• Chinese Journal of Lasers
  • Vol. 51, Issue 12, 1202301 (2024)
Hao Wang1、*, Yining Hu2, and Tao Wang2
Author Affiliations
  • 1Engineering Techniques Training Center, Civil Aviation University of China, Tianjin 300300, China
  • 2College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China
  • show less
    DOI: 10.3788/CJL231043 Cite this Article Set citation alerts
    Hao Wang, Yining Hu, Tao Wang. Microstructure and Tribological Properties of Additively Manufactured TC17 Titanium Alloy Under Different Heat Treatment Processes[J]. Chinese Journal of Lasers, 2024, 51(12): 1202301 Copy Citation Text show less
    Morphology and particle size distribution of TC17 alloy powder. (a) Morphology; (b) particle size distribution
    Fig. 1. Morphology and particle size distribution of TC17 alloy powder. (a) Morphology; (b) particle size distribution
    DED process. (a) Experimental environment; (b) TC17 alloy deposition process
    Fig. 2. DED process. (a) Experimental environment; (b) TC17 alloy deposition process
    Heat treatment process of TC17 alloy
    Fig. 3. Heat treatment process of TC17 alloy
    Pin disc wear diagram
    Fig. 4. Pin disc wear diagram
    XRD spectra of TC17 alloy. (a) 2θ=30°‒90°; (b) local magnification of Fig. 5(a)
    Fig. 5. XRD spectra of TC17 alloy. (a) 2θ=30°‒90°; (b) local magnification of Fig. 5(a)
    Microstructure of as-deposited TC17. (a) Microstructure; (b) local magnification of Fig. 6(a)
    Fig. 6. Microstructure of as-deposited TC17. (a) Microstructure; (b) local magnification of Fig. 6(a)
    Microstructures of TC17 alloys. (a1)‒(a3) 840 ℃ pre-annealing; (b1)‒(b3) pre-annealing+800 ℃ solution
    Fig. 7. Microstructures of TC17 alloys. (a1)‒(a3) 840 ℃ pre-annealing; (b1)‒(b3) pre-annealing+800 ℃ solution
    Elemental fluctuation of TC17 alloy in scanning path after 840 ℃ pre-annealing and 800 ℃ solution. (a) Scanning path; (b) elemental signal intensity
    Fig. 8. Elemental fluctuation of TC17 alloy in scanning path after 840 ℃ pre-annealing and 800 ℃ solution. (a) Scanning path; (b) elemental signal intensity
    Microstructures of TC17 alloy under different aging conditions after 840 ℃ pre-annealing and 800 ℃ solution. (a1)‒(a3) 580 ℃ aging; (b1)‒(b3) 630 ℃ aging; (c1)‒(c3) 680 ℃ aging
    Fig. 9. Microstructures of TC17 alloy under different aging conditions after 840 ℃ pre-annealing and 800 ℃ solution. (a1)‒(a3) 580 ℃ aging; (b1)‒(b3) 630 ℃ aging; (c1)‒(c3) 680 ℃ aging
    α phase sizes and volume fraction in TC17 alloy. (a) Length of αP phase; (b) width of αP phase; (c) widths of αGB phase and PFZ; (d) volume fraction of α phase
    Fig. 10. α phase sizes and volume fraction in TC17 alloy. (a) Length of αP phase; (b) width of αP phase; (c) widths of αGB phase and PFZ; (d) volume fraction of α phase
    Microstructure evolution of TC17 alloy during heat treatment. (a) Pre-annealing; (b) solution after pre-annealing; (c) aging at 580 ℃ after pre-annealing and solution; (d) aging at 630 ℃ after pre-annealing and solution; (e) aging at 680 ℃ after pre-annealing and solution
    Fig. 11. Microstructure evolution of TC17 alloy during heat treatment. (a) Pre-annealing; (b) solution after pre-annealing; (c) aging at 580 ℃ after pre-annealing and solution; (d) aging at 630 ℃ after pre-annealing and solution; (e) aging at 680 ℃ after pre-annealing and solution
    Microhardness of TC17 alloys in deposition and heat treatment states. (a) Microhardness curves; (b) average microhardness
    Fig. 12. Microhardness of TC17 alloys in deposition and heat treatment states. (a) Microhardness curves; (b) average microhardness
    Test results of wear properties of TC17 alloy. (a) Friction coefficient curves; (b) average friction coefficients during steady wear phase; (c) wear rate; (d) two dimensional wear profile
    Fig. 13. Test results of wear properties of TC17 alloy. (a) Friction coefficient curves; (b) average friction coefficients during steady wear phase; (c) wear rate; (d) two dimensional wear profile
    Wear surfaces of TC17 alloy in deposition and heat treatment states. (a) Deposition; (b) pre-annealing; (c) solution after pre-annealing; (d) aging at 580 ℃ after pre-annealing and solution; (e) aging at 630 ℃ after pre-annealing and solution; (f) aging at 680 ℃ after pre-annealing and solution
    Fig. 14. Wear surfaces of TC17 alloy in deposition and heat treatment states. (a) Deposition; (b) pre-annealing; (c) solution after pre-annealing; (d) aging at 580 ℃ after pre-annealing and solution; (e) aging at 630 ℃ after pre-annealing and solution; (f) aging at 680 ℃ after pre-annealing and solution
    PowderAlSnZrMoCrFeOTi
    TC175.062.101.973.964.000.220.11Bal.
    Table 1. Chemical compositions of TC17 alloy powder (mass fraction, %)
    Sample2θ /(°)FWHM
    Pre-annealing40.680.30
    Pre-annealing+Solution40.580.36
    Pre-annealing+Solution+630 ℃ Aging40.460.21
    Table 2. 2θ and FWHM at peak 1
    ConditionWear width /mmWear depth /mm
    Deposition2.0560.192
    Pre-annealing2.5040.093
    Pre-annealing+solution2.5380.120
    Pre-annealing+solution+580 ℃ aging1.7890.105
    Pre-annealing+solution+630 ℃ aging1.8300.108
    Pre-annealing+solution+680 ℃ aging2.0390.137
    Table 3. Maximum wear widths and depths of TC17 alloys in deposition and heat treatment states
    PositionMass fraction /%
    AlOSnZrMoCrTi
    12.977.742.171.682.993.55Bal.
    23.9519.91.651.573.253.14Bal.
    33.9617.91.691.583.253.16Bal.
    44.2814.61.932.033.473.18Bal.
    52.7415.21.921.462.913.68Bal.
    64.1420.81.621.833.143.18Bal.
    Table 4. EDS analysis results of oxide layer of TC17 alloy in deposition and heat treatment states
    Hao Wang, Yining Hu, Tao Wang. Microstructure and Tribological Properties of Additively Manufactured TC17 Titanium Alloy Under Different Heat Treatment Processes[J]. Chinese Journal of Lasers, 2024, 51(12): 1202301
    Download Citation