Strengthening mechanisms of AlCoCrFeNi-WC-Ti coating from first-principles calculations

被引:7
作者
Yutao, Li [1 ]
Hanguang, Fu [1 ,3 ]
Kaiming, Wang [2 ,4 ]
Xiaojun, Yang [1 ]
Xingye, Guo [1 ]
Jian, Lin [1 ]
机构
[1] Beijing Univ Technol, Inst Welding & Surface Technol, Key Lab Adv Funct Mat, Minist Educ, Beijing 100124, Peoples R China
[2] Changsha Univ Sci & Technol, Coll Automobile & Mech Engn, Changsha, Peoples R China
[3] Beijing Univ Technol, Inst Welding & Surface Technol, Amt 100, Pingle Garden, Beijing 100124, Peoples R China
[4] Changsha Univ Sci & Technol, Coll Automobile & Mech Engn, 960, Sect 2,Wanjiali South Rd, Changsha 410114, Hunan, Peoples R China
来源
MATERIALS TODAY COMMUNICATIONS | 2022年 / 33卷
关键词
HEA composite coating; Laser cladding; First-principles calculation; Strengthening mechanism; Hardness prediction; HIGH-ENTROPY ALLOY; MICROSTRUCTURE EVOLUTION; WEAR; PREDICTIONS; COMPOSITES; RESISTANCE; BEHAVIOR;
D O I
10.1016/j.mtcomm.2022.104869
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The AlCoCrFeNi-WC-Ti composite coating exhibits excellent hardness and wear resistance, which mainly comes from the various strengthening mechanisms. An accurate prediction model is crucial for analyzing the hardness contribution of various strengthening mechanisms. In this study, AlCoCrFeNi and AlCoCrFeNiW0.5 supercells were constructed by the special quasi random structure (SQS), and then the elastic moduli were obtained by first principles calculations. Using the elastic moduli, a predicted model was established for the hardness contribu-tion. The results showed that the shear modulus of AlCoCrFeNi and AlCoCrFeNiW0.5 alloys is 80.43 GPa and 68.64 GPa, respectively. Solid solution strengthening with a hardness contribution of 248.5 HV is the dominant strengthening mechanism for the AlCoCrFeNi-WC-Ti composite coating. The sum of hardness contribution is 271.4 HV from various strengthening mechanisms. And compared with the Vickers hardness, the relative error is only 7.4%. For the AlCoCrFeNiW0.5 alloy, namely the coating matrix (CM) of the AlCoCrFeNi-WC-Ti, its sum of hardness contributions is 251.2 HV. Compared with the nanoindentation hardness, the relative error is 4.8%, which indicates that the predicted model is accurate for the hardness contribution.
引用
收藏
页数:10
相关论文
共 56 条
  • [1] [Anonymous], 2015, ISO 14577-1
  • [2] 2-POINT STEP SIZE GRADIENT METHODS
    BARZILAI, J
    BORWEIN, JM
    [J]. IMA JOURNAL OF NUMERICAL ANALYSIS, 1988, 8 (01) : 141 - 148
  • [3] Born M., 1998, DYNAMICAL THEORY CRY
  • [4] Microstructural development in equiatomic multicomponent alloys
    Cantor, B
    Chang, ITH
    Knight, P
    Vincent, AJB
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2004, 375 : 213 - 218
  • [5] Chawla K.K., 2013, METAL MATRIX COMPOSI
  • [6] Additive manufactured high-strength tungsten composite with high deformability by using a novel CoCrNi medium-entropy binder
    Chen, Hui
    Li, Dan
    Geng, Zhaowen
    Wu, Yiyou
    Zhang, Taomei
    Jiang, Xue
    Zhao, Siqi
    Zhang, Hongbo
    Han, Yong
    Liu, Xiaochun
    Chen, Chao
    [J]. COMPOSITES PART B-ENGINEERING, 2022, 246
  • [7] Effect of vanadium addition on the microstructure and properties of AlCoCrFeNi high entropy alloy
    Dong, Yong
    Zhou, Kaiyao
    Lu, Yiping
    Gao, Xiaoxia
    Wang, Tongmin
    Li, Tingju
    [J]. MATERIALS & DESIGN, 2014, 57 : 67 - 72
  • [8] Particulate-reinforced iron-based metal matrix composites fabricated by selective laser melting: A systematic review
    Fang, Yongjian
    Kim, Min-Kyeom
    Zhang, Yali
    Duan, Ziyang
    Yuan, Quan
    Suhr, Jonghwan
    [J]. JOURNAL OF MANUFACTURING PROCESSES, 2022, 74 : 592 - 639
  • [9] Effect of actual WC content on the reciprocating wear of a laser cladding NiCrBSi alloy reinforced with WC
    Fernandez, M. R.
    Garcia, A.
    Cuetos, J. M.
    Gonzalez, R.
    Noriega, A.
    Cadenas, M.
    [J]. WEAR, 2015, 324 : 80 - 89
  • [10] SUBSTITUTIONAL SOLUTION HARDENING
    FLEISCHER, RL
    [J]. ACTA METALLURGICA, 1963, 11 (03): : 203 - &