Effects of two-stage creep-aging processing on mechanical properties of an Al-Cu-Mg alloy

被引：31
|
作者：
Lin, Y. C. [1 ,2 ,3 ]
Liu, Guan [1 ,2 ]
Chen, Ming-Song [1 ,2 ]
Li, Jia [1 ,2 ]
Zhou, Mi [1 ,2 ]
Zhou, Hua-Min [4 ]
机构：
[1] Cent S Univ, Sch Mech & Elect Engn, Changsha 410083, Hunan, Peoples R China
[2] Cent S Univ, Light Alloy Res Inst, Changsha 410083, Hunan, Peoples R China
[3] State Key Lab High Performance Complex Mfg, Changsha 410083, Hunan, Peoples R China
[4] State Key Lab Mat Proc & Die & Mould Technol, Wuhan 430074, Peoples R China
来源：
MATERIALS & DESIGN | 2015年 / 79卷
关键词：
Two-stage creep-aging; Alloy; Mechanical properties; Aging precipitates; HOT TENSILE DEFORMATION; YIELD-POINT PHENOMENON; 2024; ALUMINUM-ALLOY; NI-BASED SUPERALLOY; FRACTURE CHARACTERISTICS; DUCTILITY BEHAVIOR; FLOW-STRESS; AG ALLOY; PRECIPITATION; MICROSTRUCTURE;
D O I：
10.1016/j.matdes.2015.04.047
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
Two-stage creep-aging behavior of an Al-Cu-Mg alloy are studied by uniaxial tensile creep tests over wide ranges of temperature and external stress. Effects of creep-aging temperature and external stress on mechanical properties are discussed. It is found that the mechanical properties of the studied Al-Cu-Mg alloy are strongly sensitive to the creep-aging parameters. The two-stage creep-aging processing can change the characteristics of aging precipitates and dislocations, which greatly affects the mechanical properties of the studied Al-Cu-Mg alloy. With the increase of the second stage creep-aging temperature, the yield strength increases, while the ultimate tensile strength and elongation decrease. Meanwhile, the yield strength decreases with the increase of external stress. However, the ultimate tensile strength and elongation first increase and then decrease when the external stress is continuously increased within the tested conditions. Additionally, the mechanical properties of the two-stage creep-aged alloy are better than those of one-stage creep-aged and stress-free aged alloys. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码：127 / 135
页数：9
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