Small fatigue crack growth behavior of Ti-6Al-4V produced via selective laser melting: In situ characterization of a 3D crack tip interactions with defects
Source abstract
Abstract
Abstract Small fatigue crack growth (SFCG) behavior is examined for additively manufactured Ti-6Al-4V specimens with optimal and trial build conditions (representing an increased degree of defects) through a combination of in situ tomography and in situ energy dispersive X-ray diffraction. The results showed slower crack growth rates for the SFCG samples compared to the long cracks (which was not expected). In the case of the trial conditions, the increased levels of porosity deterred crack growth by blunting the crack, as evident by the in situ tomography characterization.
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Research context
OpenAlex topics: Additive Manufacturing Materials and Processes · Additive Manufacturing and 3D Printing Technologies · Welding Techniques and Residual Stresses
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References (61)
Show source-provided references
1. Critical assessment of the fatigue performance of additively manufactured Ti–6Al–4V and perspective for future research10.1016/j.ijfatigue.2015.12.003 ↗
2. On the mechanical behaviour of titanium alloy TiAl6V4 manufactured by selective laser melting: Fatigue resistance and crack growth performance10.1016/j.ijfatigue.2012.11.011 ↗
3. Crack propagation and fracture toughness of Ti6Al4V alloy produced by selective laser melting
4. An experimental study of residual stress and direction-dependence of fatigue crack growth behaviour in as-built and stress-relieved selective-laser-melted Ti6Al4V10.1016/j.msea.2019.04.023 ↗
5. Experimental study of effect of post processing on fracture toughness and fatigue crack growth performance of selective laser melting Ti-6Al-4V
6. Effect of build condition and direction on fatigue crack growth rates of selective laser melted Ti-6Al-4V specimens
7. Effect of build direction on the fracture toughness and fatigue crack growth in selective laser melted Ti-6Al-4 V10.1111/ffe.12303 ↗
8. Fatigue crack growth behavior and microstructural mechanisms in Ti-6Al-4V manufactured by laser engineered net shaping10.1016/j.ijfatigue.2016.08.009 ↗
9. Representing crack growth in additively manufactured Ti-6Al-4V10.1016/j.ijfatigue.2018.07.019 ↗
10. Analyzing the effects of powder and post-processing on porosity and properties of electron beam melted Ti-6Al-4V10.1080/21663831.2017.1340911 ↗
11. On the fatigue crack growth behavior in 316L stainless steel manufactured by selective laser melting10.1016/j.engfracmech.2014.03.008 ↗
12. Fatigue crack growth mechanisms at the microstructure scale in as-fabricated and heat treated Ti-6Al-4V ELI manufactured by electron beam melting10.1016/j.engfracmech.2017.03.024 ↗
13. Effect of micromorphology at the fatigue crack tip on the crack growth in electron beam welded Ti-6Al-4V joint10.1016/j.matchar.2016.08.029 ↗
14. Incorporating grain-level residual stresses and validating a crystal plasticity model of a two-phase Ti-6Al-4 V alloy produced via additive manufacturing10.1016/j.jmps.2018.07.025 ↗
15. Strain localization in Ti-6Al-4V Widmanstätten microstructures produced by additive manufacturing10.1016/j.matchar.2016.10.018 ↗
16. Understanding fatigue crack growth in aluminum alloys by in situ X-ray synchrotron tomography10.1016/j.ijfatigue.2012.06.009 ↗
17. A 3D measurement procedure for internal local crack driving forces via synchrotron X-ray microtomography10.1016/j.actamat.2003.11.014 ↗
18. Predicting the 3D fatigue crack growth rate of small cracks using multimodal data via Bayesian networks: In-situ experiments and crystal plasticity simulations10.1016/j.jmps.2018.03.007 ↗
19. Three-dimensional visualization of ductile fracture in an Al–Si alloy by high-resolution synchrotron X-ray microtomography10.1016/j.msea.2006.10.201 ↗
20. Three-dimensional fatigue crack growth behavior in an aluminum alloy investigated with in situ high-resolution synchrotron X-ray microtomography10.1016/j.actamat.2009.03.036 ↗
21. Direct observation of crack opening as a function of applied load in the interior of a notched tensile sample of Al Li 209010.1016/S1359-6454(96)00311-4 ↗
22. Measuring fatigue crack deflections via cracking of constituent particles in AA7050 via in situ x-ray synchrotron-based micro-tomography10.1016/j.ijfatigue.2018.07.005 ↗
23. In situ experiments with X ray tomography: an attractive tool for experimental mechanics10.1007/s11340-010-9333-7 ↗
24. Measuring the stress field around an evolving crack in tensile deformed Mg AZ31 using three-dimensional X-ray diffraction10.1016/j.actamat.2012.02.054 ↗
25. Combining fractography with high-energy X-ray diffraction to study fatigue crack growth in Ti-6Al-4V
26. Strain profiling of fatigue crack overload effects using energy dispersive X-ray diffraction10.1016/j.ijfatigue.2005.06.022 ↗
27. Crack tip deformation fields and fatigue crack growth rates in Ti–6Al–4V10.1016/j.ijfatigue.2009.02.043 ↗
28. Quantifying fatigue overload retardation mechanisms by energy dispersive X-ray diffraction10.1016/j.jmps.2018.10.020 ↗
29. Defects-dictated tensile properties of selective laser melted Ti-6Al-4V10.1016/j.matdes.2018.08.004 ↗
30. Additive manufacturing of strong and ductile Ti–6Al–4V by selective laser melting via in situ martensite decomposition10.1016/j.actamat.2014.11.028 ↗
31. In situ tailoring microstructure in additively manufactured Ti-6Al-4V for superior mechanical performance10.1016/j.actamat.2016.12.027 ↗
32. A. Standard, E647, Standard test method for measurement of fatigue crack growth rates, Annual Book of ASTM Standards, Section Three: Metals Test Methods and Analytical Procedures 3; 2002. p. 628–670.
