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材料导报  2021, Vol. 35 Issue (22): 22178-22192    https://doi.org/10.11896/cldb.20090151
  高分子与聚合物基复合材料 |
基于三胞模型的2.5D编织复合材料力学性能研究
赵思钰, 温卫东, 周喻
南京航空航天大学能源与动力学院,南京 210016
Investigation of Mechanical Properties of 2.5D Braided Composites Based on Triple-cell Model
ZHAO Siyu, WEN Weidong, ZHOU Yu
College of Energy and Power Engineering, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China
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摘要 为了准确预测2.5D编织复合材料的纵向力学性能,本工作以2.5D等厚度和变厚度编织复合材料为研究对象,基于细观结构表征结果,建立了一种考虑表面挤压效应和纱线错位滑移影响的2.5D等厚度和变厚度编织复合材料的全胞和三胞模型;并在所建立的全胞和三胞几何模型的基础上,基于逐渐损伤法开展了2.5D等厚度和变厚度编织复合材料的数值模拟分析,对不同结构的纵向刚度和强度进行了预测,模拟了不同结构的损伤扩展过程和损伤行为,并与实验结果进行对比验证。结果表明:考虑表面挤压效应和纱线错位滑移影响的全胞和三胞模型能更准确地预测2.5D编织复合材料的力学性能;三胞模型的数值模拟结果能更准确地反映2.5D编织复合材料的损伤扩展过程,更全面地表征2.5D编织复合材料的损伤行为。
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赵思钰
温卫东
周喻
关键词:  2.5D编织复合材料  全胞模型  三胞模型  损伤行为  力学性能    
Abstract: In order to accurately predict the longitudinal mechanical properties of 2.5D braided composites, this work takes 2.5D equal thickness and va-riable thickness braided composites as the research object. Based on the microstructure characterization results, whole cell and triple-cell models of 2.5D equal thickness and variable thickness braided composites considering the effects of surface extrusion and yarn dislocation and slip is established. Based on the established whole cell and triple-cell geometric models, the numerical simulation analysis of 2.5D braided composites with equal thickness and variable thickness is carried out based on the progressive damage method, the longitudinal stiffness and strength of different structures are predicted, the damage propagation process and damage behavior of different structures are simulated, which is compared with the experimental results. The results show that the whole cell and triple-cell model considering the effects of surface extrusion and yarn dislocation slip can more accurately predict the mechanical properties of 2.5D braided composites; the numerical simulation results of the triple-cell model can more accurately reflect the damage propagation process of 2.5D braided composites and more comprehensively characterize the da-mage behavior of 2.5D braided composites.
Key words:  2.5D braided composite material    whole cell model    triple-cell model    damage behaviors    mechanical properties
出版日期:  2021-11-25      发布日期:  2021-12-13
ZTFLH:  TB322  
基金资助: 国家科技重大专项(2017-Ⅳ-0007-0044)
通讯作者:  gswwd@nuaa.edu.cn   
作者简介:  赵思钰,南京航空航天大学硕士研究生,主要从事先进复合材料结构强度设计技术研究工作。
温卫东,南京航空航天大学教授,博士研究生导师。1985年至今,在南京航空航天大学能源与动力学院长期从事航空动力结构、强度与振动的教学与科研工作。先后承担本科生《有限元法基础》《航空发动机强度》《弹性力学》《专业英语》《机械振动基础》以及研究生《高等结构强度理论》《模态分析与测试》《机械振动学》等课程的教学工作;招收和培养博士后6人,博士研究生30余人,硕士研究生70余人。主持完成国家自然科学基金、航空基金、国防航空发动机预研项目、国防基础预研项目等重要项目40余项,目前承担多项重要研究课题。在国内外核心刊物和国际会议上发表学术论文300余篇,其中SCI和EI收入150余篇;主编《专业英语》教材1部,参编《航空涡喷、涡扇发动机结构设计准则》1部,获省部级科技进步奖4项,江苏省教学成果一等奖1项。
引用本文:    
赵思钰, 温卫东, 周喻. 基于三胞模型的2.5D编织复合材料力学性能研究[J]. 材料导报, 2021, 35(22): 22178-22192.
ZHAO Siyu, WEN Weidong, ZHOU Yu. Investigation of Mechanical Properties of 2.5D Braided Composites Based on Triple-cell Model. Materials Reports, 2021, 35(22): 22178-22192.
链接本文:  
http://www.mater-rep.com/CN/10.11896/cldb.20090151  或          http://www.mater-rep.com/CN/Y2021/V35/I22/22178
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