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Failure Mechanisms and Reinforcing Modes of Ply Splice Fiber-Reinforced Composite Laminates under Tensile Load

机译:拉伸载荷下吡啶接头纤维增强复合材料层压材料的失效机理和增强模式

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摘要

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.
机译:为了制造大规模或异常形状的复合结构,可以拼接织物层以匹配尺寸和形状要求,形成帘布层剪接结构。不同层的连接可以被认为是所得复合材料中的缺陷,影响整体机械性能。本文用来用作研究对象的研究对象,以研究这些潜在的材料缺陷的单向碳纤维增强塑料(CFRP)。分析了在不同位置对CFRP拉伸性能的影响和层剪切位置的偶联的影响。同时,建立了有限元模型以分析损伤进化,其中使用连续损伤模型和粘性区域模型来描述复合材料和界面层的损坏。模型结果与观察到的实验结果吻合良好。我们的研究结果表明,这种失败机制有三个主要因素:边界效应,是否普利接头是独立的,或者它们是否彼此靠近。简而言之,当两个帘布层接头位于边缘或彼此独立时,失效模式是首先分层,然后是纤维骨折,并且拉伸强度高。然而,当两个帘布层接头接近边缘或彼此接近时,失效模式是首先是局部纤维裂缝,然后是分层损坏,并得到的拉伸强度低。最后,通过通过模型模拟通过分析,采用不同位置处的拼接层采用不同的增强方法来改善复合材料的拉伸性能。双侧贴片修复方法用于在边缘或附近加强帘布层。另外,使用粘合剂层的韧性来增强材料内部的帘布层。这些结果表明,通过这两种增强方法增强了拉伸强度,初始损伤载荷特别升高。

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