• CN: 11-2187/TH
  • ISSN: 0577-6686

Journal of Mechanical Engineering ›› 2022, Vol. 58 ›› Issue (16): 58-67.doi: 10.3901/JME.2022.16.058

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Study on Electromagnetic Deformation Combined with Heat Treatment Process of Al-Li Alloy

XU Jiahui1,2, HUANG Liang1,2, XIE Bingxin1,2, LI Jianjun1,2   

  1. 1. School of Materials Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074;
    2. State Key Laboratory of Materials Processing and Die & Mould Technology, Huazhong University of Science and Technology, Wuhan 430074
  • Received:2021-11-30 Revised:2022-04-15 Online:2022-08-20 Published:2022-11-03

Abstract: In order to solve the forming problem of high-performance Al-Li alloy parts, an electromagnetic deformation combined with heat treatment (ET) is proposed, and the microstructure behavior and mechanical properties advantages of 2195 Al-Li alloy under ET are studied. The process of ET is solution treatment and quenching, followed by electromagnetic deformation, and then artificial aging. Compared with traditional thermomechanical heat treatment (TMT). ET is different in that its pre-deformation method is electromagnetic deformation with the advantages of high forming limit, low die-fitting gap, and excellent surface quality. It is found that the mechanical properties of the ET specimens have the advantages of low yield strength ratio and strong work hardening ability. The ultimate tensile strength, the elongation, and the yield strength ratio of the ET specimen reach 612.3 MPa±2.4 MPa, 11.7%±0.2%, and 86.9%, respectively. The yield strength ratio of the ET specimen is 7% lower than that of the TMT specimen. After the ET component is yielded, it is more stress increase margin to reach the failure stare, which is conducive to the reliable service of the parts. In addition, in the plastic deformation stage, the strain hardening rate of the ET specimen is higher, which is twice of the TMT specimen, indicating that the work hardening ability of the ET specimen is higher. Besides, through texture and Schmid factor analysis, the mechanism of higher work hardening ability of ET specimen is revealed. The (110)//RD texture volume fraction of ET specimen is higher and the Schmid factor is lower, indicating that the subsequent deformation of the ET specimen is greater and the deformation resistance is greater during the plastic deformation process. Through fracture analysis, it is found that both TMT and ET specimens show intergranular fractures and transgranular fractures, and there are local dimple morphologies. The fracture morphology of ET specimens shows a larger area of dimples, which is consistent with the results of the higher plasticity of the ET specimen.

Key words: electromagnetic deformation combined with heat treatment, 2195 Al-Li alloy, work hardening ability, texture, Schmid factor

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