A Novel Experiment Approach for Measurement Breakup Length, Cone Angle, Sheet Velocity, and Film Thickness in Swirl Air-Blast Atomizers

IF 1.1 Q3 TRANSPORTATION SCIENCE & TECHNOLOGY SAE International Journal of Engines Pub Date : 2023-07-31 DOI:10.4271/03-17-01-0006
D. Phung, Thin V. Pham, Phuong X. Pham
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Abstract

Measuring the dynamic parameters of liquid fragments generated in the near-field of atomizing sprays poses a significant challenge due to the random nature of the fragments, the instability of the spray, and the limitations of current measuring technology. Precise determination of these parameters can aid in improving the control of the atomization process, which is necessary for providing suitable spray structures with appropriate flow rates and droplet size distributions for various applications such as those used in heat engines. In piston and gas turbine engines, controlling spray characteristics such as penetration, cone angle, particle size, and droplet size distribution is crucial to improve combustion efficiency and decrease exhaust emissions. This can be accomplished by adjusting the structural and/or operating parameters of the fuel supply system. This article aims to measure the breakup length, spray cone angle, axial velocity, breakup time, and liquid sheet film thickness for a swirl air-blast atomizer used in a gas-steam engine. The measurement was conducted using a shadowgraph imaging system developed specifically for this study, consisting of a high-speed camera, a lens, and a light source. While lasers are commonly used as light sources in the literature, this study utilized a special LED high-speed pulse light generator, which is cheaper, easier to handle, and provides a more uniform background. Images were processed using a MATLAB code developed for this study. Although the breakup zone is naturally random and the breakup location significantly varies with time, the novel method developed in this study helps quantify critical parameters under different operating conditions.
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一种测量旋流鼓风雾化器破碎长度、锥角、片速和膜厚的新实验方法
由于碎片的随机性、喷雾的不稳定性以及现有测量技术的局限性,测量雾化喷雾近场产生的液体碎片的动态参数是一项重大挑战。这些参数的精确测定有助于改善雾化过程的控制,这对于为各种应用(如热机中使用的应用)提供具有适当流速和液滴尺寸分布的合适喷雾结构是必要的。在活塞式和燃气涡轮发动机中,控制喷射特性,如穿透、锥角、颗粒大小和液滴大小分布对提高燃烧效率和减少废气排放至关重要。这可以通过调整燃料供应系统的结构和/或操作参数来实现。本文旨在测量燃气蒸汽机用旋流式鼓风雾化器的破碎长度、喷雾锥角、轴向速度、破碎时间和液膜厚度。测量是使用专门为本研究开发的阴影成像系统进行的,该系统由高速摄像机、镜头和光源组成。虽然在文献中通常使用激光作为光源,但本研究使用了一种特殊的LED高速脉冲光发生器,它更便宜,更容易处理,并且提供了更均匀的背景。使用为此研究开发的MATLAB代码对图像进行处理。虽然破裂区是自然随机的,破裂位置随时间变化很大,但本研究开发的新方法有助于量化不同工况下的关键参数。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
SAE International Journal of Engines
SAE International Journal of Engines TRANSPORTATION SCIENCE & TECHNOLOGY-
CiteScore
2.70
自引率
8.30%
发文量
38
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