加工误差对压气机叶栅气动性能及稳定性影响的数据挖掘

To alleviate the 'dimension disaster' in the process of evaluating the impact of manufacturing errors, combining the spanwise average assumption and the Karhunen-Loève expansion based on the Gaussian process, a reduced order model of normal manufacturing errors on three-dimensional blade surface geometric variability was proposed. The reduced order model on geometric variability was solved by the standard deviation function of the given manufacturing error distribution, the Pseudo-Monte Carlo method was used to randomly generate samples, and the Artificial Neural Network was trained to predict the impact of manufacturing error on the aerodynamic performance and corner aerodynamic stability of a high-load linear cascade. The results show that the effects of manufacturing errors are related to the working conditions. Under the near stall conditions, compared with the nominal, the mean aerodynamic performance and stability decrease, the probability that the total pressure loss coefficient increases is about 83.29%, the probability that the static pressure coefficient decreases is about 79.20%, and the probability that the stall indicator increases is about 69.10%. Compared with the design conditions, the variability of aerodynamic stability under the near stall conditions increases, and the aerodynamic stability is more sensitive to manufacturing errors. The total pressure loss coefficient, static pressure coefficient and stall indicator are monotonously related to each other. The manufacturing error of the leading edge and suction surface profile has a greater impact on the loss, and the corresponding geometric accuracy should be further focused on.