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Experimental and numerical study of the effects of nozzle taper angle on spray characteristics of GDI multi-hole injectors at cold condition

机译:喷嘴锥角对冷条件GDI多孔喷射器喷射特性的实验和数值研究

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摘要

With today's stringent legislative requirements, every combustion/emission contributing component must be researched and optimized in modern gasoline direct injection (GDI) engines. However, a limited amount of research on the taper angle of gasoline injector nozzles can be found. In this study, three GDI fuel injectors are investigated to study the effects of nozzle taper angle on spray characteristics. All of the injectors have the same inlet diameter, and the only difference is the nozzle taper angle. Fuel pressure was set at 200 bar and fuel temperature was at room temperature. A numerical method was used to study the internal nozzle flow, and various optical techniques were applied to investigate the spray characteristics. It was found that adjusting the nozzle taper angle didn't induce any noticeable difference in the static flow rate, which was linear with the square root of the pressure differential across the orifice plate. As a result, the initial tip penetration was proportional to the injection timing, and nearly independent with the nozzle taper angle. For well-developed sprays, larger nozzle taper angle resulted in shorter penetration and faster breakup. Increasing the nozzle taper angle resulted in larger space between internal flow and the nozzle wall, which enhanced air entrainment into the nozzle. Consequently, flow radial velocity at the nozzle exit increased, which was beneficial to spray breakup and atomization. Larger nozzle taper angle resulted in wider fuel plume, larger plume angle, broader and shorter global spray, which increased the possibility of plume interaction. Smaller fuel drops were measured from the injectors with larger taper angle. Finally, it shows that adjusting the taper angle of the nozzle offers an additional degree of freedom when trying to optimize the spray characteristics of an injector for improved fuel atomization, engine combustion performance and emissions reduction.
机译:通过当今严格的立法要求,必须在现代汽油直接注射(GDI)发动机中研究和优化每个燃烧/排放贡献组件。然而,可以找到对汽油喷油喷嘴的锥角的有限数量的研究。在这项研究中,研究了三个GDI燃料喷射器,以研究喷嘴锥角对喷雾特性的影响。所有喷射器具有相同的入口直径,唯一的差异是喷嘴锥角。燃料压力设定为200巴,燃料温度在室温下。使用数值方法来研究内部喷嘴流动,并应用各种光学技术来研究喷射特性。发现调节喷嘴锥角没有诱导静态流速的任何明显差异,这与孔板上的压差的平方根线性线性。结果,初始尖端渗透与喷射正时成比例,并且与喷嘴锥角几乎独立。对于发达的喷雾,较大的喷嘴锥角导致渗透性较短,破速速度更快。增加喷嘴锥角导致内部流动和喷嘴壁之间的较大空间,该喷嘴壁增强了空气夹带到喷嘴中。因此,喷嘴出口处的流动径向速度增加,有利于喷涂分离和雾化。较大的喷嘴锥角导致更宽的燃料羽流,较大的羽量角,更宽,更短的全球喷雾,这增加了羽流相互作用的可能性。从具有较大锥角的喷射器测量较小的燃料滴。最后,它表明,当试图优化喷射器的喷射特性时,调节喷嘴的锥角提供额外的自由度,以改善燃料雾化,发动机燃烧性能和减少排放。

著录项

  • 来源
    《Fuel》 |2020年第1期|117888.1-117888.12|共12页
  • 作者单位

    Univ Michigan Dept Mech Engn Ann Arbor MI 48109 USA|Ford Motor Co Powertrain Res & Adv Engn Dearborn MI 48124 USA;

    Vitesco Technol Powertrain Technol & Innovat Auburn Hills MI 48326 USA;

    Ford Motor Co Powertrain Res & Adv Engn Dearborn MI 48124 USA;

    Ford Motor Co Powertrain Res & Adv Engn Dearborn MI 48124 USA;

  • 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

    GDI injector; Nozzle taper angle; Internal flow; Spray structure; Drop size;

    机译:GDI注射器;喷嘴锥角;内部流动;喷雾结构;滴尺寸;

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