Improvement of aerodynamic performance of a volute-free centrifugal fan at a large flow rate using a wavy shroud

Hengjun Qin, Haijiang He, Ping Luo, Zhenli Zhang, Zhengdao Wang, Hui Yang, Yikun Wei, Wei Zhang
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Abstract

The volute-free centrifugal fans in ventilation applications are used to exhaust a large amount of air under the effect of the head loss in the ventilation pipeline system, thus, a high static pressure rise at a large flow rate of the fans is anticipated. The shroud of the conventional volute-free centrifugal fans has an axisymmetric geometry, that is, the height of the fan outlet is constant over the whole circumference. Considering the non-uniform flow in the blade passages, the shroud of a wavy geometry might help in improving the static pressure rise and efficiency of the fans at a large flow rate condition. In this work, we performed a numerical investigation on the internal flow of a volute-free centrifugal fan with a wavy shroud. The effect of the geometry of the wavy shroud, as quantified by the maximum height and profile, on the aerodynamic performance of the fan is explored, and the flow physics leading to the performance improvement are demonstrated through a detailed analysis of the patterns of the internal flow. The numerical results showed that compared with the baseline fan with an axisymmetric shroud, the fan with a wavy shroud could substantially improve the static pressure rise and efficiency at the large flow rate. The wavy shroud regulates the near-wall flow especially at the fan outlet; the fluctuation of the radial velocity, secondary flow, and reversed flow is greatly weakened, producing a uniform flow at the fan outlet. The fluctuation of the static pressure in the blade passages and on the shroud side of the fan outlet greatly decreases. Further analysis of the acoustic power level field indicates that the wavy shroud increases the acoustic power at the fan inlet but does not have a notable influence on that near the outlet.
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利用波浪形护罩改善大流量无涡流离心风机的空气动力性能
通风应用中的无卷离心风机用于在通风管道系统水头损失的作用下排出大量空气,因此预计风机在大流量时会产生较高的静压升。传统无涡流离心风机的护罩具有轴对称几何形状,即风机出口的高度在整个圆周上是恒定的。考虑到叶片通道中的非均匀流动,波浪形几何形状的护罩可能有助于提高风机在大流量条件下的静压升和效率。在这项工作中,我们对带有波浪形护罩的无涡旋离心风机的内部流动进行了数值研究。通过对内部流动模式的详细分析,探讨了波浪形护罩的几何形状(以最大高度和轮廓量化)对风机空气动力性能的影响,并展示了导致性能改善的流动物理原理。数值结果表明,与带轴对称护罩的基线风扇相比,带波浪形护罩的风扇可大幅提高大流量时的静压升和效率。波浪形护罩调节了近壁流,尤其是在风机出口处,径向速度、二次流和反向流的波动大大减弱,在风机出口处产生了均匀的流动。叶片通道和风扇出口护罩一侧的静压波动大大减小。对声功率水平场的进一步分析表明,波浪形护罩增加了风扇入口处的声功率,但对出口附近的声功率影响不大。
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来源期刊
CiteScore
3.30
自引率
5.90%
发文量
114
审稿时长
5.4 months
期刊介绍: The Journal of Power and Energy, Part A of the Proceedings of the Institution of Mechanical Engineers, is dedicated to publishing peer-reviewed papers of high scientific quality on all aspects of the technology of energy conversion systems.
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