空气动力学
围带
轴流压缩机
转子(电动)
总压比
静压
噪音(视频)
降噪
还原(数学)
工程类
叶尖间隙
机械风扇
结构工程
控制理论(社会学)
声学
航空航天工程
计算机科学
机械工程
物理
数学
几何学
控制(管理)
人工智能
气体压缩机
图像(数学)
作者
Shaoguang Zhang,Runze Li,Yufei Zhang,Haixin Chen
标识
DOI:10.1061/(asce)as.1943-5525.0001304
摘要
This paper focused on the aerodynamic optimization and noise reduction of a two-stage series compact fan. The space constraints of compact fans limit the design space, which poses several challenges to aerodynamic and noise performance. The aerodynamic performance and noise characteristics of a baseline series axial fan show that the interaction between the first-stage and second-stage fans is weakened because of the effect of the honeycomb panel. A dual-objective optimization of the rotor blade with the power consumption and static pressure efficiency as the design objectives was carried out on a single-stage axial fan based on a radial basis function (RBF)-enhanced differential evolutionary (RADE) algorithm. The result showed that the dual-objective optimization achieved good results in the aerodynamic design of the two-stage series fan. Compared with the baseline configuration, the static pressure efficiency of the optimized axial-flow fan increased by 6%. The first blade-passing frequency (BPF) noise was reduced by 7 dB. An expansion shroud was designed based on the optimized design of the axial-flow fan. The expansion shroud configuration further increased the static pressure efficiency by 10%.
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