期刊文献+

7075/6009铝合金复合材料热压缩变形的本构方程 被引量:2

Constitutive Equation of 7075/6009 Aluminium Composite during Hot Compression
下载PDF
导出
摘要 采用Gleeble-3500型热模拟机对7075/6009铝合金复合材料在变形温度为300~500℃、应变速率为0.001~1s^(-1)条件下的热压缩变形进行了研究,并得出了本构方程。结果表明:应变速率和变形温度对该复合材料的流变应力有显著影响,流变应力随变形温度的升高而降低,随应变速率的提高而增大;可采用Zener-Hollomon参数的双曲正弦函数来描述该复合材料热压缩变形的峰值流变应力;热压缩变形本构方程中的结构因子A、应力水平参数α和应力指数n分别为1.23×10^(11)s^(-1),0.021和6.449,热变形激活能Q为166.89 kJ·mol^(-1)。 The hot compression deformation of 7075/6009 aluminium composite was studied in the temperature range of 300-500℃ and strain rate range of 0. 001-1 s^11 by using Gleeble-3500 thermal simulation tester, and the constitutive equation was got. The results show that the flow stress of the composite was significantly affected by strain rate and deformation temperature. The flow stress decreased with the increase of deformation temperature and increased with the increase of strain rate. The peak flow stress behavior of the composite during deformation at high temperature could be described by hyperbolic sine function of Zener-Hollomon parameter. The structural factorA, stress level parameter a and stress index n in the analysis formular of peak flow stress was 1.23 × 1011 s^-1 , 0. 021 and 6. 449, respectively. The hot deformation activation energy of the composite was 168. 89 kJ · mo1^-1
出处 《机械工程材料》 CAS CSCD 北大核心 2011年第8期93-96,共4页 Materials For Mechanical Engineering
基金 国家自然科学基金资助项目(50575076) 教育部新世纪人才支持计划项目(NCET-07-0310) 中央高校基础科研业务费资助项目(2009ZM0278)
关键词 7075/6009铝合金复合材料 热压缩变形 本构方程 7075/6009 aluminium composite hot compression deformatiom constitutive equation
  • 相关文献

参考文献10

二级参考文献56

共引文献120

同被引文献26

引证文献2

二级引证文献4

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部