Research on damage repair and high-velocity impact characteristics of thermoplastic composites

被引:1
作者
Jin, Feng [1 ]
Liu, Lulu [1 ]
Zhu, Xinying [1 ]
Xie, Zhihao [1 ]
Chen, Wei [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Aeroengine Thermal Environm & Struct Key Lab, Minist Ind & Informat Technol, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
Thermoplastic composites; Low-velocity impact damage; Compressive strength; Ballistic limit; Thermal repair; INTERFACE; POLYMERS; BEHAVIOR;
D O I
10.1016/j.tws.2024.112663
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Low-velocity impact (LVI) can result in imperceptible damage to carbon fiber reinforced thermoplastic composites (CFRTP) laminates during service, leading to a reduction in structural strength. The thermal repair of damaged CFRTP laminates is conducted using the repairability of thermoplastic resin at high temperatures. However, the high-velocity impact characteristics of CFRTP laminates following thermal repair remain uncertain. This study examines CFRTP laminates made of two different materials (CF/PEEK and CF/PPS) with varying levels of low-velocity impact damage, and investigates the thermal repair process. A comparative experimental analysis examined the high-speed impact characteristics of CFRTP laminates under varying conditions. The results indicate that CF/PEEK laminates consistently exhibit superior compressive properties and impact resistance compared to CF/PPS laminates under similar conditions. Following damage from low-velocity impact, the compressive properties and high-velocity impact resistance of CFRTP laminates decrease, with CF/PPS laminates typically showing a lower performance retention rate. However, the thermal repair process proposed in this study significantly enhances the performance of CF/PPS laminates. Moreover, the degree of performance healing in CF/PPS laminates is consistently higher than that in CF/PEEK laminates, which is closely related to the semicrystalline nature of PEEK resin.
引用
收藏
页数:15
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