啤酒罐和涡轮液体喷嘴喷雾的实验和可视化

A. Kankkunen, S. Koivisto, K. Saari, Mika Jarvinen, J. Biggs, Andrew P. Jones
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摘要

以水为试验流体,对工业规模旋流式黑液喷嘴进行了研究。简单的喷水实验对研究和比较喷黑液喷嘴非常有益。这些实验对于找到更好的喷嘴设计是很重要的。研究了三种喷嘴的设计,以了解这些喷嘴之间的功能差异。喷嘴1(“切向涡流”)和喷嘴3(“涡轮”)的压力损失分别比喷嘴2(“切向涡流”)高97%和38%。喷嘴1、喷嘴2和喷嘴3的喷雾开口角分别为75°、60°和35°。视频成像显示,喷嘴产生的喷雾从喷嘴中心线倾斜了几度。喷淋模式显示所有的喷淋都是不对称的,而喷嘴2是最对称的。激光多普勒测量显示喷嘴之间的喷射速度差异很大。当流量从1.5 L/s增加到2.5 L/s时,喷嘴1的喷射速度从9 m/s增加到15 m/s。喷嘴2的速度从7 m/s增加到11 m/s,喷嘴3的速度从8 m/s增加到13 m/s。切向流(漩涡)使喷雾远离垂直平面6°-12°。通过对高速视频图像的分析,估计了液片破碎的机理和长度。喷嘴1的液片破碎机制估计为波浪形成,液片长度估计为10 cm左右。喷管2的破片机理为波浪形成和破片穿孔,破片长度约为20 cm。3号喷嘴不应该形成液体片。喷嘴的几何形状对喷雾特性有很大的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experiments and visualization of sprays from beer can and turbo liquor nozzles
Industrial scale swirl-type black liquor nozzles were studied using water as the test fluid. Simple water spraying experiments were found to be very beneficial for studying and comparing nozzles for black liquor spraying. These kinds of experiments are important for finding better nozzle designs. Three nozzle designs were investigated to understand the functional differences between these nozzles. The pres-sure loss of nozzle 1 (“tangential swirl”) and nozzle 3 (“turbo”) were 97% and 38% higher compared to nozzle 2 (“tan-gential swirl”). Spray opening angles were 75°, 60°, and 35° for nozzles 1, 2, and 3, respectively. Video imaging showed that the nozzles produced sprays that were inclined a few degrees from the nozzle centerline. Spray patter-nation showed all the sprays to be asymmetric, while nozzle 2 was the most symmetric. Laser-Doppler measure-ments showed large differences in spray velocities between nozzles. The spray velocity for nozzle 1 increased from 9 m/s to 15 m/s when the flow rate was increased from 1.5 L/s to 2.5 L/s. The resulting velocity increase for nozzle 2 was from 7 m/s to 11 m/s, and for nozzle 3, it was from 8 m/s to 13 m/s. Tangential flow (swirl) directed the spray 6°–12° away from the vertical plane. Liquid sheet breakup mechanisms and lengths were estimated by analyzing high speed video images. The liquid sheet breakup mechanism for nozzle 1 was estimated to be wave formation, and the sheet length was estimated to be about 10 cm. Sheet breakup mechanisms for nozzle 2 were wave formation and sheet perforation, and the sheet length was about 20 cm. Nozzle 3 was not supposed to form a liquid sheet. Nozzle geometry was found to greatly affect spray characteristics.
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