Effects of post-processing and loading orientation on high-cycle fatigue of selective laser melted Ti-6Al-4V
Source abstract
Abstract
Recent research on selective laser melted (SLM) Ti-6Al-4V showed that fatigue fracture differs depending on the post-processing and loading orientation. To better understand their influences, tensile and fatigue tests on samples with three post-processing conditions, namely, stress relief (SR), Sub-transus and hot-isostatic-pressing (HIP), were conducted in both the vertical and horizontal loading orientations. The elongation-to-failure of horizontal specimens are consistently higher than the vertical ones for the SR and Sub-transus state, but the opposite trend is observed for the HIP state. This discrepancy is owing to the reduced defect in combination with the {112¯0}α preferred orientation. Comparison of the SR and Sub-transus states suggests that coarser α-lath contributes to a longer initiation phase of microcrack from the defect, which improves overall fatigue performance. Fatigue strength of the HIP state is significantly higher than the other two states, exhibiting little anisotropy, and the fatigue-cracking source shifts from the defect to the microstructural facet. Subsequently, a model is proposed to evaluate the high-cycle fatigue of SLM-built Ti-6Al-4V, by incorporating yield strength and elongation-to-failure as additional variables, achieving the life prediction error band within two to five times with respect to the experimental data.
Source: openalex_inverted_index · Quality: baseline
Research context
OpenAlex topics: Additive Manufacturing Materials and Processes · Welding Techniques and Residual Stresses · High Entropy Alloys Studies
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (51)
Show source-provided references
1. Additive manufacturing of strong and ductile Ti–6Al–4V by selective laser melting via in situ martensite decomposition10.1016/j.actamat.2014.11.028 ↗
2. Revealing the intensified preferred orientation and factors dominating the anisotropic mechanical properties of laser powder bed fusion Ti-6Al-4V alloy after heat treatment10.1016/j.jallcom.2023.169494 ↗
3. Near-threshold fatigue crack growth rates of laser powder bed fusion produced Ti-6Al-4V10.1016/j.actamat.2020.07.049 ↗
4. Mechanism of porosity formation and influence on mechanical properties in selective laser melting of Ti-6Al-4V parts10.1016/j.matdes.2018.06.049 ↗
5. The role of lattice defects, element partitioning and intrinsic heat effects on the microstructure in selective laser melted Ti-6Al-4V10.1016/j.actamat.2019.01.039 ↗
6. Effect of heat treatment on the tensile behavior of selective laser melted Ti-6Al-4V by in situ X-ray characterization10.1016/j.actamat.2020.03.003 ↗
7. Effect of HIP post-processing at 850° C/200 MPa in the fatigue behavior of Ti-6Al-4V alloy fabricated by Selective Laser Melting10.1016/j.ijfatigue.2022.107097 ↗
8. Effect of the build orientation on the mechanical properties and fracture modes of SLM Ti–6Al–4V10.1016/j.msea.2014.07.086 ↗
9. Coupling effects of microstructure and defects on the fatigue properties of laser powder bed fusion Ti-6Al-4V
10. Microstructure and defect sensitivities in the very high-cycle fatigue response of Laser Powder Bed Fused Ti–6Al–4V10.1016/j.ijfatigue.2023.107710 ↗
11. Anisotropic tensile behavior of Ti–6Al–4V components fabricated with directed energy deposition additive manufacturing10.1016/j.actamat.2014.12.054 ↗
12. In-situ investigation on the anisotropic behavior of the additively manufactured dual-phase Ti-6Al-4V alloy10.1016/j.matchar.2022.112003 ↗
13. Defects-dictated tensile properties of selective laser melted Ti-6Al-4V10.1016/j.matdes.2018.08.004 ↗
14. The anisotropy of high cycle fatigue property and fatigue crack growth behavior of Ti–6Al–4V alloy fabricated by high-power laser metal deposition10.1016/j.msea.2022.143745 ↗
15. High cycle fatigue behavior of a selective laser melted Ti6Al4V alloy: Anisotropy, defects effect and life prediction10.1016/j.ijfatigue.2022.107252 ↗
16. Anisotropic fatigue performance of directed energy deposited Ti-6Al-4V: Effects of build orientation10.1016/j.msea.2023.145112 ↗
17. A comparison of fatigue strength sensitivity to defects for materials manufactured by AM or traditional processes10.1016/j.ijfatigue.2016.06.020 ↗
18. X-ray imaging of defect population and the effect on high cycle fatigue life of laser additive manufactured Ti6Al4V alloys10.1016/j.ijfatigue.2022.106979 ↗
19. Microstructure and texture evolution in a post-dynamic recrystallized titanium during annealing, monotonic and cyclic loading10.1007/s11661-020-06071-x ↗
