南京航空航天大学学报2024,Vol.56Issue(1) :17-30.DOI:10.16356/j.1005-2615.2024.01.002

变刚度复合材料层合板研究进展

Research Progress of Variable Stiffness Composite Laminates

王显峰 阳铭广 刘琛 高文明 孙颖 叶帆
南京航空航天大学学报2024,Vol.56Issue(1) :17-30.DOI:10.16356/j.1005-2615.2024.01.002

变刚度复合材料层合板研究进展

Research Progress of Variable Stiffness Composite Laminates

王显峰 1阳铭广 1刘琛 1高文明 1孙颖 1叶帆1
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作者信息

  • 1. 南京航空航天大学材料科学与技术学院,南京 211106
  • 折叠

摘要

变刚度复合材料层合板由纤维曲线铺放而成,可以实现刚度分布的变化设计,与传统固定铺层角的复合材料层合板相比,变刚度复合材料层合板在减少重量和成本的同时,也提高了结构性能.随着铺放设备的发展,目前已经能够利用自动铺放技术实现纤维的曲线铺放.同时,为提高复合材料构件的结构性能和满足不同的工程实际需求,铺层设计方法也从单一角度的直线铺层逐渐向变角度曲线铺层发展.本文首先介绍了变刚度复合材料层合板设计制造方法与有限元建模,接着在刚度分布、屈曲特性、失效行为等方面阐述了变刚度复合材料层合板力学性能的研究进展,然后结合南京航空航天大学复合材料工程自动化技术研究中心在变刚度复合材料层合板振动特性方面的研究,对变刚度复合材料层合板振动特性进行了分析和概括,最后对变刚度复合材料层合板未来的研究趋势进行了论述与展望.

Abstract

Variable stiffness composite laminates are fabricated by laying fibers in curved patterns,allowing for a tailored design of stiffness distribution.Compared with conventional composite laminates with a fixed bedding angle,variable stiffness composite laminates not only achieve reductions in weight and cost but also exhibit enhanced structural performance.With the advancement of the layup technology,automated layup techniques have enabled the implementation of the curved fiber layup,facilitating the evolution of layup design methodologies from single-angle straight layups to variable-angle curved layups.This paper commences with an exposition of the design and manufacturing methodologies,coupled with the finite element modeling of variable stiffness composite laminates.Subsequently,comprehensive insights are provided into the research advancements pertaining to the mechanical properties of variable stiffness composite laminates,encompassing aspects such as stiffness distribution,buckling characteristics,and failure behavior.Integrating this knowledge with the investigations conducted by the Composite Materials Engineering Automation Technology Research Center at Nanjing University of Aeronautics&Astronautics on the vibration characteristics of variable stiffness composite laminates,the vibration properties of these laminates are analyzed.In conclusion,the future research trend in the domain of variable stiffness composite laminates is discussed.

关键词

变刚度复合材料层合板/纤维曲线铺放/轨迹设计/有限元建模/力学性能/振动特性

Key words

variable stiffness composite laminates/fiber curve placement/track design/finite element modeling/mechanical property/vibration performance

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基金项目

江苏省重点研发计划(BE2023014-4)

高质量发展项目(2023ZY01058)

出版年

2024
南京航空航天大学学报
南京航空航天大学

南京航空航天大学学报

CSTPCDCSCD北大核心
影响因子:0.734
ISSN:1005-2615
参考文献量91
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