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Spray Phenomena of Surrogate Fuels and Oxygenated Blends in a High Pressure Chamber

机译:高压室中替代燃料的喷雾现象和氧化混合物

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In this study, we investigate oxygenated blends and Diesel surrogate fuels under engine-like conditions in a high-pressure chamber. The investigated surrogate fuels are composed of n-decane and alpha-methylnaphthalene with different compositions according to the reference cetane numbers (CN) 53, 45, 38 and 23. In addition to the two-component surrogate fuel mixtures, we examine a three-component mixtures composed of n-decane, alpha-methylnaphthalene, and di-n-butyl ether with a reference cetane number of 53 to highlight the influence of adding di-n-butyl ether to the surrogate fuel at constant cetane number. Further, four blends with DNBE contents of 0, 10, 20 and 100 % in EN590 Diesel and corresponding cetane numbers of 53, 57.7, 62.4, and 100 were studied. We examine fuel spray characteristics in the liquid and vapor phases and the relationship between ignition quality and lift-off length. Vapor pressure is observed to significantly affect spray characteristics in the liquid phase. Vapor penetration lengths of the different fuels with the same injection pressure are found to be similar, because the differences of fuel density and viscosity in the vapor phase are too small to considerably affect the momentum flux. However, changing the injection pressures affects the vapor penetration lengths. Results show that CN is a good indicator for ignition delay. Furthermore, we discuss the fuel overlap number (OL) to indicate the separation between the liquid spray core and the reaction zone in engine-like conditions. It is found for the surrogate mixtures that OL generally increases with decreasing CN, while for the DNBE/Diesel mixtures, the opposite trend is observed. The OL number is found to be caused by a combination of cetane number and vapor pressure effects, where CN has the stronger effect for the surrogate mixtures, while the vapor pressure effect is dominant for the DNBE/Diesel blends. In the latter case, the high vapor pressure leads to short liquid penetration length and thereby larger OL number.
机译:在该研究中,我们在高压室中的发动机状条件下调查含氧混合物和柴油替代燃料。调查的替代燃料由N-​​癸烷和α-甲基萘组成,根据参考十六烷值(CN)53,45,38和23。除了双组分替代燃料混合物之外,我们检查三 - 组分混合物由N-癸烷,α-甲基萘和二丁基醚组成,具有参考十六烷数为53,以强调将二丁基醚加入常数十六烷数的替代燃料中的影响。此外,研究了在EN590柴油和相应的53,57.7,62.4和100中的0,10,20和100%的DNBE含量的四种共混物。我们检查液体和蒸汽相中的燃料喷射特性以及点火质量与升降长度之间的关系。观察到蒸气压显着影响液相中的喷雾特性。发现具有相同喷射压力的不同燃料的蒸汽渗透长度是相似的,因为燃料密度和气相中的粘度的差异太小,不能显着影响动量通量。然而,改变注射压力影响蒸汽渗透长度。结果表明,CN是点火延迟的良好指标。此外,我们讨论燃料重叠数(OL)以指示液体喷雾芯和在发动机状条件下的反应区之间的分离。发现替代混合物,即OL通常随着CN的降低而增加,而对于DNBE /柴油混合物,观察到相反的趋势。发现OL编号是由十六烷数量和蒸汽压力效应的组合引起的,其中CN具有替代混合物的效果较强,而蒸气压力效应是DNBE /柴油共混物的主导。在后一种情况下,高蒸汽压力导致液体穿透长度短,从而较大的OL数。

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