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A study of a turbulent jet ignition system fueled with iso-octane: Pressure trace analysis and combustion visualization

机译:异辛烷燃料湍流喷射点火系统的研究:压力痕量分析和燃烧可视化

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Turbulent jet ignition is an advanced pre-chamber ignition enhancement technique for spark ignition engines that uses a discharging jet of hot combusting gases to initiate main chamber combustion. The jet acts as a distributed ignition source, leading to fast burn rates and increased combustion stability. Experiments were performed in an optically accessible rapid compression machine using liquid isooctane to study the effects of auxiliary fuel injection and ignition distribution due to nozzle geometry. A custom low-flow fuel injector was used to overcome previous limitations of using liquid fuel in the pre-chamber. Jet induced autoignition behavior was also studied in depth by considering high-speed images, pressure traces, and pressure derivative data. Published by Elsevier Ltd.
机译:湍流喷射点火是用于火花点火发动机的先进的腔室预点火增强技术,该技术使用热燃烧气体的喷射流来引发主腔室燃烧。射流充当分布式点火源,导致快速燃烧,并提高了燃烧稳定性。在使用液态异辛烷的光学快速压缩机中进行了实验,以研究由于喷嘴几何形状而引起的辅助燃料喷射和点火分布的影响。使用定制的低流量燃料喷射器来克服先前在预燃室中使用液体燃料的限制。还通过考虑高速图像,压力迹线和压力导数数据对喷气诱导的自燃行为进行了深入研究。由Elsevier Ltd.发布

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