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Optimization of cure profile for thick composite parts based on finite element analysis and genetic algorithm

机译:基于有限元分析和遗传算法的厚复合部件固化谱的优化

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摘要

Cure process is the most crucial stage for manufacturing composite parts and final quality of the part is strongly dependent on the cure profile used in the curing process. In this paper, a novel approach based on cure simulation using finite element method and multi-objective genetic algorithm is developed to optimize cure profile for thick thermoset composites. Three objectives are considered simultaneously, which include the maximum difference in degree of cure, the maximum temperature difference, and the total cure time. Optimal Pareto front is obtained and the optimized cure profile is selected from Pareto front for the given application. A 24-mm thick unidirectional laminate is taken as an example and the results show that compared to typical cure profile, the optimized cure profile leads to approximately 56% reduction in the maximum difference in degree of cure, 71% decrease in the maximum difference in temperature during cure, and 33% reduction in the total cure time. It is also indicated that the residual stress can be remarkably decreased and the cure efficiency is significantly improved using the present method. The present method can also be applied to various geometries with various thicknesses and is able to provide an important reference for determination of cure profiles for the manufacturing of composite structures.
机译:固化过程是制造复合材料部件中最关键的阶段,部分质量依赖于固化过程中使用的固化曲线。本文开发了一种基于使用有限元方法和多目标遗传算法的固化模拟的新方法,以优化厚热固性复合材料的固化曲线。同时考虑三个目标,包括固化程度,最大温度差和总固化时间的最大差异。获得最佳Pareto前线,并且优化的固化曲线选自Pareto前面,用于给定的应用。以24毫米厚的单向层压体为例,结果表明,与典型的固化曲线相比,优化的固化型材导致固化程度的最大差异约为56%,最大差异减少71%固化过程中的温度,总固化时间减少了33%。还表明,使用本方法,可以显着降低残余应力,并且使用本方法显着改善固化效率。本方法也可以应用于具有各种厚度的各种几何形状,并且能够提供用于确定用于制造复合结构的固化型材的重要参考。

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