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Probabilistic Maintenance-Free Operating Period via Bayesian Filter with Markov Chain Monte Carlo (MCMC) Simulations and Subset Simulation

机译:通过贝叶斯滤波器的概率维护运行期通过Markov链蒙特卡罗(MCMC)模拟和子集模拟

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This paper presents a probabilistic approach via Bayesian-filter (BF) with Markov chain Monte Carlo (MCMC) simulations and subset simulation (SS), to determine the probabilistic maintenance-free operating period (MFOP) for probabilistic lifing assessment of aircraft fatigue critical components. State transition function representing virtual damage growth of a component and measurement function representing the SHM measurements of the component are defined. State transition function is described by a typical Paris equation for fatigue crack propagation. Measurement functions are assumed in this study, which describe the relationship between the damage features derived from SHM signals and the damage sizes. Damage tolerance (DT) and risk-based methodologies are used for fracture-based reliability assessment. Random samples for posterior joint probability density function of initial flaw size and crack growth rate are generated with information obtained through structural health monitoring (SHM) systems. Subset simulation (SS) is used in conjunction with MCMC in order to determine the small probability of failure with high efficiency. The results have shown that the MCMC-SS combined methodology is two orders of magnitude more efficient than that of MCMC alone.
机译:本文介绍了Markov链蒙特卡罗(MCMC)模拟和子集仿真(SS)的贝叶斯滤波器(BF)的概率方法,以确定飞机疲劳关键部件的概率提升评估的概率维护运行期(MFOP) 。定义了表示组件和测量函数的虚拟损伤的状态转换功能,表示代表组件的SHM测量值。状态转换功能由诸如疲劳裂纹传播的典型的巴黎方程描述。在本研究中假设测量功能,这描述了从SHM信号导出的损坏特征与损坏尺寸之间的关系。损伤耐受性(DT)和基于风险的方法用于基于裂缝的可靠性评估。通过通过结构健康监测(SHM)系统获得的信息,产生用于后关节概率密度函数的随机样品初始缺陷尺寸和裂纹生长速率。子集仿真(SS)与MCMC一起使用,以便以高效率确定故障的小概率。结果表明,MCMC-SS组合方法是单独效率的两个数量级,而不是单独的MCMC。

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