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首页> 外文期刊>International Journal of Adhesion & Adhesives >Mode II interfacial fracture toughness of composite/adhesive interfaces obtained by in-mold surface modification
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Mode II interfacial fracture toughness of composite/adhesive interfaces obtained by in-mold surface modification

机译:通过模内表面改性获得的复合材料/胶粘剂界面的II型界面断裂韧性

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In order to conduct surface modification more effectively, we have investigated the in-mold surface modification technique for composite surface that uses microstructures fabricated by imprint lithography. In the present study, we performed end notched flexure (ENF) tests to evaluate the resistance to crack propagation under macroscopic mode II loading at the modified carbon fiber reinforced plastic (CFRP)/adhesive interfaces by comparing the behaviors of brittle adhesives and ductile adhesives. In addition, we also investigated the influence of the aspect ratios (A) of the microstructures on the fracture toughness. From the ENF tests and microscopic observation of crack propagation, the mode 11 interfacial fracture toughness (G_(IIC)) of the modified surfaces were found to be improved than that of flat surfaces regardless of applied adhesives. In the case of applying Epoxy A (3M DP-100 clear), which has a Young's modulus that is approximately 6.56 times higher and a mode 1 fracture toughness that is 1.34 times higher than Epoxy B (3M DP-105 clear), the cohesive failures of the CFRP concavo-convex microstructures occurred in addition to the microscopic interfacial failures during mode II loading. In addition, G_(IIC) showed an almost constant value regardless of aspect ratio A. Thus, the interfacial fracture toughness of CFRP/Epoxy A was comparatively low compared to the CFRP cohesive failure, and the substantial crack length was almost constant, regardless of A, because the crack penetrated the concavo-convex microstructures. In the case of applying Epoxy B (3M DP-105 clear), the crack propagated along the CFRP/Epoxy B interface, including the plastic deformation of Epoxy B. Therefore, G_(IIC) increased with an increase in A. Thus, we concluded that the substantially increased crack length was mainly influenced by the interfacial fracture toughness of CFRP/Epoxy A, which was comparatively higher than the cohesive failure of Epoxy B.
机译:为了更有效地进行表面改性,我们研究了模内表面改性技术,该技术利用压印光刻技术制造的微结构对复合材料表面进行了改性。在本研究中,我们通过比较脆性胶粘剂和延性胶粘剂的行为,进行了端部切口挠曲(ENF)测试,以评估在宏观模式II载荷下改性碳纤维增强塑料(CFRP)/胶粘剂界面处的裂纹扩展阻力。此外,我们还研究了微观结构的长径比(A)对断裂韧性的影响。通过ENF测试和裂纹扩展的微观观察,发现无论使用何种粘合剂,改性表面的11型界面断裂韧度(G_(IIC))均比平坦表面有所改善。在使用环氧树脂A(3M DP-100透明)时,其杨氏模量大约是环氧树脂B(3M DP-105透明)的约6.56倍,并且其模式1断裂韧性比环氧树脂B(3M DP-105透明)高1.34倍。在模式II加载期间,除了微观界面破坏外,还发生了CFRP凹凸微结构的破坏。此外,G_(IIC)的值几乎不受常数A的影响。因此,与CFRP的内聚破坏相比,CFRP /环氧树脂A的界面断裂韧性较低,并且不论A,因为裂纹穿透了凹凸的微观结构。在使用环氧树脂B(3M DP-105透明)的情况下,裂纹沿着CFRP /环氧树脂B界面扩展,包括环氧树脂B的塑性变形。因此,G_(IIC)随着A的增加而增加。得出的结论是,裂纹长度的显着增加主要受CFRP /环氧树脂A的界面断裂韧度的影响,该断裂韧度比环氧树脂B的内聚破坏性要高。

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