Orthogonal optimization design of a Sirocco fan and numerical analysis on the internal flow characteristics

IF 1.2 4区 工程技术 Q3 ENGINEERING, MECHANICAL
Zhengfeng Liu, Zhengdao Wang, Shouhua Du, Hui Yang, Yi-kun Wei, Wei Zhang
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引用次数: 0

Abstract

The forward-curved multi-blade centrifugal fan, also termed as Sirocco fan, is characterized by its complex characteristics of internal flow within the impeller and volute. Currently most of the fans are designed with modifications or optimizations for certain geometric parameters which could not ensure the well compatibility of flow in the impeller and volute, thus it is difficult to improve the aerodynamic performances of the fans. In this paper, we performed a multi-parameter design of a Sirocco fan with optimizations on the geometric parameters of the impeller and volute. The geometric parameters of the volute were designed based on analysis of the internal flow patterns, and the influence from the impeller is also considered. Optimization on the geometric parameters was carried out using the steepest descent method to improve the static pressure rise and efficiency under the designed flow rate by taking into account the relevance of flow in the impeller and volute. The effect of the parametric optimization is evaluated and analyzed by large-eddy simulation (LES). It was found that the static pressure rise and efficiency of the optimized model increase by 1.8% and 5.0% compared with the baseline model, respectively. The static pressure rise fluctuates in a regularly periodic manner. The optimized model reduces the area of low-pressure recirculating flow at the center of the fan and the separated flow on the suction surface of the blades. The near-wall flow on the volute surface is more stable, and the pressure fluctuation around the volute tongue is reduced. The outflow of the volute exhibits better uniformity than the baseline model.
热风风机正交优化设计及内部流动特性数值分析
前曲多叶片离心风机,又称Sirocco风机,其特点是叶轮和蜗壳内部流动的复杂特性。目前大多数风机的设计都是针对某些几何参数进行修改或优化,无法保证叶轮和蜗壳内的流动具有良好的相容性,因而难以提高风机的气动性能。本文通过对叶轮和蜗壳几何参数的优化,对一台热风风机进行了多参数设计。在分析蜗壳内部流态的基础上,设计了蜗壳的几何参数,并考虑了叶轮的影响。考虑叶轮和蜗壳内流动的相关性,采用最陡下降法对几何参数进行优化,以提高设计流量下的静压升和效率。通过大涡模拟(LES)对参数优化的效果进行了评价和分析。结果表明,与基线模型相比,优化后模型的静压升和效率分别提高了1.8%和5.0%。静压升有规律地周期性波动。优化后的模型减小了风机中心低压再循环流动面积和叶片吸力面分离流动面积。蜗壳表面近壁流动更加稳定,蜗壳隔舌周围压力波动减小。蜗壳流出比基线模型表现出更好的均匀性。
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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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