the ignition timing of homogeneous charge compression ignition (HCCI) engines. The correlation of the ignition delay in shock tubes and HCCI engines under different operating conditions was studied with a reduced mechanism of the primary reference fuel (PRF) composing of n-heptane and iso-octane. According to the similarity analysis of the sensitivity coefficient, the operating conditions which affect the similarity factor are recognized. The results indicate that, under the negative temperature coefficient (NTC) region of the ignition delay in shock tubes, the weight of each reaction on the ignition delay in shock tubes is similar to that in HCCI engines. The ignition delay time in HCCI engines is defined as the period from the time of start of heat release (SHR) with the HRR greater than zero to CA10. At the high equivalence ratios in shock tubes, the similarity factor at the low ambient temperatures is small. For the cases with the high similarity factor, the ambient pressure increases with the increased temperature. It is concluded that the effect of the ambient temperature on the ignition delay is more obvious than that of equivalence ratio and the ambient pressure. Overall, under the conditions with large similarity factor, the performance of the chemical mechanism in shock tubes can be a good guide for the application of the mechanism to HCCI engines.
机译:化学动力学机制确定均质充量压缩点火(HCCI)发动机的点火正时。在不同的操作条件下激波管和HCCI发动机点火延迟的相关性与构成正庚烷和异辛烷的主参考燃料(PRF)的缩小机制研究。根据灵敏度系数的相似性分析,影响相似性因子的操作条件被识别。结果表明,在激波管点火延迟的负温度系数(NTC)区域下,在激波管点火延迟各反应的重量是类似于在HCCI发动机。在HCCI发动机中,点火延迟时间被定义为从热释放(SHR)与HRR大于零至CA10的开始的时间段。在激波管高的当量比,在低环境温度下的相似性因子是小的。对于具有高相似性因子的情况下,与环境压力增加而增加的温度。可以得出结论,在环境温度对点火延迟的效果比当量比和环境压力更加明显。总体而言,与大型的类似度的条件下,化学机制在激波管的性能可以为机制的应用,HCCI发动机具有很好的指导。

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