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The development of high performance hybrid joints between epoxy composites and PEEK/PPS composites: The mode-Ⅱ and mix mode-Ⅰ/Ⅱ fracture behaviour

机译:环氧树脂复合材料与PEEK/PPS复合材料高性能混合接头的开发:模式II.和混合模式I./II.。 断裂行为

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摘要

The development of effective methods for the bonding of Poly-etherether-ketone (PEEK) and Polyphenylenesulphide (PPS) composites to thermoset composites is appealing to expand their applications in aerospace industry. Herein, the surfaces of PEEK and PPS composites were treated by a high-power UV-irradiation technique for 6 s, that proved to significantly improve their intrinsically low surface activities. Carbon fibre reinforced epoxy composites were then directly cured onto the PEEK and PPS composites with or without an aerospace film adhesive at the joining interfaces. The mode-II and mix mode-I/II fracture behaviour of the hybrid joints were studied using an end notched flexural test and a fixed-ratio mixed-mode test, respectively. It was observed that the failure of the hybrid joints without adhesives mainly took place at the joining interfaces. In this case, the lack of resins at the fracture plane resulted in relatively low fracture toughness. Encouragingly, a cohesive failure was observed for the hybrid joints with adhesives in all the cases, owing to the enhanced adhesion between the adhesive and the PEEK/PPS composites upon the UV-treatment. This phenomenon indicated that optimal fracture resistance of the hybrid adhesive joints was obtained for the given material systems.
机译:聚醚醚酮(PEEK)和聚苯硫醚(PPS)复合材料与热固性复合材料粘接的有效方法的开发,正在扩大其在航空航天工业中的应用。本文采用高功率紫外辐照技术对PEEK和PPS复合材料的表面进行了6 s的处理,结果证明其表面活性显著降低。然后,将碳纤维增强环氧树脂复合材料直接固化到PEEK和PPS复合材料上,在连接界面处有或没有航空薄膜粘合剂。分别采用端部缺口弯曲试验和固定比率混合模式试验研究了混合节理的II.型断裂行为和I.II.型混合断裂行为。结果表明,无粘接剂的混合接头的失效主要发生在连接界面处。在这种情况下,断裂面上缺乏树脂导致断裂韧性相对较低。令人鼓舞的是,在所有情况下,由于粘合剂与PEEK/PPS复合材料之间的粘合力增强,在所有情况下,都观察到粘合剂的内聚失效。该现象表明,在给定的材料体系下,混合粘接接头的抗断裂性能最优。

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