Zhu Meng, Chen Dingding, Hu Qigao
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410000, China.
College of Military Basic Education, National University of Defense Technology, Changsha 410000, China.
Materials (Basel). 2019 Sep 9;12(18):2912. doi: 10.3390/ma12182912.
To fabricate large-scale or unusually shaped composite structures, pieces of fabric plies can be spliced to match size and shape requirements, forming ply splice structures. The junction of different plies can be considered as a defect in the resulting composite material, affecting the overall mechanical properties. In this paper, unidirectional carbon fiber-reinforced plastic (CFRP) with ply splices was used as a research object to study these potential material defects. The effects of ply splices at different positions on the tensile properties of CFRP and the coupling between position of ply splicing were analyzed. Simultaneously, a finite element model was established to analyze the damage evolution, in which a continuous damage model and a cohesive zone model were used to describe the damage of the composite and interface layers, respectively. The model results were in good agreement with observed experimental results. Our results showed that there were three main factors for this failure mechanism: boundary effects, whether the ply splices were independent, or whether they were close to each other. In short, when two ply splices were located at the edge or independent of each other, the failure mode was first delamination and then fiber fracture, and the tensile strength was high. However, when the two ply splices were close to the edge or close to each other, the failure mode was first local fiber fracture and then delamination damage, and the resulting tensile strength was low. Finally, different reinforcement methods to improve the tensile properties of composites were adopted for the splicing layers at different positions through the analysis via model simulation. The two-side patch repair method was used to reinforce the ply splices on or near the edge. Additionally, increasing the toughness of the adhesive layer was used to reinforce the ply splices that were inside the material. These results showed that the tensile strength was enhanced by these two methods of reinforcement, and the initial damage load was especially increased.
为了制造大规模或形状异常的复合材料结构,可以将织物层片拼接起来以满足尺寸和形状要求,从而形成层片拼接结构。不同层片的接合处可被视为所得复合材料中的缺陷,会影响整体力学性能。本文以具有层片拼接的单向碳纤维增强塑料(CFRP)为研究对象,研究这些潜在的材料缺陷。分析了不同位置的层片拼接对CFRP拉伸性能的影响以及层片拼接位置之间的耦合作用。同时,建立了有限元模型来分析损伤演化,其中分别使用连续损伤模型和内聚区模型来描述复合材料层和界面层的损伤。模型结果与实验观测结果吻合良好。我们的结果表明,这种失效机制主要有三个因素:边界效应、层片拼接是否独立或彼此是否靠近。简而言之,当两个层片拼接位于边缘或彼此独立时,失效模式为先分层后纤维断裂,拉伸强度较高。然而,当两个层片拼接靠近边缘或彼此靠近时,失效模式为先局部纤维断裂后分层损伤,所得拉伸强度较低。最后,通过模型模拟分析,针对不同位置的拼接层采用了不同的增强方法来提高复合材料的拉伸性能。采用双面贴片修复方法对边缘或边缘附近的层片拼接进行增强。此外,通过提高粘结层的韧性来增强材料内部的层片拼接。这些结果表明,这两种增强方法提高了拉伸强度,尤其提高了初始损伤载荷。