Time-dependent reliability optimisation for retraction mechanism with multiple clearance joints under wear

Abstract Under the coupling effect of node position deviation, joint clearance and wear factors, the complex landing gear retraction mechanism suffers from low kinematic accuracy, slow retraction performance and shortened reliable life. Addressing these issues, a time-dependent reliability analysis and optimisation design method for the kinematic accuracy of the retraction mechanism is proposed, considering the uncertainty of node position deviation, initial clearance, and dynamic multi-joint wear. Initially, a wear prediction model and a dynamic model of the retraction mechanism considering node position deviation and joint clearance are established to analyse their influence on retraction accuracy and joint wear depth. Subsequent retraction testing under various working conditions is conducted to ascertain the critical failure condition and validate the simulation model. The time-dependent kinematic accuracy reliability model, accounting for the dynamic evolution of wear clearance, is then established to assess reliability variation with retraction cycles. Finally, the reliability optimisation design focusing on hole-axis matching accuracy aims to strike a balance between accuracy cost and reliability, thereby enhancing performance and prolonging operational life.

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Publication Details

Journal
The Aeronautical Journal
Published
2025-04-16
DOI
https://doi.org/10.1017/aer.2025.20
Primary Topic
Gear and Bearing Dynamics Analysis
Type
article
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article

Time-dependent reliability optimisation for retraction mechanism with multiple clearance joints under wear

Yumeng Yan, Jiyuan Zhou, Xian Wei, Taotao Liang et al.
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The Aeronautical Journal
Gear and Bearing Dynamics Analysis
article

Time-dependent reliability optimisation for retraction mechanism with multiple clearance joints under wear

Yumeng Yan, Jiyuan Zhou, Xian Wei, Taotao Liang, Yin Yin, Hong Nie
article en

Abstract

Abstract Under the coupling effect of node position deviation, joint clearance and wear factors, the complex landing gear retraction mechanism suffers from low kinematic accuracy, slow retraction performance and shortened reliable life. Addressing these issues, a time-dependent reliability analysis and optimisation design method for the kinematic accuracy of the retraction mechanism is proposed, considering the uncertainty of node position deviation, initial clearance, and dynamic multi-joint wear. Initially, a wear prediction model and a dynamic model of the retraction mechanism considering node position deviation and joint clearance are established to analyse their influence on retraction accuracy and joint wear depth. Subsequent retraction testing under various working conditions is conducted to ascertain the critical failure condition and validate the simulation model. The time-dependent kinematic accuracy reliability model, accounting for the dynamic evolution of wear clearance, is then established to assess reliability variation with retraction cycles. Finally, the reliability optimisation design focusing on hole-axis matching accuracy aims to strike a balance between accuracy cost and reliability, thereby enhancing performance and prolonging operational life.

The Aeronautical JournalVol. 129(1339)
Shanghai Special Equipment Supervision and Inspection Institute (CN), Nanjing University of Aeronautics and Astronautics (CN)
Openalex Percentile: Top 93%
Gear and Bearing Dynamics Analysis
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Time-dependent reliability optimisation for retraction mechanism with multiple clearance joints under wear — Yumeng Yan, Jiyuan Zhou, et al. · The Aeronautical Journal (2025) | TGRS Research Map | TGRS