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三维编织与层合复合材料力学性能对比试验

张迪 郑锡涛 孙颖 范献银

航空材料学报Issue(3):89-96,8.
航空材料学报Issue(3):89-96,8.DOI:10.11868/j.issn.1005-5053.2015.3.015

三维编织与层合复合材料力学性能对比试验

Comparative Investigation of Mechanical Properties between 3D Braided and Laminated Composites

张迪 1郑锡涛 1孙颖 2范献银1

作者信息

  • 1. 西北工业大学 航空学院,西安 710072
  • 2. 天津工业大学 复合材料研究所,天津 300160
  • 折叠

摘要

Abstract

The mechanical properties between three-dimensional (3D)braided and laminated composites were comparatively studied. These two sorts of composites were produced by the same carbon fiber,resin matrix and the same preparation process (RTM).There were totally four kinds of 3D multi-directionally braided composites,which contain 3D four-direction (3D4d ),3D five-direction (3D5d),3D six-direction (3D6d)and 3D seven-direction (3D7d)braiding respectively.And the three kinds of laminated composites manufactured utilizing tire cord fabric were 0°,90°and[0 /(45)2 /90]2s laminates.The mechanical properties of braided and laminat-ed specimens were measured by the same tension,compression and shear testing methods.The results show that the properties of lami-nated composites are worse than that of 3D-braided composite except 0°unidirectional laminates.As to the braided composites,the smaller the braiding angle is,the better longitudinal properties and worse shear properties are.The braiding fabric is also an important factor which affects the mechanical properties.Meanwhile,the failure modes were also discussed,and the results show that,braiding fabric and the braiding angle are the main factors that affect the failure mode.

关键词

复合材料/三维编织/试验/力学性能/破坏模式

Key words

composites/three-dimensional braid/experiment/mechanical property/failure mood

分类

通用工业技术

引用本文复制引用

张迪,郑锡涛,孙颖,范献银..三维编织与层合复合材料力学性能对比试验[J].航空材料学报,2015,(3):89-96,8.

基金项目

西北工业大学研究生创意新种子基金(Z2015045);陕西省国际科技合作与交流计划项目 ()

航空材料学报

OA北大核心CSCDCSTPCD

1005-5053

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