| 注册
首页|期刊导航|航天器环境工程|新型锆钛合金的动态拉伸力学性能与微观断裂机制试验研究

新型锆钛合金的动态拉伸力学性能与微观断裂机制试验研究

刘崧 覃金贵 陈荣 龚自正 张品亮

航天器环境工程2013,Vol.30Issue(3):310-315,6.
航天器环境工程2013,Vol.30Issue(3):310-315,6.DOI:10.3969/j.issn.1673-1379.2013.03.016

新型锆钛合金的动态拉伸力学性能与微观断裂机制试验研究

Tests of dynamic tensile properties and microscopic fragment mechanism for a new zirconium-titanium alloy

刘崧 1覃金贵 2陈荣 2龚自正 1张品亮3

作者信息

  • 1. 西南交通大学材料科学与工程学院,成都610039
  • 2. 国防科技大学理学院,长沙410073
  • 3. 北京卫星环境工程研究所可靠性与环境工程技术重点实验室,北京100094
  • 折叠

摘要

Abstract

Dynamic tension tests were conducted by employing the SHTB(split Hopkinson tension bar) to study the dynamic machanical properties of a new zirconium-titanium alloy.The dynamic mechanical properties of the alloy were determined at high strain rates ranging from 800 S-1 to 4000 s-1 at room temperature.The results show that the mechanical behavior of zirconium-titanium alloy depends on the strain rate,the dynamic strengths(including σ0.2 and σb),the unstable strain,the elongation,and the strain energy density all increase with the increase of the strain rates.The SEM fractographic observation shows that there exists a strain rate dependence of the fracture mode for the alloy sample.At room temperature and 800 s-1,the sample is brittle,but its fracture modes changes from a quasi-cleavage one to a ductile one with increased strain rates.

关键词

Hopkinson杆/动态拉伸/应变率/锆钛合金

Key words

Hopkinson bar/ dynamic tension/ strain rate/ zirconium-titanium alloy

分类

通用工业技术

引用本文复制引用

刘崧,覃金贵,陈荣,龚自正,张品亮..新型锆钛合金的动态拉伸力学性能与微观断裂机制试验研究[J].航天器环境工程,2013,30(3):310-315,6.

基金项目

国家重点基础研究发展计划资助项目(编号:2010CB731600) (编号:2010CB731600)

航天器环境工程

OACSTPCD

1673-1379

访问量0
|
下载量0
段落导航相关论文