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Effects of axial inclined guide vanes on a turbo air classifier

机译:轴向倾斜导向叶片对涡轮空气分级机的影响

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摘要

For a turbo air classifier, the upward axial velocity in the annular region will cause the negative influence on the stability of flow field, and it is also detrimental to material dispersion. As a result, the classification accuracy will be reduced. In order to decrease the upward axial velocity, a downward force must be introduced to offset it. According to the guiding principle of guide vanes, the axial direction of airflow will be changed when the guide vanes are inclined. In this paper an axial inclined guide vane model was designed. Four models (T-0, T-2.5, T-5, T-7.5) were established with axial inclined angles of 0 degrees, 2.5 degrees, 5 degrees and 7.5 degrees. Fluent software was used to simulate the inner flow field of different structures. The simulation results show that axial inclined guide vanes can decrease the upward axial velocity in the annular region. Especially, when the inclined angle is 2.5 degrees, the upward axial velocity is decreased and the tangential velocity is increased. This is favorable to keep the flow field stable. At the same time the classification force field is enhanced to improve the dispersion of the powders. Discrete phase simulation results reveal that particle residence time in the annular region of structure T-2.5 is shorter than it is in the annular region of structure T-0. This can reduce the collision probability of particles and the energy cost is reduced. The partial classification efficiencies of T-2.5 are higher than that of T-0. From the numerical Tromp curves, it is observed that the cut size of T-2.5 is smaller than that of T-0. The classification accuracy of T-2.5 is 90.7%, while that of T-0 is 88.5%. That means that the classification performance is improved with the new structure. Calcium carbonate classification experiment results also show that the cut size decreases by 0.97-8.42 mu m and the accuracy increases by 6%-9% for the structure T-2.5, compared to the structure T-0. Therefore, the structure T-2.5 is more favorable for classification than the structure T-0. These actual experimental results are in good agreement with the simulation results and the significance of this optimization is proved. (C) 2015 Elsevier B.V. All rights reserved.
机译:对于涡轮空气分级机,环形区域中的轴向向上速度将对流场的稳定性产生负面影响,并且也不利于材料分散。结果,分类精度将降低。为了减小向上的轴向速度,必须引入向下的力以抵消它。根据导向叶片的导向原理,倾斜导向叶片时会改变气流的轴向方向。本文设计了一种轴向倾斜导叶模型。建立了四个模型(T-0,T-2.5,T-5,T-7.5),它们的轴向倾斜角分别为0度,2.5度,5度和7.5度。 Fluent软件用于模拟不同结构的内部流场。仿真结果表明,轴向倾斜导流叶片可以减小环形区域中的向上轴向速度。特别地,当倾斜角为2.5度时,向上的轴向速度减小并且切向速度增大。这有利于保持流场稳定。同时,增强了分级力场,以改善粉末的分散性。离散相仿真结果表明,在结构T-2.5的环形区域中的粒子停留时间比在结构T-0的环形区域中的停留时间短。这可以降低粒子的碰撞概率,并且降低了能量成本。 T-2.5的部分分类效率高于T-0。从数字Tromp曲线可以看出,T-2.5的切割尺寸小于T-0的切割尺寸。 T-2.5的分类精度为90.7%,而T-0的分类精度为88.5%。这意味着通过新结构可以提高分类性能。碳酸钙分级实验结果还表明,与结构T-0相比,结构T-2.5的切割尺寸减小了0.97-8.42μm,精度提高了6%-9%。因此,结构T-2.5比结构T-0更有利于分类。这些实际的实验结果与仿真结果吻合良好,并证明了该优化的意义。 (C)2015 Elsevier B.V.保留所有权利。

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