航空学报 > 2026, Vol. 47 Issue (7): 232500-232500   doi: 10.7527/S1000-6893.2025.32500

固体力学与飞行器总体设计

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基于诊断与预测的金属搭接结构动态风险评估

韩亮, 贺小帆()   

  1. 北京航空航天大学 航空科学与工程学院 强度与结构完整性全国重点实验室,北京 102206
  • 收稿日期:2025-07-01 修回日期:2025-08-20 接受日期:2025-09-10 出版日期:2025-09-19 发布日期:2025-09-18
  • 通讯作者: 贺小帆
  • 基金资助:
    国家自然科学基金(12472341)

Dynamic risk assessment of metallic lap-joint structures based on diagnosis and prognosis

Liang HAN, Xiaofan HE()   

  1. National Key Laboratory of Strength and Structural Integrity,School of Aeronautics Science and Engineering,Beihang University,Beijing 102206,China
  • Received:2025-07-01 Revised:2025-08-20 Accepted:2025-09-10 Online:2025-09-19 Published:2025-09-18
  • Contact: Xiaofan HE
  • Supported by:
    National Natural Science Foundation of China(12472341)

摘要:

针对金属搭接结构隐藏裂纹难检、传统风险评估高度依赖离线无损检测的问题,基于数字孪生框架提出了一种诊断-预测一体的动态风险评估方法。该方法以实测应变驱动物理-数据融合的裂纹扩展模型,并建立动态贝叶斯网络实现虚实闭环;通过CUSUM检测裂纹存在、KNN定位裂纹位置、MOGPR识别裂纹尺寸,结合DBN实时更新裂纹扩展参数Cm。在此基础上,采用蒙特卡洛仿真计算SFPOF。试验结果表明:CUSUM-SFPOF联合判据能及时实现裂纹预警,降低对高精度EIFS的依赖;随着监测数据累积,参数Cm标准差逐渐降低,寿命预测不确定性降低。该方法可实现金属搭接结构持续在线风险量化评估,为结构视情维护提供可靠支撑。

关键词: 风险评估, 结构故障诊断与健康管理, 疲劳损伤诊断与预测, 单次飞行失效概率, 裂纹扩展

Abstract:

Hidden cracks in metallic lap-joint structures are difficult to detect, and conventional risk assessment methods rely heavily on offline nondestructive inspections. To address these challenges, an integrated diagnosis and prognosis dynamic risk assessment method within a digital twin framework has been proposed. The method employs an experimental strain driven physics and data fusion crack propagation model and implements a dynamic Bayesian network to close the loop between virtual and physical models. Crack initiation is detected using the Cumulative Sum Control Chart (CUSUM) algorithm; crack location is determined by a k-Nearest Neighbors (KNN) classifier; crack size is estimated through a Multi-Output Gaussian Process Regression (MOGPR) model; subsequently, a Dynamic Bayesian Network (DBN) is employed to dynamically update the crack propagation parameters C and m in real time. Based on these updated parameters, the Single Flight Probability of Failure (SFPOF) is computed through Monte Carlo simulation. Experimental results demonstrate that the combined CUSUM and SFPOF criterion provides timely crack warnings and reduces dependence on high-precision Equivalent Initial Flaw Size (EIFS). As monitoring data accumulate, the standard deviations of C and m decrease, lowering uncertainty in life predictions. The proposed method enables continuous online quantitative risk evaluation of metallic lap-joint structures, offering reliable support for condition-based maintenance decisions.

Key words: risk assessment, structural fault diagnosis and health management, fatigue damage diagnosis and prognosis, single flight probability of failure, crack propagation

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