Effects of Process Parameters and Process Defects on the Flexural Fatigue Life of Ti-6Al-4V Fabricated by Laser Powder Bed Fusion

The fatigue performance of laser powder bed fusion-fabricated Ti-6Al-4V alloy was investigated using four-point bending testing. Specifically, the effects of keyhole and lack-of-fusion porosities along with various surface roughness parameters, were evaluated in the context of pore circularity and size using 2D optical metallography. Surface roughness of S<sub>a</sub> = 15 to 7 microns was examined by SEM, and the corresponding fatigue performance was found to vary by 10<sup>2</sup> cycles to failure. The S-N curves for the various defects were also correlated with process window examination in laser beam power-velocity (P-V) space. Basquin's stress-life relation was well fitted to the experimental S-N curves for various process parameters except keyhole porosity, indicating reduced importance for LPBF-fabricated Ti-6Al-4V alloy components.

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Publication Details

Journal
Materials
Published
2024-09-16
DOI
https://doi.org/10.3390/ma17184548
Citations
5
Primary Topic
Additive Manufacturing Materials and Processes
Type
article
Field-Weighted Citation Impact
1.06

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article

Effects of Process Parameters and Process Defects on the Flexural Fatigue Life of Ti-6Al-4V Fabricated by Laser Powder Bed Fusion

L.E. Murr, Shadman Tahsin Nabil, Alex De La Cruz, Edel Arrieta et al.
5 citations
Materials
Additive Manufacturing Materials and Processes
1.06
article

Effects of Process Parameters and Process Defects on the Flexural Fatigue Life of Ti-6Al-4V Fabricated by Laser Powder Bed Fusion

L.E. Murr, Shadman Tahsin Nabil, Alex De La Cruz, Edel Arrieta, Cristian Banuelos, Ryan B. Wicker, Brandon Ramirez, Francisco R. Medina
article en
5 citations

Abstract

The fatigue performance of laser powder bed fusion-fabricated Ti-6Al-4V alloy was investigated using four-point bending testing. Specifically, the effects of keyhole and lack-of-fusion porosities along with various surface roughness parameters, were evaluated in the context of pore circularity and size using 2D optical metallography. Surface roughness of S<sub>a</sub> = 15 to 7 microns was examined by SEM, and the corresponding fatigue performance was found to vary by 10<sup>2</sup> cycles to failure. The S-N curves for the various defects were also correlated with process window examination in laser beam power-velocity (P-V) space. Basquin's stress-life relation was well fitted to the experimental S-N curves for various process parameters except keyhole porosity, indicating reduced importance for LPBF-fabricated Ti-6Al-4V alloy components.

MaterialsVol. 17(18)
The University of Texas at El Paso (US)
National Aeronautics and Space Administration
Openalex Percentile: Top 26%
Additive Manufacturing Materials and Processes
1.06
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Effects of Process Parameters and Process Defects on the Flexural Fatigue Life of Ti-6Al-4V Fabricated by Laser Powder Bed Fusion — L.E. Murr, Shadman Tahsin Nabil, et al. · Materials (2024) | TGRS Research Map | TGRS