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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Analysis of Crank Angle- Resolved Vortex Characteristics Under High Swirl Condition in a Spark-Ignition Direct- Injection Engine
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Analysis of Crank Angle- Resolved Vortex Characteristics Under High Swirl Condition in a Spark-Ignition Direct- Injection Engine

机译:火花点火式直喷发动机高涡度条件下曲轴转角涡旋特性分析

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摘要

In-cylinder air flow structure makes significant impacts on fuel spray dispersion, fuel mixture formation, and flame propagation in spark ignition direct injection (SIDI) engines. While flow vortices can be observed during the early stage of intake stroke, it is very difficult to clearly identify their transient characteristics because these vortices are of multiple length scales with very different swirl motion strength. In this study, a high-speed time-resolved two-dimensional (2D) particle image velocimetry (PIV) is applied to record the flow structure of in-cylinder flow field along a swirl plane at 30 mm below the injector tip. First, a discretized method using flow field velocity vectors is presented to identify the location, strength, and rotating direction of vortices at different crank angles. The transients of vortex formation and dissipation processes are revealed by tracing the location and motion of the vortex center during the intake and compression strokes. In addition, an analysis method known as the wind-rose diagram, which is implemented for meteorological application, has been adopted to show the velocity direction distributions of 100 consecutive cycles. Results show that there exists more than one vortex center during early intake stroke and their fluctuations between each cycle can be clearly visualized. In summary, this approach provides an effective way to identify the vortex structure and to track the motion of vortex center for both large-scale and small-scale vortices.
机译:缸内空气流动结构对火花点火直接喷射(SIDI)发动机中的燃油喷雾扩散,燃油混合物形成以及火焰传播产生了重大影响。尽管可以在进气冲程的早期阶段观察到涡流,但很难清楚地识别它们的瞬态特性,因为这些涡流具有多个长度尺度,且涡流运动强度差异很大。在这项研究中,采用高速时间分辨二维(2D)粒子图像测速技术(PIV)来记录缸内流场沿喷油嘴尖端下方30 mm的旋流平面的流动结构。首先,提出了一种使用流场速度矢量的离散化方法来识别不同曲柄角处涡旋的位置,强度和旋转方向。通过追踪进气和压缩冲程期间涡流中心的位置和运动,揭示了涡流形成和消散过程的瞬态。另外,已经采用了一种被称为风玫瑰图的分析方法,该方法用于气象应用,以显示100个连续周期的速度方向分布。结果表明,在早期进气冲程中存在一个以上的涡旋中心,并且可以清楚地看到每个周期之间的波动。总之,该方法为大型和小型涡旋提供了一种识别涡旋结构并跟踪涡旋中心运动的有效方法。

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