航空航天
机身
热塑性复合材料
材料科学
热塑性塑料
焊接
耐久性
先进复合材料
复合材料
航空航天材料
复合数
飞机工业
机械工程
制造工程
航空
损伤容限
持续性
热塑性聚合物
工程类
热塑性弹性体
航空航天工程
凯夫拉
范围(计算机科学)
作者
Tonmoy Sarker,Protick Chandra Ghosh,Adnan Ahammed Bhuiyan,Md Raihanul Islam,M. S. Rabbi
标识
DOI:10.1177/08927057261447758
摘要
Thermoplastic composites have been adopted in aerospace mainly as substitutes for thermosets, facilitating recyclability and reuse, extended shelf life, and expedited manufacturing, which have gained significance due to stringent production rates and sustainability objectives. Progress in aerospace-grade PPS and PAEK systems, along with advancements in automated forming and welding, has facilitated the transition from localized substitutes to extensive structural integration. Contemporary aircraft utilize thermoplastic composites not merely as isolated replacements; they now encompass aviation systems hardware, high-volume secondary aerostructures, and progressively integrated airframe substructures facilitated by the fusion welding of PEEK/PEKK-based architectures. The future direction is towards highly automated, weld-focused assembly, enhanced by in-process monitoring, nondestructive inspection, and certification-ready durability proof. At the same time, circularity initiatives concentrate on scalable end-of-life recovery methods for fiber-reinforced thermoplastics.
科研通智能强力驱动
Strongly Powered by AbleSci AI