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Publishing Language: Chinese

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

Liang HANXiaofan HE( )
National Key Laboratory of Strength and Structural Integrity, School of Aeronautics Science and Engineering, Beihang University, Beijing 102206, China
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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.

CLC number: V215.5 Document code: A Article ID: 1000-6893(2026)07-232500-21

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
HAN L, HE X. Dynamic risk assessment of metallic lap-joint structures based on diagnosis and prognosis. Acta Aeronautica et Astronautica Sinica, 2026, 47(7). https://doi.org/10.7527/S1000-6893.2025.32500

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Received: 01 July 2025
Revised: 20 August 2025
Accepted: 10 September 2025
Published: 19 September 2025
© 2026 The Journal of Acta Aeronautica et Astronautica Sinica