Aug 2026· 2026 8th International Conference on System Reliability and Safety Engineering (SRSE)· pp. 96-103· 0 citations· 13 references
Abstract
Traditional safety factor design adopts empirical fixed values, leading to unnecessary structural redundancy and failing to quantify failure probability. Monte Carlo Simulation (MCS) brings extremely high computational costs, while existing methods cannot fully optimize the relationship among machining tolerance, manufacturing cost and safety factor. To address these issues, this paper presents a refined design method combining Optimal Latin Hypercube Design, PSO-BP neural network surrogate model and African Vultures Optimization Algorithm (AVOA). The PSO-BP model replaces time-consuming finite element simulations. Combined with stress-strength interference theory considering confidence levels, an optimization model is established with machining tolerance as design variables and manufacturing cost as well as reliability as constraints, and solved via AVOA. The results show that under cost limits and high reliability requirements, load-carrying stability is improved by approximately 22.5 percent. The optimized safety factor is 1.03068, a reduction of 26.38 percent compared with the traditional value of 1.4. The proposed method realizes optimal tolerance allocation and structural lightweighting under manufacturing cost constraints.
Retaining walls are designed today with two objectives in mind: construction cost and embodied carbon, while the ground properties that govern their safety are known only in distribution. Treating both requirements at once yields a reliability-constrained multi-objective problem whose nested Monte Carlo evaluation is e...
Reducing structural weight in commercial aviation is a primary challenge for efficiency. This study introduces a design framework optimizing a Fowler flap bracket using topology optimization (TO) tailored for additive manufacturing (AM) constraints. Rather than expensive fluid simulations, the methodology utilizes anal...
M. Bayrak, Okan Bakbak· Journal of Polytechnic· 0 citations
Composite materials have become widespread for use in aircraft load bearing structures due to their ability of reducing structural mass without compromising the required stiffness, strength and safety requirements in the face of aerodynamic, inertial and thermal service loads. This work has addressed with success the d...
Hao-Ming He· SAE technical paper series· 0 citations
Composite patch repair has emerged as an effective technique for extending the service life of cracked metallic structures by reducing crack-tip stress intensity and avoiding costly component replacement. However, identifying an optimal repair configuration remains challenging because minimizing both the stress intensi...
Nadjib Kacemi, Reda Yahiaoui· Journal of composite materia...· 0 citations
This paper presents a two-stage, deterministic optimization procedure for designing economical reinforcement layouts in Mechanically Stabilized Earth (MSE) walls. The method builds on a conventional analysis engine that performs internal stability checks (e.g., per AASHTO-type codes) and global stability using Limit Eq...
Cristian Salvalaggio, S. Javankhoshdel, Carlos Rodriguez et al.· E3S Web of Conferences· 0 citations
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