Tailoring the theory of critical distances to better assess the combined effect of complex geometries and process-inherent defects during the fatigue assessment of SLM Ti-6Al-4V
Source abstract
Abstract
This work aims to apply the Theory of Critical Distances (TCD) to the fatigue assessment of additively manufactured (AM) Ti-6Al-4V material produced via the selective laser melting (SLM) process. Modified alternatives to traditional TCD methods are considered. In this sense, it is sought to develop a fatigue prediction model that is better suited to assessing the impact of multiple stress-rising features which are located in close proximity to each other. Hereby, consideration has been given to modelling process-inherent surface roughness in combination with an internally positioned artificial defect, shaped as a feature that is reminiscent of a pore. Simultaneously, the research also seeks to circumnavigate a potential issue with respect to the current TCD methodology. This concerns the matter of applying TCD practices to components whereby the area of interest for conducting stress-distance analytics is on a size scale that is smaller than that of the critical distance length parameter itself. Several different strategies were attempted as a way to try and achieve meaningful modifications to the TCD process. Results show that it is possible to overcome such challenges that can often present themselves during the fatigue appraisal of AM metal parts. In this sense, the optimal novel strategy that was experimented with returned average error margins of 13.7% or better. It is anticipated that such models may assist in further optimising the accuracy of service life evaluation for metallic AM components that are intended for industry.
Source: openalex_inverted_index · Quality: baseline
Research context
OpenAlex topics: Additive Manufacturing Materials and Processes · Additive Manufacturing and 3D Printing Technologies · Welding Techniques and Residual Stresses
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (46)
Show source-provided references
1. Polmear I, StJohn D, Nie JF, Qian M. Titanium alloys; 2017.10.1016/B978-0-08-099431-4.00007-5 ↗
2. Advances in medical applications of additive manufacturing10.1016/j.eng.2020.02.018 ↗
3. Liu · 2017
4. Materials for additive manufacturing10.1016/j.cirp.2017.05.009 ↗
5. Selective laser melting of Ti6Al4V alloy: Process parameters, defects and post-treatments10.1016/j.jmapro.2021.01.009 ↗
6. Additive manufacturing of Ti6Al4V alloy: A review10.1016/j.matdes.2018.107552 ↗
7. Fatigue performance of additive manufactured TiAl6V4 using electron and laser beam melting10.1016/j.ijfatigue.2016.05.001 ↗
8. Fatigue performance evaluation of selective laser melted Ti-6Al-4V10.1016/j.msea.2014.01.041 ↗
9. Evaluation of low cycle fatigue performance of selective laser melted titanium alloy Ti-6Al-4V10.3390/met9101041 ↗
10. High Cycle Fatigue (HCF) Performance of Ti-6Al-4V Alloy Processed by Selective Laser Melting10.4028/www.scientific.net/AMR.816-817.134 ↗
11. High cycle fatigue in selective laser melted Ti-6Al-4V10.1016/j.actamat.2020.05.041 ↗
12. Fatigue life of additively manufactured Ti–6Al–4V in the very high cycle fatigue regime10.1016/j.ijfatigue.2016.05.018 ↗
13. Fatigue Performance of Selective Laser Melted Ti-6Al-4V Components: State of The Art
14. A survey of fatigue properties from wrought and additively manufactured Ti-6Al-4V10.1016/j.matlet.2020.128800 ↗
15. A Review of the As-Built SLM Ti-6Al-4V Mechanical Properties towards Achieving Fatigue Resistant Designs10.3390/met8010075 ↗
16. Fatigue Performance of Powder Metallurgy (PM) Ti-6Al-4V Alloy: A Critical Analysis of Current Fatigue Data and Metallurgical Approaches for Improving Fatigue Strength10.1007/s11837-016-1821-5 ↗
17. High Cycle Fatigue Performance Evaluation of a Laser Powder Bed Fusion Manufactured Ti-6Al-4V Bracket for Aero-Engine Applications
18. H. Duong Bui, J.-B. Leblond, and N. Stalin-Muller, “Background on Fracture Mechanics,” in Handbook of Materials Behaviour Models, 2001, pp. 549–557.10.1016/B978-012443341-0/50061-2 ↗
19. Limitations of Linear Elastic Fracture Mechanics in Respect of Small Fatigue Cracks and Microstructure10.1111/j.1460-2695.1986.tb01207.x ↗
20. Evaluation on Limitation of Linear Elastic Fracture Mechanics for Small Fatigue Crack Growth10.1111/j.1460-2695.1987.tb00207.x ↗
21. H. Neuber, Theory of notch stresses: principles for exact calculation of strength with reference to structural form and material, 2nd Editio. 1958.
