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Publishing Language: Chinese

Uncertainty technologies in aircraft digital strength twins

Yifei WANGGeyong CAOYang CAOXiaojun WANG( )
National Key Laboratory of Strength and Structural Integrity, Institute of Solid Mechanics, Beihang University, Beijing 102206, China
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Abstract

The rapid development of the aviation industry has introduced triple challenges-timeliness, precision, and intelligence-for next-generation aircraft's full lifecycle management (design, manufacturing, and operation/maintenance). As an enabling technology of the Fourth Industrial Revolution, digital twin has emerged as a core solution for aircraft structural health monitoring and performance prediction, leveraging its real-time interactivity, multi-source heterogeneous data fusion, and high-fidelity modeling capabilities. However, multi-source uncertainties-including material property dispersion during aircraft development, manufacturing tolerances, and in-service structural accidental damage or complex load disturbances-pose significant challenges to the credibility of aircraft digital strength twins. This paper addresses multidimensional uncertainty issues across an aircraft's full lifecycle (design verification, production, operation, and maintenance) while incorporating key technical requirements such as high-precision load identification and high-confidence structural damage diagnosis. It proposes a conceptual framework and technical architecture for aircraft digital strength twins. To enable the engineering implementation of digital strength twin systems, we systematically organize critical technologies including distributed sensor network construction, high-performance computing platform integration, multi-source data fusion, and dynamic model updating, which provide robust hardware/software foundations for engineering applications and efficient uncertainty resolution. Guided by core requirements for interactive real-time performance, model fidelity, and analytical refinement, this study takes uncertainty-driven digital strength twin entities as its research focus. It conducts in-depth analyses of uncertainty propagation mechanisms, key technical pathways, and future development directions across three core processes: load twin, structural damage state twin, and mechanical behavior/performance twin.

CLC number: V215 Document code: A Article ID: 1000-6893(2025)19-532408-44

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
WANG Y, CAO G, CAO Y, et al. Uncertainty technologies in aircraft digital strength twins. Acta Aeronautica et Astronautica Sinica, 2025, 46(19). https://doi.org/10.7527/S1000-6893.2025.32408

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Received: 12 June 2025
Revised: 30 June 2025
Accepted: 21 July 2025
Published: 28 July 2025
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica