Transactions of Nonferrous Metals Society of China The Chinese Journal of Nonferrous Metals

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中国有色金属学报

ZHONGGUO YOUSEJINSHU XUEBAO

第24卷    第5期    总第182期    2014年5月

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文章编号:1004-0609(2014)05-1268-07
6013铝合金平面热压缩流变应力曲线修正与本构方程
肖 罡1, 2,李落星1, 2,叶 拓1, 2

(1. 湖南大学 汽车车身先进设计制造国家重点实验室,长沙 410082;
2. 湖南大学 机械与运载工程学院,长沙 410082
)

摘 要: 采用Gleeble-3500热模拟机研究6013铝合金在613~773 K、0.001~10 s-1下的平面应变流变力学行为。基于热传导对材料变形热效应的影响,优化材料变形温升的计算方程,分析变形能及热传导对实测流变应力误差的影响。结果表明:热传导对变形温升的影响不可忽略,其影响随着真应变的增加和应变速率的降低而更加显著;通过热传导对变形温升的修正,变形温升随变形能的增大呈非线性变化趋势;在较高应变速率和较低变形温度下,变形能及热传导对材料变形温升及稳态流变应力的影响明显;可用包含Zener-Hollomon参数(Z)的本构方程预测6013铝合金在不同变形条件下的流变应力峰值,其热变形激活能为364.48 kJ/mol;修正的实测峰值应力与预测值的吻合程度有所提高,平均相对误差为5.54%。

 

关键字: 6013铝合金;平面热压缩;流变应力;热传导;瞬时温升;本构方程

Modification of flow stress curves and constitutive equations during hot plane compression deformation of 6013 aluminum alloy
XIAO Gang1, 2, LI Luo-xing1, 2, YE Tuo1, 2

1. State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body,
Hunan University, Changsha 410082, China;
2. College of Mechanical and Vehicle Engineering, Hunan University, Changsha 410082, China

Abstract:The hot plane compression deformation behavior of 6013 aluminum alloy was investigated on Gleeble-3500 thermal-mechanical simulating tester in the temperature range from 613 to 773 K and strain rate range from 0.001 to 10 s-1. The mathematical expression of temperature rising is optimized based on the influence of the heat conduction during hot deformation. Meanwhile, the effects caused by deformation energy and heat conduction on the measured stress errors were analyzed. The results show that the influence of heat conduction cannot be neglected and becomes more obvious with increasing true strain and decreasing strain rate. The relationship between the change of temperature rising corrected by heat conduction and deformation heating is nonlinear. The temperature rising and the steady flow stress are seriously affected by deformation energy and heat conduction during higher stain rate and lower temperature. The peak flow stress can be represented by the Zener-Hollomon parameter (Z) in the hyperbolic sine equation with the hot deformation activation energy of 364.48 kJ/mol. The corrected measured value exhibits a better agreement with the flow stress predicted by the constitutive equation, and the average relative error is 5.54%.

 

Key words: 6013 aluminum alloy; hot plane compression deformation; flow stress; heat conduction; instantaneous temperature rising; constitutive equation

ISSN 1004-0609
CN 43-1238/TG
CODEN: ZYJXFK

ISSN 1003-6326
CN 43-1239/TG
CODEN: TNMCEW

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