22. Notch Sensitivity
23. D. Taylor, The Theory of Critical Distances: A New Perspective in Fracture Mechanics. 2007.10.1016/B978-008044478-9/50003-X ↗
24. 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 ↗
25. On the determination of fatigue properties of Ti6Al4V produced by selective laser melting
26. Applications of the theory of critical distances in failure analysis10.1016/j.engfailanal.2010.07.002 ↗
27. A novel formulation of the theory of critical distances to estimate lifetime of notched components in the medium-cycle fatigue regime10.1111/j.1460-2695.2007.01122.x ↗
28. Fatigue behaviour of notched additive manufactured Ti6Al4V with as-built surfaces10.1016/j.ijfatigue.2017.04.009 ↗
29. Empirical Approach to Understanding the Fatigue Behavior of Metals Made Using Additive Manufacturing10.1007/s11661-016-3501-z ↗
30. Notch fatigue and crack growth resistance of Ti-6Al-4V ELI additively manufactured via selective laser melting: A critical distance approach to defect sensitivity10.1016/j.ijfatigue.2018.12.020 ↗
31. C. Santus, D. Taylor, and M. Benedetti, “Determination of the fatigue critical distance according to the Line and the Point Methods with rounded V-notched specimen,” Int. J. Fatigue, vol. 106, no. October 2017, pp. 208–218, 2018, doi: 10.1016/j.ijfatigue.2017.10.002.10.1016/j.ijfatigue.2017.10.002 ↗
32. The critical distance method to estimate the fatigue strength of notched additively manufactured titanium alloys10.1016/j.prostr.2020.11.114 ↗
33. Application of the Theory of Critical Distances to predict the effect of induced and process inherent defects for SLM Ti-6Al-4V in high cycle fatigue
34. The Analysis of Small-Scale Notches on the Fatigue Performance of SLM Ti-6Al-4V; A Theory of Critical Distances Approach10.4028/p-h0iapl ↗
35. On the use of critical distance theories for the prediction of the high cycle fatigue limit stress in notched Ti-6Al-4V10.1016/j.ijfatigue.2004.06.002 ↗
36. Fatigue life prediction of small notched Ti-6Al-4V specimens using critical distance10.1016/j.engfracmech.2010.04.001 ↗
37. HCF strength estimation of notched Ti-6Al-4V specimens considering the critical distance size effect10.1016/j.ijfatigue.2011.12.019 ↗
38. Metal fatigue
39. High Cycle Fatigue and Fatigue Crack Growth Rate in Additive Manufactured Titanium Alloys
40. Assessment of the effect of isolated porosity defects on the fatigue performance of additive manufactured titanium alloy
41. Application of critical distances to fatigue at pores10.1111/ffe.13004 ↗
42. Comparison on mechanical anisotropies of selective laser melted Ti-6Al-4V alloy and 304 stainless steel10.1016/j.msea.2017.04.031 ↗
43. Strength or toughness? A criterion for crack onset at a notch10.1016/S0997-7538(01)01184-6 ↗
44. Boundary-value problem in the mechanics of the deformation and failure of damaged bodies with yielded zones10.1007/BF02369389 ↗
45. Modeling the deformation process of a plate with a stress concentrator taking into account the postcritical stage of material deformation10.15593/perm.mech/2020.3.04 ↗
46. The analytical and numerical solution of the problem of stretching a system of parallel elements with random strength characteristics taking into account the postcritical stage of deformation and rigidity of the loading system10.1007/s11012-022-01573-x ↗