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Computer Fluid Dynamics Analysis of Cryogenic Oil Mist and Structural Optimization of Spraying Nozzle

机译:电脑流体动力学分析对喷嘴的低温油雾和结构优化

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An investigation of the cryogenic oil mist flow field of nozzle was carried out in this study. A domain of the nozzle jet area was modeled with Pro/ENGINEER. CFD (Computational Fluid Dynamics) analysis was used to state the velocity field of different distances from the outlet of nozzle. The simulating velocity field was verified with the experimental results. Experimental results on velocity were measured by SYT-2000 digital multipurpose wind speed gage. The orthogonal experiment was designed to investigate the main effects parameters on velocity and temperature. It indicates that higher flow of cold air and smaller diameter of nozzle's outlet will generate higher velocity. The temperature of cold air has most influence on the temperature of measuring point. Finally the optimum structure of the spraying nozzle was proposed.
机译:本研究开展了对喷嘴冷冻油雾流动场的研究。喷嘴喷射区域的域用Pro / ENGINEER建模。 CFD(计算流体动力学)分析用于达到喷嘴出口的不同距离的速度场。通过实验结果验证了模拟速度场。通过SYT-2000数字多用途风速测量测量速度的实验结果。正交实验旨在研究对速度和温度的主要影响参数。它表示较高的冷空气流量和喷嘴出口的较小直径将产生更高的速度。冷空气的温度对测量点的温度影响最大。最后提出了喷嘴的最佳结构。

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