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纳米压痕技术表征T800碳纤维的弹性模量和硬度

张东生 李新涛 夏汇浩 冯志海 赵高文

宇航材料工艺2017,Vol.47Issue(4):79-85,7.
宇航材料工艺2017,Vol.47Issue(4):79-85,7.DOI:10.12044/j.issn.1007-2330.2017.04.018

纳米压痕技术表征T800碳纤维的弹性模量和硬度

Characterization of Elastic Modulus and Hardness of T800 Carbon Fiber Via Nanoindentation Technique

张东生 1李新涛 2夏汇浩 1冯志海 2赵高文2

作者信息

  • 1. 中国科学院上海应用物理研究所,上海201800
  • 2. 航天材料及工艺研究所,先进功能复合材料技术重点实验室,北京 100076
  • 折叠

摘要

Abstract

The elastic modulus and hardness of T800SC carbon fiber with different orientation respect to its axis direction were tested by nanoindentation,and the scatter in the data was treated in terms of the two-parameter Weibull statistical analysis.It is shown that with the increase of the intersection angle between the test plane and the axis direction,the elastic modulus and hardness of T800SC increase.When the intersection angle increases from 0° to 90°,the elastic modulus of T800SC rises to (50.96±5.73) GPa from (5.84±2.00) GPa,and the hardness increases from (2.71±0.51) GPa to (5.24±0.91) GPa.For the elastic modulus and hardness of T800SC carbon fiber with different orientation,the modulus of Weibull distribution ranges from 9.0 to 10.5 and from 6.0 to 8.0,respectively.

关键词

纳米压痕/碳纤维/弹性模量/Weibull分布/硬度

Key words

Nanoindentation/Carbon fiber/Elastic modulus/Weibull distribution/Hardness

分类

通用工业技术

引用本文复制引用

张东生,李新涛,夏汇浩,冯志海,赵高文..纳米压痕技术表征T800碳纤维的弹性模量和硬度[J].宇航材料工艺,2017,47(4):79-85,7.

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

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