• Chinese Journal of Lasers
  • Vol. 49, Issue 8, 0802023 (2022)
Qunli Zhang1、2, Hua Huang1、2, Zehao Tang1、2, Guochang Li1、2, Qing’an Niu1、2, Zhijun Chen1、2, Yangqiong Du3, and Jianhua Yao1、2、*
Author Affiliations
  • 1Institute of Laser Advanced Manufacturing, Zhejiang University of Technology, Hangzhou, Zhejiang 310023, China
  • 2Collaborative Innovation Center of High-End Laser Manufacturing Equipment (National "2011 Plan" ), Zhejiang University of Technology, Hangzhou, Zhejiang 310023, China
  • 3Zhongzhe High-Speed Railway Bearing Co., Ltd., Quzhou, Zhejiang 324407, China
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    DOI: 10.3788/CJL202249.0802023 Cite this Article Set citation alerts
    Qunli Zhang, Hua Huang, Zehao Tang, Guochang Li, Qing’an Niu, Zhijun Chen, Yangqiong Du, Jianhua Yao. Rolling Wear and Fatigue Damage Behavior of Laser-Induction Hybrid Quenching on 42CrMo Steel[J]. Chinese Journal of Lasers, 2022, 49(8): 0802023 Copy Citation Text show less
    Microstructure of 42CrMo steel matrix
    Fig. 1. Microstructure of 42CrMo steel matrix
    Schematic of laser-induction hybrid quenching on 42CrMo steel
    Fig. 2. Schematic of laser-induction hybrid quenching on 42CrMo steel
    Microhardness curves of laser-induction hybrid quenching hardened layers
    Fig. 3. Microhardness curves of laser-induction hybrid quenching hardened layers
    Physical model and locations of feature points
    Fig. 4. Physical model and locations of feature points
    Schematic of rolling wear test device
    Fig. 5. Schematic of rolling wear test device
    Microstructure of laser-induction hybrid quenching hardened layer
    Fig. 6. Microstructure of laser-induction hybrid quenching hardened layer
    Residual stress distributions of hardened layer samples with different depths. (a) Residual stress distribution of 3.5 mm depth specimen along X direction; (b) residual stress distribution of 3.5 mm depth specimen along Y direction; (c) residual stress distribution of 4.5 mm depth specimen along X direction; (d) residual stress distribution of 4.5 mm depth specimen along Y direction; (e) residual stress distribution of 6.3 mm depth specimen along X direction; (f) residual stress distribution of 6.3 mm depth specimen along Y direction
    Fig. 7. Residual stress distributions of hardened layer samples with different depths. (a) Residual stress distribution of 3.5 mm depth specimen along X direction; (b) residual stress distribution of 3.5 mm depth specimen along Y direction; (c) residual stress distribution of 4.5 mm depth specimen along X direction; (d) residual stress distribution of 4.5 mm depth specimen along Y direction; (e) residual stress distribution of 6.3 mm depth specimen along X direction; (f) residual stress distribution of 6.3 mm depth specimen along Y direction
    Surface damage morphologies of fatigue specimens with different depths of hardened layers. (a) Specimen with 3.5 mm depth; (b) specimen with 4.5 mm depth; (c) specimen with 6.3 mm depth
    Fig. 8. Surface damage morphologies of fatigue specimens with different depths of hardened layers. (a) Specimen with 3.5 mm depth; (b) specimen with 4.5 mm depth; (c) specimen with 6.3 mm depth
    Three-dimensional morphologies and two-dimensional profiles of cross-section for fatigue specimens with different depths of hardened layers. (a) Specimen with 3.5 mm depth; (b) specimen with 4.5 mm depth; (c) specimen with 6.3 mm depth
    Fig. 9. Three-dimensional morphologies and two-dimensional profiles of cross-section for fatigue specimens with different depths of hardened layers. (a) Specimen with 3.5 mm depth; (b) specimen with 4.5 mm depth; (c) specimen with 6.3 mm depth
    Sectional crack morphology of fatigue specimen with hardened layer depth of 3.5 mm
    Fig. 10. Sectional crack morphology of fatigue specimen with hardened layer depth of 3.5 mm
    Sectional crack morphology of fatigue specimen with hardened layer depth of 4.5 mm
    Fig. 11. Sectional crack morphology of fatigue specimen with hardened layer depth of 4.5 mm
    Sectional crack morphology of fatigue specimen with hardened layer depth of 6.3 mm
    Fig. 12. Sectional crack morphology of fatigue specimen with hardened layer depth of 6.3 mm
    Schematic of surface cracking under heavy load condition
    Fig. 13. Schematic of surface cracking under heavy load condition
    Schematic of internal cracking under heavy load condition
    Fig. 14. Schematic of internal cracking under heavy load condition
    ElementCSiMnCrMoSPNiFe
    Mass fraction /%0.420.20.50.80.91.20.2≤0.035≤0.0350.03Bal.
    Table 1. Chemical composition of 42CrMo steel
    ElementCOFeCrMnSiNiCuAlS
    Mass fraction /%5.17319.72071.8901.1201.3140.3630.1270.1840.0220.086
    Table 2. Element distribution in area A in Fig. 12
    Qunli Zhang, Hua Huang, Zehao Tang, Guochang Li, Qing’an Niu, Zhijun Chen, Yangqiong Du, Jianhua Yao. Rolling Wear and Fatigue Damage Behavior of Laser-Induction Hybrid Quenching on 42CrMo Steel[J]. Chinese Journal of Lasers, 2022, 49(8): 0802023
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