Multidisciplinary design optimization to reduce erosion of blades in a mixed flow fan

作者：Wang Jian; Wen Suping^*; Li Ting; Xi Guang

来源：Proceedings of the Institution of Mechanical Engineers - Part A: Journal of Power and Energy , 2014, 228(1): 64-82.

DOI：10.1177/0957650913508549

• Multidisciplinary design optimization
• anti-erosion design
• solid particle erosion
• turbomachinery
• mixed flow fan
• Pareto optimum

This paper presents an anti-erosion design approach of multidisciplinary design optimization (MDO) for turbomachinery to improve the erosion resistance of the blades, and its application to the design of an industrial mixed flow fan is given. The method is based on a concept for turbomachinery anti-erosion design in the aerodynamic design stage by modifying the geometry of the turbomachinery. The MDO approach replaces the traditional time consuming design method through automatic analyses of the aerodynamic performance, stress distribution and erosion characteristics, controlled by the optimization strategy. In the MDO approach, a multi-objective optimization algorithm non-dominated sorting genetic algorithm-II combined with radial basis function meta-model is used to find the compromise between the conflicting demands of high-efficiency and low average erosion rate with constraints on the pressure ratio and the safety factor for the blade; finite element method is used to analyze the static mechanical responses of the blade; a Navier-Stokes solver is used to predict the aerodynamic performance; solid particle paths in a viscous flow are calculated by Lagrangian method, and then the prediction of erosion is performed based on Tabakoff erosion model. Both the aerodynamic and anti-erosion performances of three selected robust optimal solutions on the Pareto front are compared to those of the baseline. The results show that the main reason for the efficiency improvement of the optimized blades is probably the smaller flow separation region and weaker secondary flows. Furthercomparative analysis between the baseline blade and the compromise blade for the impinging parameters is presented, and the erosion rate of compromise blade can be considerably decreased due to the lower impact velocity, suitable impact angle and fewer impact times in comparison with that of the baseline blade. As a conclusion, it can be drawn that the proposed approach gives a further opportunity for turbomachinery anti-erosion design in consideration of other disciplines,and the methodology presented can be also applied to other turbomachinery and anti-erosion problem by a minor modification.

• 出版日期2014-2
• 单位西安交通大学