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Experimental study on impingement spray and near-field spray characteristics under high-pressure cross-flow conditions

机译:高压错流条件下冲击喷雾和近场喷雾特性的实验研究

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摘要

The fuel spray injected into a direct injection (DI) engine is substantially affected by both the in-cylinder air flow and the piston cavity wall impingement. The combined effect of the air flow and the wall impingement plays an important role on the spray development, mixture formation, and subsequent combustion. In this study, the effects of cross-flow and flat wall impingement on the spray development and dispersion were investigated. The spray was injected by a valve covered orifice (VCO) nozzle under various cross-flow velocities and ambient pressures. Impingement spray images in a vertical plane and several horizontal planes were obtained by a high speed video camera and a continuous wave laser sheet. A high speed video camera connected with a long-distance microscope was employed to obtain the near-field spray images. The results show that cross-flow favors spray dispersion while the high ambient pressure tends to compress the spray profiles. Additionally, under an approximate liquid-to-air momentum flux ratio q, when the ambient pressure and cross-flow velocity were varied, at 2 ms ASOI the outlines of the spray in the windward side agree well, whereas the spray extended further in the leeward side at a lower ambient pressure. At the plane of y = 25 mm, a complex vortex movement was observed that resulted in a non-uniform distribution of droplets in the upper part of the spray in the leeward side. In addition, at the plane of y = 45 mm, an empty belt area occurred in the vortex core region revealing that the density of the droplets in this region was quite low. The quantitative analysis shows that with increasing cross-flow velocity, the spray tip penetration decreases slightly before impingement while the spray tip penetrates further on the wall surface after impingement. The high cross-flow velocity favors the spray breakup and dispersion leading to a larger wall-jet vortex while the high ambient pressure restrains the spray dispersion leading to a smaller spray tip penetration and vortex height. For near-field spray, the spray image at higher ambient pressure shows fewer ligaments. With increasing cross-flow velocity, the whole spray shifted downstream. The spray outline was wider at the initial stage (0.05 ms ASOI) than that at steady stage (2 ms ASOI) of spray evolution.
机译:喷射到直接喷射(DI)发动机中的燃油喷雾基本上受缸内气流和活塞腔壁撞击的影响。气流和壁撞击的综合作用在喷雾形成,混合物形成和随后的燃烧中起重要作用。在这项研究中,研究了横流和扁平壁撞击对喷雾形成和分散的影响。通过阀盖孔口(VCO)喷嘴在各种错流​​速度和环境压力下喷射喷雾。通过高速摄像机和连续波激光片获得垂直平面和几个水平平面上的冲击喷涂图像。使用与远距离显微镜连接的高速摄像机来获得近场喷雾图像。结果表明,错流有利于喷雾分散,而高环境压力则倾向于压缩喷雾分布。此外,在近似的液-气动量通量比q下,当环境压力和横流​​速度发生变化时,在2 ms ASOI时,迎风侧的喷雾轮廓很好地吻合,而喷雾在下风侧处于较低的环境压力。在y = 25 mm的平面上,观察到复杂的涡旋运动,这导致了在背风侧喷雾上部的液滴分布不均匀。另外,在y = 45mm的平面上,在涡流芯区域中出现空带区域,这表明该区域中的液滴的密度非常低。定量分析表明,随着横流速度的增加,在撞击之前,喷嘴的穿透力会略微降低,而在撞击之后,喷嘴会进一步渗透到壁表面。较高的横流速度有利于喷雾破裂和分散,从而导致较大的壁流涡流,而较高的环境压力则抑制喷雾分散,从而导致较小的喷嘴尖端渗透和涡流高度。对于近场喷雾,在较高环境压力下的喷雾图像显示较少的韧带。随着横流速度的增加,整个喷雾向下游移动。在初始阶段(0.05 ms ASOI),喷雾轮廓要比在稳定阶段(2 ms ASOI)的喷雾轮廓宽。

著录项

  • 来源
    《Fuel》 |2018年第15期|12-22|共11页
  • 作者单位

    Hiroshima Univ, Dept Mech Syst Engn, 1-4-1 Kagamiyama, Higashihiroshima 7398527, Japan;

    Hiroshima Univ, Dept Mech Syst Engn, 1-4-1 Kagamiyama, Higashihiroshima 7398527, Japan;

    Hiroshima Univ, Dept Mech Syst Engn, 1-4-1 Kagamiyama, Higashihiroshima 7398527, Japan;

    Hiroshima Univ, Dept Mech Syst Engn, 1-4-1 Kagamiyama, Higashihiroshima 7398527, Japan;

    Wuhan Univ Technol, Sch Mech & Elect Engn, 122 Luoshi Rd, Wuhan 430070, Hubei, Peoples R China;

    Xi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Shaanxi, Peoples R China;

    Xi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Shaanxi, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Fuel spray; High-pressure cross-flow; Spray-wall impingement; Laser sheet; Near-field spray;

    机译:燃油喷雾;高压横流;喷壁撞击;激光薄板;近场喷雾;

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