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Effect of the swirl control valve on the in-cylinder air motion in a four- valve si engine

机译:旋流控制阀对四阀Si发动机缸内空气运动的影响

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The effect of the Swirl Control Valve (SCV) on the in-cylinder flow characteristics was studied using LDA measurement in a single cylinder four- valve spark ignition engine with a SCV. Mean velocity, root-mean-square (rms) velocity fluctuation, and frequency structure of the velocity fluctuation were analyzed to illustrate flow features under the SCV open and closed conditions. The results show that when the SCV is open, large-scale flow structure in the cylinder is mainly tumble vortex, which will distort and break up during the late stage of the compression stroke. The rms velocity fluctuation increases during the compression process and reaches its maximum at certain crank angle before TDC. Larger scale eddies and lower frequency structures in the flow field become more near the end of compression process due to breakup of the tumble. The rms velocity fluctuation in the combustion chamber is roughly uniform at the end of the compression process. When the SCV is closed, however, strong swirl motion produced in the intake process sustains up to the end of compression process. The mean velocity in the cylinder is nearly doubled and the rms velocity fluctuation in the central area of the combustion chamber increases by about 30% compared with the SCV open condition. Smaller scale eddies and higher frequency structures in the flow field increase considerably. And the rms velocity fluctuation in the combustion chamber becomes non-uniform due to its higher value in the central area of the combustion chamber and lower values near the chamber wall.
机译:使用SCV的单缸四阀火花点火发动机中的LDA测量研究了旋流控制阀(SCV)对缸内流动特性的影响。分析了平均速度,根均方(RMS)速度波动和速度波动的频率结构,以说明SCV打开和闭合条件下的流动特征。结果表明,当SCV开放时,气缸中的大规模流动结构主要是滚动涡流,这将在压缩冲程的后期扭曲和分解。在压缩过程中,RMS速度波动增加,并且在TDC之前以某些曲柄角达到其最大值。由于翻滚的分解,流场中的较大刻度漩涡和较低频率结构变得更加接近压缩过程结束。燃烧室中的RMS速度波动在压缩过程结束时大致均匀。然而,当SCV关闭时,在进气过程中产生的强旋流运动会达到压缩过程的结束。与SCV打开状态相比,汽缸中的平均速度几乎加倍,并且燃烧室的中心区域中的速率波动增加了约30%。流场中的较小规模漩涡和较高频率结构会增加。并且由于其在燃烧室的中心区域和腔室壁附近的较低值中,燃烧室中的燃烧室中的速率波动变得不均匀。

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