Abstract:A Bayesian method for estimating the initial crack length distribution is proposed for probabilistic risk analysis (PRA) of repaired structural details. Noninformative prior is updated using a likelihood function, which is constructed using inspection capability, structural geometry, and material properties. The likelihood function based on the equivalent initial flaw size method was used for the left tail to avoid calculating the small-crack growth. The right tail was estimated based on the inspection capabil… Show more
“…11,12,16 Based on the initial crack length distribution and inspection reliability, a repair crack length distribution was estimated for node a r by using the Bayesian method proposed in the work of one of the present authors. 25 Figure 10 shows the repair crack length distribution applied.…”
Using a dynamic Bayesian network (DBN) to estimate the failure risk of a component or system that deteriorates with time has several advantages. A DBN discretizes the probability distribution of variables and thereby increases the efficiency of computing resources and reduces computation time. However, it is important to devise an optimal discretization scheme because the size of the model grows exponentially as the number of discretized intervals increases. In this paper, we propose an optimal discretization scheme for a DBN used to model the time-varying deterioration of a turbine blade component. The results of estimating the reliability indices with the DBN were verified by comparing them with the results of a Monte Carlo simulation. In addition, compared with a log-transformed discretization method, our DBN discretization method shows a significantly increased computation speed.
“…11,12,16 Based on the initial crack length distribution and inspection reliability, a repair crack length distribution was estimated for node a r by using the Bayesian method proposed in the work of one of the present authors. 25 Figure 10 shows the repair crack length distribution applied.…”
Using a dynamic Bayesian network (DBN) to estimate the failure risk of a component or system that deteriorates with time has several advantages. A DBN discretizes the probability distribution of variables and thereby increases the efficiency of computing resources and reduces computation time. However, it is important to devise an optimal discretization scheme because the size of the model grows exponentially as the number of discretized intervals increases. In this paper, we propose an optimal discretization scheme for a DBN used to model the time-varying deterioration of a turbine blade component. The results of estimating the reliability indices with the DBN were verified by comparing them with the results of a Monte Carlo simulation. In addition, compared with a log-transformed discretization method, our DBN discretization method shows a significantly increased computation speed.
“…Boris et al [22] introduced a framework utilizing a DBN with MCMC for predicting and updating crack length in fatigued structural components, including parameter probability density identification and updating. Lee et al [23] proposed a Bayesian method to estimate initial crack length distribution for PRA of repaired structures, improving parameter selection and analyzing KT-1 aircraft repair risk.…”
Monitoring the health status of aerospace structures during their service lives is a critical endeavor, aimed at precisely evaluating their operational condition through observation data and physical modeling. This study proposes a probabilistic assessment approach utilizing Dynamic Bayesian Networks (DBNs), enhanced by an improved adaptive particle filtering technique. This approach combines physical modeling with various predictive sources, encompassing cognitive uncertainties inherent in stochastic predictions and crack propagation forecasts. By employing crack observation data, it facilitates predictions of crack growth and the residual life of metal structure. To demonstrate the efficacy of this method, the research leverages data from three-point bending and single-edge tension fatigue tests. It gathers data on crack length during the fatigue crack progression, integrating these findings with digital twin theory to forecast the residual fatigue life of the specimens. The outcomes show that the adaptive DBN model can precisely predict fatigue crack propagation in test specimens, offering a potential tool for the online health assessment and life evaluation for aerospace structures.
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