摘要
This research first proposed a new aerodynamic optimization method that using machine learning XGBoost algorithm as the regression model, and global optimization algorithm MaxLIPO Trust Region method as the optimization method on regression model. In order to ensure the accuracy of the regression model near the optimal value, a dynamic recognition add point method is used to construct a dynamically updated regression model, and a double convergence criterion is used to determine the convergence of the optimization process. After constructing the optimization process, a new type of weight reduction high-pressure turbine blade was optimized. The results show that the optimization process can achieve rapid and effective optimization of aerodynamic performance compared to traditional optimization methods, and the regression prediction accuracy near the optimal value reaches a level with a minimum error from the CFD result. Meanwhile, the influence weight factor of geometrical parameters on the aerodynamic performance could be analyzed. Finally, the effective aerodynamic optimization design of the weight reduction turbine blade is achieved.
- 单位