Regression Model for Civil Aero-engine Gas Path Parameter Deviations Based on Res-BP Neural Network

Xingjie Zhou, Xu-yun Fu, Minghang Zhao, S. Zhong
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引用次数: 1

Abstract

The gas path parameter deviations as crucial parameters can assist each airline to realize the performance state trend analysis, life prediction and fault diagnosis of aero-engine. However, the calculation of gas path parameter deviations is complicated and the calculation models are also mastered by the original equipment manufacturer (OEM), which makes it burdensome for airlines to independently analyze the gas path performance of the aeroengine. At present, airlines have accumulated a large number of samples of gas path parameter deviations, which makes it possible to establish a regression model between gas path parameters and its deviations by data-driven method. In order to enhance the analysis capability of airline in gas path performance, we apply the residual learning blocks to the back propagation (BP) neural network based on the learning mechanism of the residual networks (ResNets). According to the solution characteristics of gas path parameter deviations, the regression models for the gas path parameter deviations are established based on Res-BP neural network. The screening for nonlinear independent variables of regression model is carried out by mean impact value (MIV) method, and then the input and output of Res-BP neural network can be determined. After the regression model training, the test set is tested by the proposed regression model. By comparing with BP neural network regression model and traditional regression model, the proposed regression model manifests higher prediction accuracy and generalization performance on the three key gas path parameter deviations, which is of great guiding significance for the aero-engine condition monitoring.
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基于Res-BP神经网络的民用航空发动机气路参数偏差回归模型
气路参数偏差作为关键参数,可以帮助各航空公司实现航空发动机性能状态趋势分析、寿命预测和故障诊断。然而,气路参数偏差计算复杂,且计算模型又由原始设备制造商(OEM)掌握,这给航空公司独立分析航空发动机气路性能带来了很大的负担。目前航空公司已经积累了大量的气路参数偏差样本,这使得通过数据驱动的方法建立气路参数与其偏差之间的回归模型成为可能。为了提高航空公司气路性能的分析能力,基于残差网络的学习机制(ResNets),将残差学习块应用到BP神经网络中。根据气路参数偏差的求解特点,建立了基于Res-BP神经网络的气路参数偏差回归模型。采用平均影响值法对回归模型的非线性自变量进行筛选,从而确定Res-BP神经网络的输入和输出。回归模型训练完成后,对测试集进行回归模型测试。通过与BP神经网络回归模型和传统回归模型的比较,所提出的回归模型对三种关键气路参数偏差的预测精度和泛化性能均有所提高,对航空发动机状态监测具有重要的指导意义。
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