Role of thermal-mechanical loading sequence on creep aging behaviors of 5A90 Al-Li alloy

被引:20
作者
Fu, J. [1 ]
Li, H. [1 ]
Lei, C. [1 ]
Zheng, G. W. [1 ]
Bian, T. J. [1 ]
Zhan, L. H. [2 ]
机构
[1] Northwestern Polytech Univ, Sch Mat Sci & Engn, State Key Lab Solidificat Proc, Xian 710072, Shaanxi, Peoples R China
[2] Cent S Univ, Sch Mech & Elect Engn, State Key Lab High Performance Complex Mfg, Changsha 410083, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
5A90 Al-Li alloy; Creep age forming; Thermal-mechanical loading sequence; Creep deformation; Mechanical properties; Microstructures; ALUMINUM-ALLOY; INITIAL TEMPERS; MG ALLOY; MICROSTRUCTURES; DEFORMATION; SPRINGBACK; KINETICS; TENSILE;
D O I
10.1016/j.jmatprotec.2017.12.028
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Creep age forming (CAF), under thermal-mechanical environment, may be sensitive to the thermal and mechanical loading conditions. Unfortunately, the different creep aging (CA) behaviors under two inverse thermal mechanical loading sequences, viz. loading-heating (LH) and heating-loading (HL), are almost neglected in experiments or modeling of CAF. In this work, taking solution treated 5A90 Al-Li alloy as a case material, the loading sequence related CA behaviors of the alloy are investigated using continuous/interrupted tensile CA tests at 130 degrees C/175 MPa combined with high-resolution Transmission Electron Microscope (HRTEM) and mechanical properties tests. The results show that, the inverse loading sequences result in different initial tempers for CA process, viz. solution temper under LH and stress-free aged temper under HL. The solution temper for CA process under LH can lead to a more stable and repeatable CA process than HL does, which causes a stress-free aged temper with randomly and discretely distributed precipitates for CA process. After two inverse loadings and 18 h of isothermal CA, the total creep deformation for LH (0.1475%) is twice larger than that for HL (0.0720%), thanks to the remarkable creep strain in the LH non-isothermal CA process with 49.2% of total creep strain. The samples under LH present a lower strength and a higher elongation than those under HL during the whole process, and the gap of the mechanical properties of samples under the two loading sequences reaches its maximum (15 MPa for yield strength and 8.45% for elongation) after 0.5 h of isothermal CA, and then gradually decreases in subsequent process. After 0.5 h of isothermal CA, though the volume fraction of the delta' precipitates (Al3Li) under LH is larger than that under HL, the dislocations density under LH is less than that under HL, which makes a lower material strength under LH. It is noted that, after 18 h of isothermal CA, the microstructures and macroscopic mechanical properties of the samples have less disparity for the two inverse loading sequences.
引用
收藏
页码:354 / 363
页数:10
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