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A Study on Droplets Evaporation at Diesel Spray Boundary During Ignition Delay Period

机译:点火延迟期间柴油喷雾边界液滴蒸发研究

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Diesel spray evaporation in a high pressure and high ambient temperature close to actual diesel engine condition was investigated in this study. A nano-spark shadowgraph photography technique and a rapid compression machine were applied in this experiment. By using this method, relatively clear image of liquid phase, vapor phase and droplets was obtained. In order to quantify the spray characteristics in the spray liquid area and vapor phase area, an image analysis method was applied. An algorithm was developed to quantify the droplets size and number of the droplets characteristic in the vapor phase. Experimental results have revealed that the injection pressure and the ambient temperature do not affect the spray penetration length apparently. In the case of ambient temperature T{sub}I=700K, the liquid core is observed in the region near the spray axis. Meanwhile, the vapor exists mostly in the outer region in the middle of the spray. However, at T{sub}I=950K, the vapor phase expands and dominates the spray tip region. This is because high ambient temperature promotes the evaporation, and consequently, instantaneous evaporation on a fuel spray occurs as soon as the fuel injection. According to close reference of vapor phase at the spray boundary region, many dark spots can be visualized inside the vapor region. These dark spots seem to indicate the existence of liquid droplets inside the vapor phase. When the fuel is injected into the spray chamber, droplets at outer region of the spray are flying away and evaporate simultaneously. In the case of the evaporation process at high ambient temperature and high injection pressure, the evaporation speed is expedited exceeding the droplets velocity thus trapped the flying droplets in vapor region.
机译:在本研究中研究了柴油喷雾蒸发,在高压和高环境温度下,靠近实际柴油发动机状况进行了研究。在该实验中应用了纳米火车影子拍摄技术和快速压缩机。通过使用该方法,获得液相,气相和液滴的相对清晰的图像。为了量化喷雾液体区域和气相面积的喷射特性,施加图像分析方法。开发了一种算法,以量化液滴在气相中的液滴尺寸和数量。实验结果表明,注射压力和环境温度显然不会影响喷雾渗透长度。在环境温度T {SUB} I = 700K的情况下,在喷射轴附近的区域中观察液体芯。同时,蒸汽主要存在于喷雾中间的外部区域中。然而,在T {Sub} I = 950K处,气相扩增并主导喷雾尖端区域。这是因为高环境温度促进蒸发,因此,一旦燃料喷射就会发生燃料喷雾上的瞬时蒸发。根据喷射边界区域的蒸汽相的紧密参考,可以在蒸汽区内部可视化许多暗点。这些暗点似乎表示存在在气相内的液滴的存在。当将燃料喷射到喷射室中时,喷雾的外部区域的液滴被同时飞走并蒸发。在高环境温度和高注射压力下蒸发过程的情况下,蒸发速度超时超过液滴速度被捕获蒸汽区域中的飞液滴。

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