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The fuel spray structure of high-pressure direct swirl injector for gasoline injection system

机译:用于汽油喷射系统的高压直流喷射器的燃料喷涂结构

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This paper presents an investigation into global spray behavior and characteristics of injected spray from a High-pressure Direct Swirl Injector (HDSI) at ambient conditions. Three types of swirler were designed at the initial development stage and they were used to analyze the relationship between tangential swirl port angle and spray characteristics. The swirler of the HDSI was designed based on these experimental results; being finalized with design of the valve seat and body. Using the "forward scattering image" method for visualization, the fuel and air mixing characteristics were assessed and laser diffraction was used to measure droplet size. Preliminary results regarding spray development showed that mixing increases with injection pressure. It was also found that the design of the swirler influences initial spray angle, and penetration length. Final analysis indicated spray characteristics of HDSI with mean droplet size below 20 μm, about 70° of spray angle, wide dynamic flow range and low end linearity. Vibration and operating endurance testing were performed to verify the injector performance.
机译:本文介绍了在环境条件下从高压直流喷射器(HDSI)的全局喷射行为和注入喷射的特性。在初始开发阶段设计了三种类型的旋流器,它们用于分析切向旋流角度和喷射特性之间的关系。基于这些实验结果设计了HDSI的旋流器;最终确定阀座和身体的设计。使用“前进散射图像”方法进行可视化,评估燃料和空气混合特性,并使用激光衍射测量液滴尺寸。关于喷雾开发的初步结果表明,混合随注射压力增加。还发现旋流器的设计影响初始喷射角度和穿透长度。最终分析表明HDSI的喷涂特性,平均液滴尺寸低于20μm,约70°的喷射角,宽动态流量范围和低端线性度。进行振动和操作耐久性测试以验证注射器性能。

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