An experimental and theoretical investigation on residual stress of 7075-T651 aluminum alloy hole under electromagnetic cold expansion

被引:1
|
作者
Tang, Kangjie [1 ]
Zhang, Xu [1 ]
Wu, Dingfeng [1 ]
Dong, Dongying [2 ]
Deng, Huakun [1 ]
Cui, Junjia [3 ]
机构
[1] Changsha Univ Sci & Technol, Coll Automot & Mech Engn, Changsha 410114, Peoples R China
[2] Changsha Univ Sci & Technol, Coll Energy & Power Engn, Changsha 410114, Peoples R China
[3] Hunan Univ, State Key Lab Adv Design & Mfg Vehicle Body, Changsha 410082, Peoples R China
基金
中国国家自然科学基金;
关键词
Electromagnetic cold expansion; Residual stress; Theoretical model; 7075-T651 aluminum alloy;
D O I
10.1016/j.engfailanal.2024.108793
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The electromagnetic cold expansion process (ECE) was adopted in this work. The theoretical plastic radius, hole wall stress, radial stress, circumferential stress and release stress under different expansion rates (ER) were studied based on thick cylinder theory and ECE experiments. The released strain, residual stress (RS) and failure force were measured. The tensile fracture morphology was characterized. The results showed that the theoretical plastic radius (maximum 15.87 mm), internal stress (maximum 982.9 MPa), radial stress (maximum -820.9 MPa) and circumferential stress (maximum -271.4 MPa) increased with the increase of ER. The absolute radial and circumferential stress decreased and increased in negative and positive ranges respectively with distance increased. The release strain (maximum -3033 mu epsilon, 10-6 microstrain), radial RS (maximum 600.9 MPa) and circumferential RS (maximum 601.1 MPa) also increased with the increase of ER, and the minimum relative error of the plastic zone radius of the theoretical model was 3.78 % proving the reliability of the model. In addition, ECE increased the release stress (the maximum radial and circumferential release stresses were 1402.6 MPa and 747.5 MPa) and decreased the failure force (minimum 44.7kN) with increased ER. The initial crack position tended to transition from the inlet and outlet surfaces to the middle position, and the crack propagation angle and axial crack size gradually decreased with the decreased ER and stress level.
引用
收藏
页数:20
相关论文
共 50 条
  • [41] Experimental Study on the Thermal Stability of Aluminum Alloy 7075-T651 Structural Parts after Rolling Correction
    Lu, Laixiao
    Qin, Meizhen
    Jia, Xiaodong
    Wang, Zhonglei
    Chen, Qingqiang
    Sun, Jie
    Jiao, Shourong
    METALS, 2023, 13 (02)
  • [42] Investigation of Uniaxial Asymmetric High-cycle Fatigue Failure Behavior of 7075-T651 Aluminum Alloy Sheet
    Yang, Da-Lian
    Liu, Yi-Lun
    Li, Song-Bai
    Yi, Jiu-Huo
    Tao, Jie
    PROCEEDINGS OF THE 2015 INTERNATIONAL CONFERENCE ON MATERIAL SCIENCE AND APPLICATIONS (ICMSA 2015), 2015, 3 : 252 - 257
  • [43] Test method for corrosion pit-to-fatigue crack transition from a corner of hole in 7075-T651 aluminum alloy
    Arunachalam, Saravanan
    Fawaz, Scott
    INTERNATIONAL JOURNAL OF FATIGUE, 2016, 91 : 50 - 58
  • [44] Corrosion-fatigue behaviour of 7075-T651 aluminum alloy subjected to periodic overloads
    Chlistovsky, R. M.
    Heffernan, P. J.
    DuQuesnay, D. L.
    INTERNATIONAL JOURNAL OF FATIGUE, 2007, 29 (9-11) : 1941 - 1949
  • [45] The role of brass texture on the deformation response of 7075-T651 aluminum alloy under equi-biaxial tension
    Srinivasan, Nedunchezhian
    Velmurugan, R.
    Bhaskar, Lalith Kumar
    Singh, Satish Kumar
    Pant, Bhanu
    Kumar, Ravi
    MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2021, 812
  • [46] Fatigue life of 7075-T651 aluminium alloy treated with vibratory stress relief
    Gao, Hanjun
    Zhang, Yidu
    Wu, Qiong
    Song, Jing
    Wen, Kai
    INTERNATIONAL JOURNAL OF FATIGUE, 2018, 108 : 62 - 67
  • [47] Modelling the effects of intergranular corrosion around a fastener hole in 7075-T651 aluminium alloy
    Harrison, Timothy J.
    Crawford, Bruce R.
    Brandt, Milan
    Clark, Graham
    COMPUTATIONAL MATERIALS SCIENCE, 2014, 84 : 74 - 82
  • [48] Dynamic fracture-initiation toughness determination of Al 7075-T651 aluminum alloy
    Loya, J. A.
    Fernandez-Saez, J.
    JOURNAL OF TESTING AND EVALUATION, 2007, 35 (01) : 25 - 30
  • [49] Effect of cutting parameters on machinability of 7075-T651 aluminum alloy in different processing methods
    Luo, Heng
    Wang, Youqiang
    Zhang, Ping
    INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2020, 110 (7-8): : 2035 - 2047
  • [50] Fatigue Performance Improvement of 7075-T651 Aluminum Alloy by Ultrasonic Nanocrystal Surface Modification
    Zhang, Ruixia
    Chiang, Richard
    Ren, Zhencheng
    Zhang, Hao
    Zhao, Weidong
    Wang, Guo-Xiang
    Vasudevan, Vijay K.
    Dong, Yalin
    Ye, Chang
    JOURNAL OF MATERIALS ENGINEERING AND PERFORMANCE, 2022, 31 (03) : 2354 - 2363