Investigation of the mechanisms by which hot isostatic pressing improves the fatigue performance of powder bed fused Ti-6Al-4V
Source abstract
Abstract
Hot isostatic pressing (HIP) is often needed to obtain powder bed fused (PBF) Ti-6Al-4V parts with good fatigue performance. This manuscript attempts to clarify the mechanisms through which HIP treatment acts to improve high cycle fatigue performance. Several mechanisms are considered and examined against experimental data sets available in the literature. The results suggest that HIP may act most significantly by decreasing the fraction of the defect population that can initiate fatigue cracks, both by decreasing defect sizes below a threshold and by changing the microstructure that surrounds defects. Given the novelty of the latter conclusion, an electron backscatter diffraction microscopy study was performed for validation. The gained understanding provides initial guidance on the choice of optimum HIP soak parameters (Temperature-Pressure-Time) for the high cycle fatigue performance of PBF Ti-6Al-4V.
Source: europepmc · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Additive Manufacturing Materials and Processes · Titanium Alloys Microstructure and Properties · Additive Manufacturing and 3D Printing Technologies
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References (71)
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. Fundamental aspects of hot isostatic pressing: an overview10.1007/s11661-000-0078-2 ↗
3. ASTM F2924-14 Standard Specification for Additive Manufacturing Titanium-6 Aluminum-4 Vanadium with Powder Bed Fusion. West Conshohocken, PA: ASTM International; 2014. .
4. Titanium Alloy Castings, Investment 6Al - 4V Hot Isostatic Pressed, Anneal Optional. AMS; 1980. .
5. Metallic Materials Properties Development and Standardization (MMPDS-05). Battelle Memorial Institute; 2010.
6. Fatigue performance of laser additive manufactured Ti-6Al-4V in very high cycle fatigue regime up to 109 cycles10.3389/fmats.2015.00072 ↗
7. Defect distribution and microstructure heterogeneity effects on fracture resistance and fatigue behavior of EBM Ti-6Al-4V10.1016/j.ijfatigue.2016.06.001 ↗
8. Lütjering · 2007
9. Rekedal KD, Liu D. Fatigue life of selective laser melted and hot isostatically pressed Ti-6Al-4V absent of surface machining. In: Proceedings of the 56th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference, Kissimmee, FL; 2015.10.2514/6.2015-0894 ↗
10. A comparison of the tensile, fatigue, and fracture behavior of Ti-6Al-4V and 15-5 PH stainless steel parts made by selective laser melting10.1007/s00170-013-5106-7 ↗
11. 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 ↗
12. Improvement of fatigue resistance and ductility of TiAl6V4 processed by selective laser melting10.1016/j.jmatprotec.2015.01.025 ↗
13. On the fatigue properties of metals manufactured by selective laser melting-the role of ductility10.1557/jmr.2014.157 ↗
14. Computed tomography for characterization of fatigue performance of selective laser melted parts10.1016/j.matdes.2015.06.063 ↗
15. Quintus Technology. The ultimate heat treatment solution brochure; 2018.
16. Comparison of the microstructures and mechanical properties of Ti-6Al-4V fabricated by selective laser melting and electron beam melting10.1016/j.matdes.2015.12.135 ↗
17. Fatigue performance of additive manufactured TiAl6V4 using electron and laser beam melting10.1016/j.ijfatigue.2016.05.001 ↗
18. The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminum
19. Fatigue life of additively manufactured Ti-6Al-4V in the very high cycle fatigue regime10.1016/j.ijfatigue.2016.05.018 ↗
20. The effectiveness of hot isostatic pressing for closing porosity in titanium parts manufactured by selective electron beam melting10.1007/s11661-016-3429-3 ↗
21. Fatigue performance evaluation of selective laser melted Ti-6Al-4V10.1016/j.msea.2014.01.041 ↗
22. Influence of defects on mechanical properties of Ti-6Al-4V components produced by selective laser melting and electron beam melting10.1016/j.matdes.2015.07.147 ↗
23. Effects of defects in laser additive manufactured Ti-6Al-4V on fatigue properties10.1016/j.phpro.2014.08.120 ↗
24. The effect of manufacturing defects on the fatigue behaviour of Ti-6Al-4V specimens fabricated using selective laser melting
25. Titanium alloys at extreme pressure conditions
26. The positive effect of hot isostatic pressing on improving the anisotropies of bending and impact properties in selective laser melted Ti-6Al-4V alloy10.1016/j.msea.2016.02.023 ↗
27. Microstructure and tensile properties of selectively laser-melted and of HIPed laser-melted Ti-6Al-4V10.1016/j.msea.2013.04.099 ↗
28. Effects of post-processing on cyclic fatigue response of a titanium alloy additively manufactured by electron beam melting10.1016/j.msea.2016.10.059 ↗
29. Microstructure and mechanical properties of long Ti-6Al-4V rods additively manufactured by selective electron beam melting out of a deep powder bed and the effect of subsequent hot isostatic pressing10.1007/s11661-015-2976-3 ↗
30. Porosity measurements by x-ray computed tomography: accuracy evaluation using a calibrated object10.1016/j.precisioneng.2017.03.007 ↗
31. X-ray computed tomography for additive manufacturing: a review10.1088/0957-0233/27/7/072001 ↗
32. Fatigue strength prediction for titanium alloy TiAl6V4 manufactured by selective laser melting10.1007/s11661-015-2864-x ↗
33. Solubility of argon in laser additive manufactured α-titanium under hot isostatic pressing condition10.1016/j.commatsci.2017.01.040 ↗
34. Analyzing the effects of powder and post-processing on porosity and properties of electron beam melted Ti-6Al-4V10.1080/21663831.2017.1340911 ↗
35. Porosity regrowth during heat treatment of hot isostatically pressed additively manufactured titanium components10.1016/j.scriptamat.2016.05.002 ↗
36. The influence of porosity on fatigue crack initiation in additively manufactured titanium components10.1038/s41598-017-06504-5 ↗
37. Murakami · 2002
38. Fatigue strength of Ti-6Al-4V alloys containing small artificial defects10.2472/jsms.52.12Appendix_263 ↗
39. Fatigue crack initiation in hot isostatically pressed Ti-6Al-4V castings10.1007/BF00551032 ↗
40. Crystallography of fatigue crack initiation and growth in fully lamellar Ti-6Al-4V10.1007/s11661-009-0064-2 ↗
41. Effects of defects, surface roughness and hip on fatigue strength of Ti-6Al-4V manufactured by additive manufacturing10.1016/j.prostr.2017.11.055 ↗
42. Zhang B, Ham K, Shao S, Shamsaei N, Thompson SM. Effect of heat treatment and hot isostatic pressing on the morphology and size of pores in additive manufactured Ti-6Al-4V parts, SFFs, 2017.
