(1. 湖南大學(xué) 汽車車身先進(jìn)設(shè)計(jì)制造國家重點(diǎn)實(shí)驗(yàn)室，長沙 410082；
2. 湖南大學(xué) 機(jī)械與運(yùn)載工程學(xué)院，長沙 410082)
摘 要: 采用Gleeble-3500熱模擬機(jī)研究6013鋁合金在613~773 K、0.001~10 s-1下的平面應(yīng)變流變力學(xué)行為。基于熱傳導(dǎo)對材料變形熱效應(yīng)的影響，優(yōu)化材料變形溫升的計(jì)算方程，分析變形能及熱傳導(dǎo)對實(shí)測流變應(yīng)力誤差的影響。結(jié)果表明：熱傳導(dǎo)對變形溫升的影響不可忽略，其影響隨著真應(yīng)變的增加和應(yīng)變速率的降低而更加顯著；通過熱傳導(dǎo)對變形溫升的修正，變形溫升隨變形能的增大呈非線性變化趨勢；在較高應(yīng)變速率和較低變形溫度下，變形能及熱傳導(dǎo)對材料變形溫升及穩(wěn)態(tài)流變應(yīng)力的影響明顯；可用包含Zener-Hollomon參數(shù)(Z)的本構(gòu)方程預(yù)測6013鋁合金在不同變形條件下的流變應(yīng)力峰值，其熱變形激活能為364.48 kJ/mol；修正的實(shí)測峰值應(yīng)力與預(yù)測值的吻合程度有所提高，平均相對誤差為5.54%。
關(guān)鍵字: 6013鋁合金；平面熱壓縮；流變應(yīng)力；熱傳導(dǎo)；瞬時溫升；本構(gòu)方程
（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
