| 注册
首页|期刊导航|宇航材料工艺|芳纶纤维/环氧树脂界面相的准静态纳米压痕研究

芳纶纤维/环氧树脂界面相的准静态纳米压痕研究

宋应登 李斌太 邢丽英

宇航材料工艺2017,Vol.47Issue(2):81-85,5.
宇航材料工艺2017,Vol.47Issue(2):81-85,5.DOI:10.12044/j.issn.1007-2330.2017.02.018

芳纶纤维/环氧树脂界面相的准静态纳米压痕研究

Interphase Characterization of Aramid/Epoxy Composites by Quasistatic Nanoindentation Method

宋应登 1李斌太 1邢丽英1

作者信息

  • 1. 北京航空材料研究院,中航工业复合材料中心,北京100095
  • 折叠

摘要

Abstract

The elastic modulus and hardness of interphase region for both Kevlar-49/epoxy and F-12/epoxy unidirectional composites were analyzed using quasistatic nanoindentation method.The results show that the height difference of aramid fiber and epoxy resin in longitudinal section of unidirectional composites is low.Therefore,the experimental error induced by indenter shape can be reduced,so that the mechanical properties of interphase region can be analyzed more accurately.The elastic modulus and hardness of interphase region are distinctly different from those of aramid fiber and epoxy resin.Based on the results of mechanical properties for fiber,epoxy and interphase obtained from nanoindentation,it is assumed that the width of property transition region is less than 1 μm.

关键词

芳纶纤维/芳纶纤维复合材料/界面相/纳米压痕

Key words

Aramid fiber/Aramid fiber composite/Interphase/Nanoindentation

分类

通用工业技术

引用本文复制引用

宋应登,李斌太,邢丽英..芳纶纤维/环氧树脂界面相的准静态纳米压痕研究[J].宇航材料工艺,2017,47(2):81-85,5.

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

访问量0
|
下载量0
段落导航相关论文