基于RTM-预浸料工艺的数值模拟与固化制度优化OA
Simulation and optimization based on RTM-prepreg process
RTM-预浸料工艺界面处预浸料和树脂固化的不同步导致了明显的固化度梯度,使得界面力学性能下降,但是目前少有共固化过程的数值模拟和对其固化制度的探索.基于环氧树脂和碳纤维/环氧树脂预浸料的固化动力学模型,利用ABAQUS软件的二次开发对共固化过程进行数值模拟,从而优化工艺曲线参数,使界面处两种材料同步固化,并通过短梁剪切试验和双悬臂梁试验验证了模拟结果的可靠性.结果表明:界面的两种材料存在放热耦合作用,但对界面材料的固化影响很小;在不同固化制度下,层合板界面层短梁剪切强度和Ⅰ型层间断裂韧性均优于预浸料层相应值,且采用以约5 ℃/min的升温速率升温至180 ℃保温2 h的固化制度,层合板力学性能更优.研究结果对实际生产具有一定的指导意义.
The unsynchronized curing of prepreg and resin at the interface of RTM-prepreg process results in an obvious curing gradient,which reduces the mechanical properties of the interface.However,there are few studies on the co-curing process simulation and co-curing process curve.In this study,the mathematical models of the curing kinetics of epoxy resin and carbon fiber/epoxy resin prepreg were established,and the co-curing process was simu-lated by user-defined subroutine of ABAQUS software.The parameters of temperature profile such as heating rate,holding time,and holding temperature were optimized to simultaneous curing of the two materials at the interface.Fi-nally,the reliability of the simulation results was verified by short beam shear experiments and double cantilever beam experiments.The results show that the two materials at the interface have exothermic coupling,but have little effect on the resin curing of the interface materials.The short beam shear strength and mode Ⅰ interlaminar fracture toughness of the interface of the laminate are better than those of the prepreg layer under different curing curve.When the tem-perature profile is about 5 ℃/min,the temperature is raised to 1 80 ℃ and kept for 2 hours,the mechanical proper-ties of laminates are better than those of other curing curve.It has certain guiding significance for actual production.
陈婕;谢金鑫;彭飞;张峰嘉;许林鹏;周何乐子;周华民
华中科技大学材料科学与工程学院,武汉 430074北京宇航系统工程研究所,北京 100076北京宇航系统工程研究所,北京 100076华中科技大学材料科学与工程学院,武汉 430074华中科技大学材料科学与工程学院,武汉 430074华中科技大学材料科学与工程学院,武汉 430074华中科技大学材料科学与工程学院,武汉 430074
通用工业技术
RTM-预浸料工艺共固化数值模拟优化试验验证
RTM-prepreg processco-curingsimulationoptimizedexperimental validation
《复合材料科学与工程》 2026 (1)
82-91,140,11
民用航天预研项目(D030102)
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