33. DOD U. Military Handbook: Metallic Materials and Elements for Aerospace Vehicle Structures, MIL-HDBK-5G, 2 vols. Wright-Patterson AFB, OH: US Department of Defense; 1994.
34. Residual strain analysis in linear friction welds of similar and dissimilar titanium alloys using energy dispersive X-ray diffraction10.1007/s11661-018-5034-0 ↗
35. E384-17 A. Standard test method for microindentation hardness of materials. American Society for Testing of Materials (ASTM) International West; 2017.
36. TomoPy: a framework for the analysis of synchrotron tomographic data10.1107/S1600577514013939 ↗
37. Adaptive center determination for effective suppression of ring artifacts in tomography images10.1063/1.4897441 ↗
38. NIH Image to ImageJ: 25 years of image analysis10.1038/nmeth.2089 ↗
39. Z. Konrad, User's Guide – Avizo; 2017.
40. Role of heat treatment and build orientation in the microstructure sensitive deformation characteristics of IN718 produced via SLM additive manufacturing
41. Liu QC, Elambasseril J, Sun SJ, Leary M, Brandt M, Sharp PK. The effect of manufacturing defects on the fatigue behaviour of Ti-6Al-4V specimens fabricated using selective laser melting. Trans Tech Publ 2014; 1519–24.10.4028/www.scientific.net/AMR.891-892.1519 ↗
42. Elastic anisotropy of HCP metal crystals and polycrystals
43. A study of the microstructural evolution during selective laser melting of Ti–6Al–4V10.1016/j.actamat.2010.02.004 ↗
44. The effect of laser energy input on the microstructure, physical and mechanical properties of Ti-6Al-4V alloys by selective laser melting10.1080/17452759.2016.1142215 ↗
45. Microstructure and mechanical property of selective laser melted Ti6Al4V dependence on laser energy density10.1108/RPJ-12-2015-0193 ↗
46. Lütjering G, Williams JC. Titanium. Springer Science & Business Media; 2007.
47. On the process of transition of the cubic-body-centered modification into the hexagonal-close-packed modification of zirconium10.1016/S0031-8914(34)80244-3 ↗
48. Determination of the orientation of a parent β grain from the orientations of the inherited α plates in the phase transformation from body-centred cubic to hexagonal close packed10.1107/S0021889895004067 ↗
49. The calculation of a parent grain orientation from inherited variants for approximate (bcc–hcp) orientation relations10.1107/S0021889802005824 ↗
50. ARPGE: a computer program to automatically reconstruct the parent grains from electron backscatter diffraction data10.1107/S0021889807048777 ↗
51. A method to determine the orientation of the high-temperature beta phase from measured EBSD data for the low-temperature alpha phase in Ti-6Al-4V10.1016/S0921-5093(02)00535-X ↗
52. An automated method to determine the orientation of the high-temperature beta phase from measured EBSD data for the low-temperature alpha-phase in Ti–6Al–4V10.1016/S0921-5093(02)00844-4 ↗
53. Bachmann F, Hielscher R, Schaeben H. Texture analysis with MTEX–free and open source software toolbox. Trans Tech Publ 2010; 63–8.10.4028/www.scientific.net/SSP.160.63 ↗
54. Simonelli M, Tse YY, Tuck C. Further understanding of Ti-6Al-4V selective laser melting using texture analysis 2012; 1–4.
55. Microstructures and mechanical properties of Ti6Al4V parts fabricated by selective laser melting and electron beam melting10.1007/s11665-013-0658-0 ↗
56. Microstructure and texture evolution during solidification processing of Ti–6Al–4V10.1016/S0924-0136(02)00865-8 ↗
57. Effects of internal porosity and crystallographic texture on Charpy absorbed energy of electron beam melting titanium alloy (Ti-6Al-4V)10.1016/j.msea.2018.11.005 ↗
58. Rice RC, Jackson JL, Bakuckas J, Thompson S. Metallic materials properties development and standardization. MMPDS). National Technical Information Service, cap. 2003 Jan:1-4.
59. Dhansay NM, Tait R, Becker T. Fatigue and fracture toughness of Ti-6Al-4V titanium alloy manufactured by selective laser melting. Trans Tech Publ 2014; 248–53.10.4028/www.scientific.net/AMR.1019.248 ↗
60. Evaluation of fatigue crack propagation behaviour in Ti-6Al-4V manufactured by selective laser melting10.1016/j.ijfatigue.2017.07.014 ↗
61. A crack growth evaluation method for interacting multiple cracks10.1299/jsmea.46.15 ↗