Author Affiliations
1Engineering Techniques Training Center, Civil Aviation University of China, Tianjin 300300, China2College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, Chinashow less
Fig. 1. Morphology and particle size distribution of TC17 alloy powder. (a) Morphology; (b) particle size distribution
Fig. 2. DED process. (a) Experimental environment; (b) TC17 alloy deposition process
Fig. 3. Heat treatment process of TC17 alloy
Fig. 4. Pin disc wear diagram
Fig. 5. XRD spectra of TC17 alloy. (a) 2θ=30°‒90°; (b) local magnification of Fig. 5(a)
Fig. 6. Microstructure of as-deposited TC17. (a) Microstructure; (b) local magnification of Fig. 6(a)
Fig. 7. Microstructures of TC17 alloys. (a1)‒(a3) 840 ℃ pre-annealing; (b1)‒(b3) pre-annealing+800 ℃ solution
Fig. 8. Elemental fluctuation of TC17 alloy in scanning path after 840 ℃ pre-annealing and 800 ℃ solution. (a) Scanning path; (b) elemental signal intensity
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
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
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
Fig. 12. Microhardness of TC17 alloys in deposition and heat treatment states. (a) Microhardness curves; (b) average microhardness
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
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
Powder | Al | Sn | Zr | Mo | Cr | Fe | O | Ti |
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TC17 | 5.06 | 2.10 | 1.97 | 3.96 | 4.00 | 0.22 | 0.11 | Bal. |
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Table 1. Chemical compositions of TC17 alloy powder (mass fraction, %)
Sample | 2θ /(°) | FWHM |
---|
Pre-annealing | 40.68 | 0.30 | Pre-annealing+Solution | 40.58 | 0.36 | Pre-annealing+Solution+630 ℃ Aging | 40.46 | 0.21 |
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Table 2. 2θ and FWHM at peak 1
Condition | Wear width /mm | Wear depth /mm |
---|
Deposition | 2.056 | 0.192 | Pre-annealing | 2.504 | 0.093 | Pre-annealing+solution | 2.538 | 0.120 | Pre-annealing+solution+580 ℃ aging | 1.789 | 0.105 | Pre-annealing+solution+630 ℃ aging | 1.830 | 0.108 | Pre-annealing+solution+680 ℃ aging | 2.039 | 0.137 |
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Table 3. Maximum wear widths and depths of TC17 alloys in deposition and heat treatment states
Position | Mass fraction /% |
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Al | O | Sn | Zr | Mo | Cr | Ti |
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1 | 2.97 | 7.74 | 2.17 | 1.68 | 2.99 | 3.55 | Bal. | 2 | 3.95 | 19.9 | 1.65 | 1.57 | 3.25 | 3.14 | Bal. | 3 | 3.96 | 17.9 | 1.69 | 1.58 | 3.25 | 3.16 | Bal. | 4 | 4.28 | 14.6 | 1.93 | 2.03 | 3.47 | 3.18 | Bal. | 5 | 2.74 | 15.2 | 1.92 | 1.46 | 2.91 | 3.68 | Bal. | 6 | 4.14 | 20.8 | 1.62 | 1.83 | 3.14 | 3.18 | Bal. |
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Table 4. EDS analysis results of oxide layer of TC17 alloy in deposition and heat treatment states