43. The effect of porosity on the fatigue life of cast aluminium-silicon alloys10.1111/j.1460-2695.2004.00780.x ↗
44. Modeling of processing-induced pore morphology in an additively-manufactured Ti-6Al-4V alloy10.3390/ma10020145 ↗
45. ABAQUS, 6.14 documentation, Dassault Systemes Simulia Corporation; 2014.
46. Ingrafea · 1996
47. ASTM E399-17 standard test method for linear-elastic plane-strain fracture toughness KIc of metallic materials. West Conshohocken, PA: ASTM International; 2017.
48. Three-dimensional problems of strongly interacting arbitrarily located penny-shaped cracks10.1007/BF00018861 ↗
49. The asymptotic theory of extreme order statistics
50. Relationship between fatigue life distribution, notch configuration, and SN curve of a 2024-T4 aluminum alloy10.1115/1.3225804 ↗
51. Effect of stress amplitude on statistical variability in fatigue life of 75S-T6 aluminum alloy
52. Size effect in randomly loaded specimens10.1016/0142-1123(86)90026-5 ↗
53. Nonparametric estimation from incomplete observations10.1080/01621459.1958.10501452 ↗
54. Fatigue life distribution and size effect in ductile cast iron for wind turbine components10.1016/j.engfailanal.2010.07.001 ↗
55. As-fabricated and heat-treated microstructures of the Ti-6Al-4V alloy processed by selective laser melting10.1007/s11661-011-0731-y ↗
56. Friedman JH, Stuetzle W. The in-out method for linear regression with censored data. Technical report, Stanford University Technical Report; 1981.
57. Microstructural evolution and mechanical properties of powder metallurgy Ti-6Al-4V alloy based on heat response10.1016/j.msea.2015.05.041 ↗
58. Effect of hot isostatic pressing conditions and cooling rate on microstructure and properties of Ti-6Al-4V alloy from atomized powder10.1016/j.jmst.2014.04.011 ↗
59. Effect of hot-isostatic-pressing parameters on the microstructure and properties of powder Ti-6Al-4V hot-isostatically-pressed samples10.1007/s11661-009-0149-y ↗
60. Effect of hot isostatic pressing procedure on performance of Ti6Al4V: surface qualities, microstructure and mechanical properties10.1016/j.jallcom.2016.05.280 ↗
61. Inagaki Shirai Y, Cho IK, Niinomi M. Effects of hot working conditions on fatigue strength of Ti-6Al-4V alloy. In: Proceedings of the 13th world conference on titanium. Wiley Online Library; 2016. p. 811–5.10.1002/9781119296126.ch138 ↗
62. The effect of processing on the 455°C tensile and fatigue behavior of boron-modified Ti-6Al-4V10.1016/j.ijfatigue.2009.04.013 ↗
63. Flow behavior and globularization kinetics during hot working of Ti-6Al-4V with a colony alpha microstructure10.1016/S0921-5093(98)01156-3 ↗
64. The effect of hot deformation parameters on microstructure evolution of the α-phase in Ti-6Al-4V10.1007/s11661-016-3552-1 ↗
65. Pressure sintering by power law creep10.1016/0001-6160(75)90136-4 ↗
66. Studies of the growth and collapse of voids in viscous solids10.1115/1.2904298 ↗
67. Hot isostatic pressing diagrams: new developments10.1016/0001-6160(85)90177-4 ↗
68. Microstructural mechanisms during hot working of commercial grade Ti-6Al-4V with lamellar starting structure10.1016/S0921-5093(01)01448-4 ↗
69. Hot working of commercial Ti-6Al-4V with an equiaxed α–β microstructure: materials modeling considerations10.1016/S0921-5093(00)00741-3 ↗
70. Hot deformation behavior of Ti-6Al-4V alloy: effect of initial microstructure10.1016/j.jallcom.2017.05.097 ↗
71. The variation of strain rate sensitivity exponent and strain hardening exponent in isothermal compression of Ti-6Al-4V alloy10.1016/j.matdes.2009.09.055 ↗