Blade shape optimization and internal-flow characteristics of the backward non-volute centrifugal fan

被引:5
|
作者
Zhang, Hongjie [1 ]
Wang, Zhengdao [1 ]
Yang, Hui [1 ]
Zhu, Zuchao [1 ]
Wei, Yikun [1 ]
机构
[1] Zhejiang Sci Tech Univ, Fac Mech Engn & Automat, Natl Prov Joint Engn Lab Fluid Transmiss Syst Tec, 2 Jianggan Areas, Hangzhou 310018, Zhejiang, Peoples R China
基金
中国国家自然科学基金;
关键词
Blade profile; non-volute centrifugal fan; steepest descent method; computational fluid dynamics; PERFORMANCE; ANGLE;
D O I
10.1177/09576509211052728
中图分类号
O414.1 [热力学];
学科分类号
摘要
The work proposed the double parameter optimization method of the non-volute centrifugal fan's blade profile based on the steepest descent method. Total-pressure efficiency improvement at the high-flow area was taken as an optimization objective. A method of applying the steepest descent method to modify the blade profile of backward centrifugal fan is proposed in this paper. The gradient descent direction was analyzed to design the blade profile and obtain the optimal blade profile at a high-flow rate. Besides, numerical simulations were carried out to analyze the aerodynamic performance and the internal flow characteristics of the centrifugal fan by the computational fluid dynamics method. Numerical results showed that the blade profile along the gradient descent was optimized to effectively increase the total pressure and the total pressure efficiency of the original model at the high-flow rate. The steepest descent method for local optimization could improve the fan blade design.
引用
收藏
页码:673 / 688
页数:16
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