20. The effects of powder reuse on the mechanical response of electron beam additively manufactured Ti6Al4V parts
21. Formation of a transition V-rich structure during the α'to α+ β phase transformation process in additively manufactured Ti-6Al-4V10.1016/j.actamat.2022.118104 ↗
22. The role of crystallographic and geometrical relationships between α and β phases in an α/β titanium alloy10.1016/S1359-6454(03)00179-4 ↗
23. Defect-associated microstructure evolution and deformation heterogeneities in additively manufactured 316L stainless steel10.1016/j.msea.2022.144287 ↗
24. Microstructure, mechanical properties and cracking behaviour in a γ′-precipitation strengthened nickel-base superalloy fabricated by electron beam melting10.1016/j.matdes.2018.08.054 ↗
25. Improvement of fatigue resistance and ductility of TiAl6V4 processed by selective laser melting10.1016/j.jmatprotec.2015.01.025 ↗
26. Effects of defects in laser additive manufactured Ti-6Al-4V on fatigue properties10.1016/j.phpro.2014.08.120 ↗
27. Competing crack initiation behaviors of a laser additively manufactured nickel-based superalloy in high and very high cycle fatigue regimes10.1016/j.ijfatigue.2020.105580 ↗
28. Investigating post-processing impact on fatigue performance in LPBF Ti6Al4V with heat treatment, high pressure heat treatment, and dry electropolishing strategies10.1016/j.ijfatigue.2024.108365 ↗
29. Internal fatigue crack propagation in a Ti-6Al-4V alloy: An in situ study10.1016/j.ijfatigue.2022.107450 ↗
30. Quantitative evaluation of effects of non-metallic inclusions on fatigue strength of high strength steels. I: Basic fatigue mechanism and evaluation of correlation between the fatigue fracture stress and the size and location of non-metallic inclusions10.1016/0142-1123(89)90054-6 ↗
31. Fabrication of artificial defects to study internal fatigue crack propagation in metals10.1016/j.scriptamat.2019.05.018 ↗
32. Krupp U. Fatigue crack propagation in metals and alloys: microstructural aspects and modelling concepts. 2007: Wiley Online Library.10.1002/9783527610686 ↗
33. Processing titanium alloys for optimum fatigue performance10.1016/S0142-1123(99)00061-4 ↗
34. Fatigue Crack Initiation and Facet Formation in Ti-6Al-4V
35. Different post-processing methods to improve fatigue properties of additively built Ti-6Al-4V alloy10.1016/j.ijfatigue.2023.107850 ↗
36. High temperature fatigue behavior of a near-alpha titanium alloy10.1016/j.ijfatigue.2022.106918 ↗
37. The effect of the residual stresses generated by surface finishing methods on the very high cycle fatigue behavior of matrix HSS10.1016/j.ijfatigue.2010.07.009 ↗
38. Fatigue life and mechanistic modeling of interior micro-defect induced cracking in high cycle and very high cycle regimes10.1016/j.actamat.2018.07.036 ↗
39. Fatigue life evaluation of Ti–6Al–4V welded joints manufactured by electron beam melting10.1111/ffe.13490 ↗
40. The potency of defects on fatigue of additively manufactured metals10.1016/j.ijmecsci.2022.107185 ↗
41. The nature and the mechanism of crack initiation and early growth for very-high-cycle fatigue of metallic materials–An overview10.1016/j.tafmec.2017.05.002 ↗
42. The role of microstructural evolution on the fatigue behavior of additively manufactured Ti–6Al–4V alloy10.1016/j.msea.2022.144232 ↗
43. Effect of heat treatment on the phase transformation and mechanical properties of Ti6Al4V fabricated by selective laser melting10.1016/j.jallcom.2018.06.076 ↗
44. Effects of defects on tensile and fatigue behaviors of selective laser melted titanium alloy in very high cycle regime10.1016/j.ijfatigue.2020.105795 ↗
45. Fatigue performance of laser additive manufactured Ti–6Al–4V in very high cycle fatigue regime up to 109 cycles10.3389/fmats.2015.00072 ↗
46. An experimental investigation of fatigue performance and crack initiation characteristics for an SLMed Ti-6Al-4V under different stress ratios up to very-high-cycle regime10.1016/j.ijfatigue.2022.107119 ↗
47. Low-and high-cycle fatigue resistance of Ti-6Al-4V ELI additively manufactured via selective laser melting: Mean stress and defect sensitivity10.1016/j.ijfatigue.2017.10.021 ↗
48. Microstructures and mechanical properties of Ti6Al4V parts fabricated by selective laser melting and electron beam melting10.1007/s11665-013-0658-0 ↗
49. Influence of defects on mechanical properties of Ti–6Al–4 V components produced by selective laser melting and electron beam melting10.1016/j.matdes.2015.07.147 ↗
50. Comparative study of fatigue properties of Ti-6Al-4V specimens built by electron beam melting (EBM) and selective laser melting (SLM)10.1016/j.matchar.2018.03.028 ↗
51. Walker · The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminum · 1970