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Publishing Language: Chinese

Structural reliability design for aero-engines: Review and prospects

Xi LIU1,2,3, Dianyin HU2,3,4( ), Yi WANG4, Rongqiao WANG1,2,3, Gaoxiang CHEN2,3,4, Weihan KONG1
School of Energy and Power Engineering, Beihang University, Beijing 100191, China
Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing 100191, China
United Research Center of Mid-Small Aero-Engine, Beijing 100191, China
Research Institute of Aero-Engine, Beihang University, Beijing 100191, China
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Abstract

This paper reviews the current state of research on structural reliability design for aero-engines. It discusses the recent advances, challenges, and development trends from several key perspectives, including reliability design process reliability metric analysis, the sources and characterization of uncertainties affecting structural reliability, reliability metrics, structural reliability analysis methods, and reliability-based design optimization techniques. Despite notable progress, the practical application of structural reliability design methods in engineering remains challenging. Ongoing research is needed in areas such as multi-source uncertainty modeling and propagation, data-driven and intelligent optimization, reliability testing and validation, and Model-Based Systems Engineering (MBSE)-based reliability design. The goal is to establish a new generation of reliability design systems characterized by data-driven approaches, model-centric integration, and the fusion of simulation and physical testing, thereby supporting the coordinated improvement of structural reliability, performance, and design efficiency in aero-engines.

CLC number: V232 Document code: A Article ID: 1000-6893(2025)21-532625-25

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
LIU X, HU D, WANG Y, et al. Structural reliability design for aero-engines: Review and prospects. Acta Aeronautica et Astronautica Sinica, 2025, 46(21). https://doi.org/10.7527/S1000-6893.2025.32625

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Received: 24 July 2025
Revised: 19 August 2025
Accepted: 08 September 2025
Published: 12 September 2025
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica