Author Affiliations
1Institute of Laser Advanced Manufacturing, Zhejiang University of Technology, Hangzhou, Zhejiang 310023, China2Collaborative Innovation Center of High-End Laser Manufacturing Equipment (National "2011 Plan" ), Zhejiang University of Technology, Hangzhou, Zhejiang 310023, China3Zhongzhe High-Speed Railway Bearing Co., Ltd., Quzhou, Zhejiang 324407, Chinashow less
Fig. 1. Microstructure of 42CrMo steel matrix
Fig. 2. Schematic of laser-induction hybrid quenching on 42CrMo steel
Fig. 3. Microhardness curves of laser-induction hybrid quenching hardened layers
Fig. 4. Physical model and locations of feature points
Fig. 5. Schematic of rolling wear test device
Fig. 6. Microstructure of laser-induction hybrid quenching hardened layer
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
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
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
Fig. 10. Sectional crack morphology of fatigue specimen with hardened layer depth of 3.5 mm
Fig. 11. Sectional crack morphology of fatigue specimen with hardened layer depth of 4.5 mm
Fig. 12. Sectional crack morphology of fatigue specimen with hardened layer depth of 6.3 mm
Fig. 13. Schematic of surface cracking under heavy load condition
Fig. 14. Schematic of internal cracking under heavy load condition
Element | C | Si | Mn | Cr | Mo | S | P | Ni | Fe |
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Mass fraction /% | 0.42 | 0.2 | 0.50.8 | 0.91.2 | 0.2 | ≤0.035 | ≤0.035 | 0.03 | Bal. |
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Table 1. Chemical composition of 42CrMo steel
Element | C | O | Fe | Cr | Mn | Si | Ni | Cu | Al | S |
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Mass fraction /% | 5.173 | 19.720 | 71.890 | 1.120 | 1.314 | 0.363 | 0.127 | 0.184 | 0.022 | 0.086 |
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Table 2. Element distribution in area A in Fig. 12