Author Affiliations
1Institute of Civil Aviation Technology, Civil Aviation University of China, Tianjin 300300, China2College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China3Sino-European Institute of Aviation Engineering, Civil Aviation University of China, Tianjin 300300, Chinashow less
Fig. 1. Material powders for cladding. (a) TC4; (b) Ni60
Fig. 2. TruDisk4002 coaxial powder feeding fiber laser
Fig. 3. Macro-morphology of single-pass laser cladding layer
Fig. 4. Cross-sectional SEM morphology of single-pass laser cladding layer
Fig. 5. Gaussian heat source model
Fig. 6. Finite element model
Fig. 7. Thermo-physical performance parameters versus temperature. (a) Thermal conductivity; (b) specific heat; (c) density; (d) linear expansion coefficient
Fig. 8. Mechanical performance parameters versus temperature. (a) Modulus of elasticity; (b) Poisson’s ratio; (c) yield stress
Fig. 9. Comprehensive heat transfer coefficient versus temperature
Fig. 10. Temperature contours at different moments. (a) t=3 s; (b) t=6 s
Fig. 11. Actual high-definition motion track of laser heat source
Fig. 12. Temperature contours of local area at t=3 s. (a) Cross section; (b) longitudinal section; (c) magnification of cross section
Fig. 13. Residual stress contours after cooling. (a) Surface residual stress; (b) cross-sectional residual stress
Fig. 14. Crack morphology of cladding layer. (a) Edge; (b) bonding area
No. | Parameter | Value | Unit |
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1 | Laser power | 1100 | W | 2 | Scanning speed | 400 | mm·min-1 | 3 | Spot diameter | 3.0 | mm | 4 | Power feeding rate | 1.4 | r·min-1 | 5 | Laser focal length | 16 | mm | 6 | Flow of powder feeder | 7 | L·min-1 | 7 | Flow of protection gas | 11 | L·min-1 |
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Table 1.
Process parameters for laser cladding