Optimized preparation and aerospace applications of wear-resistant POM composites: a mini-review

IF 2 Q2 MATERIALS SCIENCE, MULTIDISCIPLINARY
Zheng Liu, Ruihan Zhang, Xingbei Liu, Zhenbo Yin, Zhiwei Li, Haoran Guo
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引用次数: 0

Abstract

Polyoxymethylene (POM) composites are promising self-lubricating materials for aerospace bearings due to their excellent friction properties, mechanical rigidity and dimensional stability. However, inherent drawbacks including high volatile organic compound emissions and poor high-temperature thermal stability severely restrict their large-scale aerospace applications. This review systematically summarizes the state-of-the-art optimization strategies of aviation-oriented POM composites, covering low-VOC and heat-resistant resin modification, particle/fiber reinforcement, and intelligent porous self-lubricating structural design. The service mechanisms and key performance evaluation criteria of POM composites under complex aerospace working conditions are analyzed, and the advantages and limitations of mainstream molding processes are clarified. Current technical bottlenecks limiting the aerospace engineering application of POM composites are discussed. Finally, future development directions focusing on multi-scale synergistic modification, intelligent lubrication design and closed-loop performance optimization are proposed, aiming to promote the high-reliability application of POM-based composites in advanced aviation bearing systems.

Graphical Abstract

耐磨POM复合材料的优化制备及航空航天应用综述
聚甲醛(POM)复合材料具有优异的摩擦性能、机械刚度和尺寸稳定性,是一种很有前途的航空航天轴承自润滑材料。然而,其固有的缺点包括高挥发性有机化合物排放和较差的高温热稳定性严重限制了其大规模的航空航天应用。本文系统总结了面向航空的聚甲醛复合材料的优化策略,包括低voc和耐热树脂改性、颗粒/纤维增强和智能多孔自润滑结构设计。分析了复合材料在航空航天复杂工况下的服役机理和关键性能评价标准,明确了主流成型工艺的优势和局限性。讨论了目前制约聚甲醛复合材料航天工程应用的技术瓶颈。最后,提出了以多尺度协同改性、智能润滑设计和闭环性能优化为重点的未来发展方向,旨在推动pomm基复合材料在先进航空轴承系统中的高可靠性应用。图形抽象
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
8.60
自引率
0.00%
发文量
1
审稿时长
13 weeks
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