Microstructural evolution and vibration fatigue properties of 7075-T651 aluminum alloy treated by nitrogen ion implantation

被引:24
|
作者
Liu, Wenming [1 ,2 ]
Man, Qiyun [1 ,2 ]
Li, Jing [1 ,2 ]
Liu, Lin [1 ,2 ,3 ]
Zhang, Wei [1 ]
Wang, Zhijian [1 ]
Pan, Haijun [1 ]
机构
[1] Changzhou Univ, Sch Mech Engn & Rail Transit, Changzhou 213164, Peoples R China
[2] Changzhou Univ, Jiangsu Key Lab Green Proc Equipment, Changzhou 213164, Peoples R China
[3] Changzhou Univ, Sch Mech Engn & Rail Transit, Gehuzhong Rd 21, Changzhou 213164, Jiangsu, Peoples R China
关键词
Ion implantation; 7075-T651 aluminum alloy; Microstructure; Vibration fatigue; Fracture morphologies; HIGH-CYCLE FATIGUE; SURFACE NANOCRYSTALLIZATION; MECHANICAL-PROPERTIES; CRACK PROPAGATION; RADIATION-DAMAGE; IRRADIATION; BEHAVIORS; GROWTH; LIFE;
D O I
10.1016/j.vacuum.2022.110931
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The effects of nitrogen ion implantation on the microstructures and the vibration fatigue properties of the 7075-T651 aluminum alloy were investigated. Nitrogen ions were implanted into 7075-T651 aluminum alloy by metal vapor vacuum arc (MEVVA) at the dose of 3 x 10(17) ions/cm(2) at room temperature. The trajectory distribution range and the introduced defects of nitrogen ion-implanted 7075-T651 aluminum alloy were simulated using the Stopping and Range of Ions in Matter software. The phase composition was tested by X-ray diffraction (XRD), the microstructures were characterized using a transmission electron microscope (TEM), and the fracture mor-phologies of vibration samples were observed using a scanning electron microscope (SEM). Experimental results indicate that the fatigue life of the ion-implanted vibration samples increased by 75% compared with the un-treated samples. The ion implantation caused the microscopic strain,which increased the density of dislocation structure and reduced the grain size. The gradient microstructure and fracture properties of the sample were analyzed. The results show that the high-density dislocation and fine grains induced by ion implantation are beneficial to prolong the vibration fatigue life.
引用
收藏
页数:10
相关论文
共 50 条
  • [21] Micro structure-based multistage fatigue modeling of aluminum alloy 7075-T651
    Xue, Y.
    McDowell, D. L.
    Horstemeyer, M. F.
    Dale, M. H.
    Jordon, J. B.
    ENGINEERING FRACTURE MECHANICS, 2007, 74 (17) : 2810 - 2823
  • [22] Microstructure and properties of 7075-T651 aluminum alloy friction plug welding joint
    Li S.
    Sun Z.
    Liu X.
    Wang L.
    Ma S.
    Hanjie Xuebao/Transactions of the China Welding Institution, 2023, 44 (07): : 95 - 101
  • [23] Effect of ductile thermal spray coatings on fatigue performance of 7075-T651 aluminum alloy
    Arsenault, B
    Lynn, AK
    Duquesnay, DL
    CANADIAN METALLURGICAL QUARTERLY, 2005, 44 (04) : 495 - 504
  • [24] THE PLASTIC COMPRESSIBILITY OF 7075-T651 ALUMINUM-ALLOY PLATE
    FREED, AD
    SANDOR, BI
    EXPERIMENTAL MECHANICS, 1986, 26 (02) : 119 - 121
  • [25] Superplasticity of a Friction Stir Processed 7075-T651 aluminum alloy
    Dieguez, T.
    Burgueno, A.
    Svoboda, H.
    11TH INTERNATIONAL CONGRESS ON METALLURGY & MATERIALS SAM/CONAMET 2011, 2012, 1 : 110 - 117
  • [26] THE EFFECTS OF WARM WORKING ON ALUMINUM-ALLOY 7075-T651
    PAPAZIAN, JM
    MATERIALS SCIENCE AND ENGINEERING, 1981, 51 (02): : 223 - 230
  • [27] STRESS CORROSION OF ALUMINUM ALLOY 7075-T651 IN ORGANIC LIQUIDS
    PROCTER, RPM
    PAXTON, HW
    JOURNAL OF MATERIALS, 1969, 4 (03): : 729 - &
  • [28] Environmentally influenced near-threshold fatigue crack growth in 7075-T651 aluminum alloy
    Lee, FU
    Sanders, HC
    George, K
    Agarwala, VV
    ENVIRONMENTALLY ASSISTED CRACKING: PREDICTIVE METHODS FOR RISK ASSESSMENT AND EVALUATION OF MATERIALS, EQUIPMENT, AND STRUCTURES, 2000, 1401 : 382 - 393
  • [29] Effects of different structural parameters on the 7075-T651 aluminum alloy lug structure fatigue life
    Hui, Li
    Wang, Hongda
    Huang, Yanqing
    Yang, Wenjun
    Zhou, Song
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (15) : 3304 - 3312
  • [30] Orthogonal impact load in 6061-T651 and 7075-T651 aluminum alloy plates
    Frutos, J. A.
    Ambriz, R. R.
    Garcia, Ch. J.
    Jaramillo, D.
    JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T, 2023, 26 : 4245 - 4262