中国安全科学学报 ›› 2026, Vol. 36 ›› Issue (6): 24-32.doi: 10.16265/j.cnki.issn1003-3033.2026.06.0711

• 安全技术与工程 • 上一篇    下一篇

考虑服役环境的RBF-ANN飞机襟翼结构损伤预测

张春晓1(), 闫春雨2, 邢志伟2, 冯博文3, 王芸2, 丛子棋4   

  1. 1 中国民航大学 民用航空器适航与维修重点实验室, 天津 300300
    2 中国民航大学 电子信息与自动化学院, 天津 300300
    3 沈阳北方飞机维修有限公司, 辽宁 沈阳 110170
    4 北京飞机维修工程有限公司, 北京 100020
  • 收稿日期:2026-01-21 修回日期:2026-04-14 出版日期:2026-06-28
  • 作者简介:

    张春晓 (1971—),女,青海西宁人,硕士,教授,主要从事民航统计预测与决策、民机可靠性评估及智能运维与维修优化等方面的研究。E-mail:

    邢志伟,教授

  • 基金资助:
    国家重点研发项目(2023YFB4302400); 研究生科研创新项目(2024YJSKC02006)

RBF-ANN damage prediction of aircraft flap structure considering service environment

Zhang Chunxiao1(), Yan Chunyu2, Xing Zhiwei2, Feng Bowen3, Wang Yun2, Cong Ziqi4   

  1. 1 Civil Aircraft Airworthiness and Maintenance Key Laboratory, Civil Aviation University of China, Tianjin 300300, China
    2 Faculty of Electronic Information and Automation, Civil Aviation University of China, Tianjin 300300, China
    3 Shenyang North Aircraft Maintenance, Shenyang Liaoning 110170, China
    4 Aircraft Maintenance and Engineering Corporation Beijing, Beijing 100020, China
  • Received:2026-01-21 Revised:2026-04-14 Published:2026-06-28

摘要:

为提升复杂服役环境下民用飞机襟翼复合材料结构损伤预测能力,提出一种融合服役环境信息的径向基函数(RBF)人工神经网络(ANN)预测方法。首先,构建涵盖结构维修记录与环境信息的多维运维数据库,采用灰色关联分析提取关键环境因子,实现服役环境定量表征,并通过聚类分析和方差分析识别损伤因素;然后,构建RBF-ANN预测模型,采用贝叶斯优化进行超参数调优,预测小样本条件下襟翼结构凹坑损伤深度;最后,通过消融试验和对比试验验证模型有效性。结果表明:贝叶斯优化显著提升模型性能,均方误差(MSE)和决定系数R2分别为0.031和0.962,优化后的模型在预测精度、误差控制及拟合能力方面均优于支持向量机(SVM)、长短期记忆网络(LSTM)及贝叶斯神经网络(BNN)等方法。

关键词: 服役环境, 径向基函数(RBF)-人工神经网络(ANN), 飞机襟翼, 结构损伤, 运维数据, 贝叶斯优化, 小样本

Abstract:

In order to improve the damage prediction ability of the composite structure of the civil aircraft flap in a complex service environment, a damage prediction method of the flap structure based on RBF-ANN considering the complex service environment was proposed. Firstly, a multi-dimensional operation and maintenance database covering structural maintenance information and corresponding environmental information was constructed. The key environmental factors were extracted by grey correlation analysis to realize the quantitative characterization of the service environment, and the damage factors were identified by cluster analysis and variance analysis. Secondly, the RBF-ANN model was constructed, and the hyperparameters of the RBF-ANN model were optimized by Bayesian optimization to realize the prediction of feature damage under the condition of small sample data. Finally, the effectiveness of the proposed model was verified by ablation experiments and comparative experiments. The results show that Bayesian optimization can significantly improve the performance of the model. Mean square error(MSE) and R2 of the model are 0.031 and 0.962, respectively. The optimized model is superior to support vector machine (SVM), long short-term memory network (LSTM) and Bayesian neural network (BNN) in prediction accuracy, error control and fitting ability.

Key words: service environment, radial basis function(RBF)-artificial neural network(ANN), aircraft flap, structure damage, operation and maintenance data, Bayesian optimization, small sample

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