Abstract
Laser powder bed fusion (LPBF) has demonstrated its unique ability to produce customized, complex engineering components. However, processing of many commercial Al-alloys by LPBF remains challenging due to the formation of solidification cracking, although they are labelled castable or weldable. In order to elucidate this divergence, solidification cracking susceptibility from the steepness of the solidification curves, specifically |dT/dfS1/2|, as the fraction solidified nears 1 towards complete solidification, was calculated via Scheil–Gulliver model as a function of solute concentration in simple binary Al-Si, Al-Mg, and Al-Cu systems. Introduction of “diffusion in solid” into Scheil–Gulliver model resulted in a drastic reduction in the cracking susceptibility (i.e., reduction in the magnitude of |dT/dfS1/2|) and a shift in the maximum |dT/dfS1/2| to higher concentrations of solute. Overall, the calculated solidification cracking susceptibility correlated well with experimental observation made using LPBF AA5083 (e.g., Al-Mg) and Al-Si binary alloys with varying Si concentration. Cracking susceptibility was found to be highly sensitive to the composition of the alloy, which governs the variation of |dT/dfS1/2|. Furthermore, experimental observation suggests that the contribution of “diffusion in solids” to reduce the cracking susceptibility can be more significant than what is expected from an instinctive assumption of negligible diffusion and rapid cooling typically associated with LPBF.
Original language | English |
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Pages (from-to) | 5-13 |
Number of pages | 9 |
Journal | Journal of Phase Equilibria and Diffusion |
Volume | 42 |
Issue number | 1 |
DOIs | |
State | Published - Feb 2021 |
Externally published | Yes |
Funding
This research was sponsored, in part by the Office of Naval Research (No. N00014-17-1-2559) and in part by the CDCC Army Research Laboratory (No. W911NF1720172). The views, opinions, and conclusions made in this document are those of the authors and should not be interpreted as representing the official policies, either expressed or implied, of the Office of Naval Research or the US Army Research Laboratory or the US Government. The US Government is authorized to reproduce and distribute reprints for Government purposes notwithstanding any copyright notation herein. This research was sponsored, in part by the Office of Naval Research (No. N00014-17-1-2559) and in part by the CDCC Army Research Laboratory (No. W911NF1720172). The views, opinions, and conclusions made in this document are those of the authors and should not be interpreted as representing the official policies, either expressed or implied, of the Office of Naval Research or the US Army Research Laboratory or the US Government. The US Government is authorized to reproduce and distribute reprints for Government purposes notwithstanding any copyright notation herein.
Keywords
- additive manufacturing
- aluminum alloy
- cracking susceptibility
- diffusion
- laser powder bed fusion