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首页> 外文期刊>International journal of engine research >Influence of intake geometry variations on in-cylinder flow and flow-spray interactions in a stratified direct-injection spark-ignition engine captured by time-resolved particle image velocimetry
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Influence of intake geometry variations on in-cylinder flow and flow-spray interactions in a stratified direct-injection spark-ignition engine captured by time-resolved particle image velocimetry

机译:时间分辨粒子图像测速仪捕获的分层直喷式火花点火发动机中进气几何形状变化对缸内流和喷流相互作用的影响

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Time-resolved particle image velocimetry and Mie-scattering of fuel droplets at 16kHz were used to capture simultaneously the temporal evolution of the in-cylinder flow field and spray formation within a direct-injection spark-ignition engine. The engine was operated in stratified combustion mode, with stratified mixtures created by a triple injection late in the compression stroke. The impact of geometric variation of the intake port on in-cylinder flow and flow-spray interactions was investigated, focusing on the second injection, since it provides ignitable mixtures at the time of ignition and is subject to strong fluctuations, rather than the first injection, which is very reproducible. Flow field statistics conditioned on the spray shape of the second injection revealed regions with macroscopic cycle-to-cycle flow variations, which correlated with the spray for all recorded cycles. The flow-spray interaction was traced back to before the first injection using correlation analysis, which revealed that cycle-to-cycle fluctuations of the large-scale tumble vortex had a big impact on the spray shape of the second injection, while the first injection was unaffected. This indicates that the origin of the spray fluctuations may be during intake. Despite significant flow modifications due to the intake port geometry variation, fluctuation levels of the second injection were the same for both geometries, that is, spray fluctuations were not sensitive to the geometric change.
机译:时间分辨粒子图像测速和16kHz处燃料滴的Mie散射用于同时捕获缸内流场的时间演变和直喷式火花点火发动机内的喷雾形成。发动机以分层燃烧模式运行,在压缩冲程后期通过三次喷射产生分层混合物。研究了进气口几何变化对缸内流动和流动-喷雾相互作用的影响,重点是第二次喷射,因为它在点火时会提供可点燃的混合气并且易受剧烈波动的影响,而不是第一次喷射,这是非常可重复的。以第二次喷射的喷雾形状为条件的流场​​统计数据显示出区域之间存在宏观的逐周期流动变化,该变化与所有记录的循环的喷雾都相关。使用相关性分析可以追溯到第一次喷射之前的流-流相互作用,结果表明,大滚转涡旋的逐周期波动对第二次喷射的喷雾形状有很大影响,而第一次喷射不受影响。这表明喷雾波动的起因可能是在进气期间。尽管由于进气口几何形状的变化导致流量发生了重大变化,但第二次喷射的波动水平对于两个几何形状都是相同的,也就是说,喷雾波动对几何形状的变化不敏感。

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