薄层碳纤维增强树脂基复合材料研究与应用进展  

Research and Application Progresses of Thin-Ply Carbon Fiber Reinforced Polymer Matrix Composites

作　　者：邱超[1] 马心旗 王亚震 郭子月 吴海宏[1] QIU Chao;MA Xinqi;WANG Yazhen;GUO Ziyue;WU Haihong(Carbon Fiber Composites International Joint Research Lab in Henan,Henan University of Technology,Zhengzhou 450001,China)

机构地区：[1]河南工业大学碳纤维复合材料河南省国际合作实验室,郑州450001

出　　处：《航空制造技术》2021年第14期22-31,共10页Aeronautical Manufacturing Technology

基　　金：国家自然科学基金委-河南省联合基金重点项目(U1604253);国家重点研发计划(2016YFB0101602)。

摘　　要：薄层碳纤维增强树脂基复合材料(CFRP)具有质轻、力学性能好、对复杂型面适应性好、可设计性强的优点,在航空航天领域广受重视。从CFRP层合板宏观、细观、微观尺度出发,综述了薄层化对CFRP层合板孔隙率、细(微)观结构演化、损伤机制等基础问题作用效应的研究进展,分析了一些重要的研究结论对薄层复合材料发展的指导意义,探讨了尚存争议的研究结果及其理论基础。在此基础上,介绍了薄层CFRP在航空结构、卫星可折叠结构以及大型液体燃料储罐中的应用。Thin-ply carbon fiber reinforced polymers(CFRP)have the advantages of light weight,good mechanical properties,good adaptability to complex shapes,strong designability,which are valuable characteristics in aerospace applications.From the views of the macro,meso and micro scales of CFRP laminates,the research progresses for the thinply effects on the basic problems of the laminate such as porosity,meso(micro)structural evolution and damage mechanism are reviewed,and the direct meanings of the important research conclusions to the development of thin-ply composites are analyzed in this paper.The controversial research results and related theoretical foundation are discussed.Furthermore,the applications of thin-ply CFRP structural parts in aircraft,foldable structures in satellite and large liquid fuel storage tanks are introduced.

关 键 词：薄层化效应 碳纤维 复合材料 宏观尺度 微观尺度 

分 类 号：V258.3[一般工业技术—材料科学与工程] TB332[航空宇航科学与技术—航空宇航制造工程] TQ327.3[化学工程—合成树脂塑料工业]