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首页> 外文期刊>International Journal of Multiphase Flow >Measurement and prediction of droplet size in annular gas-liquid flows in aero-engine oil systems
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Measurement and prediction of droplet size in annular gas-liquid flows in aero-engine oil systems

机译:航空发动机油系统中环形气液流动液滴尺寸的测量与预测

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Two-phase gas-liquid annular flows are encountered in ventless aero-engine oil system pipes. The droplet size in the flow has an important impact on the performance of downstream equipment as breathers and de-aerators. However, literature studies present semi-empirical models that are not in the range of operating conditions of the oil system. To investigate the effect of the use of lubrication oil on the droplet sizes, this paper presents experimental results of annular flow with oil flow rates from 160 to 640 1/h and air flow rates from 60 to 120 Nm(3)/h. Comparison of the Sauter-Mean Diameter predicted by existing correlation show an error of minimum 30% compared to experimental values for higher oil flow rates, which are the most important in oil systems. To address this issue, correlations were adapted to fit experimental results. With the new set of parameters, the Sauter-Mean Diameter is estimated with an error of maximum 18% for higher oil flow rates. Results analysis illustrate that the main difference between existing and new correlations could be due do the surface tension and viscosity of lubrication oil, which are very different from water at low temperature. The results are also consistent with the transition between bag and ligament break-up droplet generation mechanism at a flow rate of 80 Nm(3)/h. (C) 2017 Elsevier Ltd. All rights reserved.
机译:Vtilless Aero-Megent油系统管道遇到了两相气体环形流量。流动中的液滴尺寸对下游设备的性能产生了重要影响,作为呼吸和拆卸器。然而,文学研究存在目前没有在石油系统的运行条件范围内的半实证模型。为了探讨使用润滑油在液滴尺寸上使用润滑油的影响,本文介绍了从160至6401 / h的油流速的环形流动的实验结果,以及60至120nm(3)/ h的空气流速。与现有相关性预测的燃露刀平均直径的比较显示出与更高的油流速的实验值相比最低30%的误差,这是油系统中最重要的。为了解决这个问题,相关性适于适应实验结果。利用新的一组参数,估计制冷器平均直径,误差最大为18%,以获得更高的油流量。结果分析说明现有和新相关性之间的主要区别可能是由于润滑油的表面张力和粘度,这与低温下的水非常不同。结果也与袋子和韧带分解液滴产生机制的过渡以80nm(3)/ h的流速一致。 (c)2017 Elsevier Ltd.保留所有权利。

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