首页|期刊导航|Aerospace Traffic and Safety|Research on reliability assessment method of harbinger solenoid valves based on multi-physics field coupled degradation

Research on reliability assessment method of harbinger solenoid valves based on multi-physics field coupled degradationOA

中文摘要

In response to the insufficient research on the multi-physics coupling degradation mechanisms of solenoid valves,a dual-factor coupled reliability model integrating spring stiffness degradation and seal leakage degradation is proposed.A nonlinear exponential decay with environmental compensation model(EDECM)is established to characterize the time-varying spring stiffness,and A Triple-Stage Fractal Contact Degradation Model(TSFCDM)is constructed based on fractal contact theory to describe the seal leakage degradation.Additionally,Wiener processes are introduced to depict the stochastic fluctuations of parameters.Monte Carlo simulations reveal that the reliability of the solenoid valve first drops to the 0.999 threshold within 296,000 usage cycles,with significant dispersion in the failure threshold distribution due to parameter uncertainties.Compared with traditional single-factor models,this coupled model effectively reduces prediction deviations by quantifying the bidirectional degradation mechanisms,meeting the precision requirements for the reliability threshold(>0.999)of aeronautical equipment.

Shiyun Zhang;Zhigeng Fang;Chengjie Zhang;Yifan Yang;Shuyu Xiao;Zhi Sun

College of Economics and Management,Nanjing University of Aeronautics and Astronautics,ChinaCollege of Economics and Management,Nanjing University of Aeronautics and Astronautics,ChinaCollege of Economics and Management,Nanjing University of Aeronautics and Astronautics,ChinaCollege of Economics and Management,Nanjing University of Aeronautics and Astronautics,ChinaCollege of Economics and Management,Nanjing University of Aeronautics and Astronautics,ChinaKey Laboratory of Civil Aviation Emergency Science&Technology,CAAC,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China

航空航天

Reliability assessmentAerospace solenoid valves Multi-physics couplingCoupled degradation mechanismsStochastic process modelingFailure threshold analysis

《Aerospace Traffic and Safety》 2025 (3)

P.137-144,8

financially supported by supported by Shanghai Central Guidance Science and Technology Development Fund(NO:YDZX20233100004008)National Natural Science Foundation of China(NO:T2441003)。

10.1016/j.aets.2025.10.003

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