| Literature DB >> 30839937 |
Vladimir V Popov1, Alexander Katz-Demyanetz1, Andrey Koptyug2, Menachem Bamberger3.
Abstract
High Entropy Alloys (HEAs) is a novel promising class of multi-component materials which may demonstrate superior mechanical properties useful for high-temperature applications. Despite the high potential of HEAs, their production is complicated, using pre-alloyed powders in powder metallurgy route. This significantly complicates development and implementation of refractory BCC solid solution based HEAs. The present paper reports on experiments aiming at production of Al0.5CrMoNbTa0.5 multi-principle alloy using powder bed beam based additive manufacturing. Samples were manufactured using Selective Electron Beam Melting (SEBM) additive manufacturing technique from a blend of elemental powders aiming at achieving microstructure with high configurational entropy. Though it was not possible to achieve completely homogeneous microstructure, the as-printed material was composed of the zones with two multi-component solid solutions, which differed only by Al content confirming in situ alloying. The process parameters optimization was not carried out and the as-print material contained a notable amount of residual porosity. It was possible to reach lower porosity level using heat treatment at 1300 °C for 24 hours, however undesirable alloy composition changes took place. The main conclusion is that the production of the Al0.5CrMoNbTa0.5 multi-principle alloy from elemental powder blends using SEBM technique is achievable, but the process parameter optimization rather than post-process heat treatment should be performed to reduce the porosity of samples.Entities:
Keywords: Materials science; Metallurgical engineering
Year: 2019 PMID: 30839937 PMCID: PMC6366149 DOI: 10.1016/j.heliyon.2019.e01188
Source DB: PubMed Journal: Heliyon ISSN: 2405-8440
Fig. 1Secondary Electron images of elemental powders and final blended Al0.5CrMoNbTa0.5 powder. a – Aluminum powder; b – Chromium powder; c – Molybdenum powder; d – Niobium powder; e – Ta – Tantalum powder; f – powders blend.
Characteristics of powders.
| Powder | Purity, % | Fraction, μm | Supplier |
|---|---|---|---|
| Aluminum | 99.0 | 200 mesh/74 μm | ACROS Organics |
| Chromium | 99.0 | −100 mesh/149 μm | Strem Chemicals, Inc. |
| Niobium | 99.8 | −325 mesh/44 μm | Strem Chemicals, Inc. |
| Tantalum | 99.8 | −325 mesh/44 μm | Strem Chemicals, Inc. |
| Molybdenum | 99.9 | 3–7 | Strem Chemicals, Inc. |
Calculation of Al0.5Cr1.0Mo1.0Nb1.0Ta0.5 powder blend per total volume 300 ml.
| Element | Molar % | Molar weight, g/mole | Density, g/cm3 | Volume % | Volume per overall volume 300 cm3, cm3 | Weight per overall volume 300 cm3, g |
|---|---|---|---|---|---|---|
| Al | 12 | 26,98 | 2,69 | 12.66 | 38.0 | 102 |
| Cr | 25 | 52,00 | 7,19 | 19,09 | 57.3 | 412 |
| Mo | 25 | 95,94 | 10,22 | 24,79 | 74,4 | 760 |
| Nb | 25 | 92,91 | 8,57 | 28,59 | 85,7 | 734 |
| Ta | 13 | 180,95 | 16,65 | 14,87 | 44.6 | 743 |
Fig. 2Production chain: a – powder semi-sintering in each layer; b – melting of the samples in each layer; c – manufactured bulk samples sounded by the semi-sintered powder; d – bulk samples removed from the base plate.
Fig. 3Powder loss during SEBM process: a – “fireworks” – powder removed from the powder bed by high power electron beam; b – metalized surface of the powder hopper and rake after SEBM process; c – SEM-image of the powder lost by “fireworks”; d–e – SEM-images of the metallization flakes in different magnifications.
Fig. 4Typical microstructures of the as-manufactured (a, b) and heat-treated samples at 1000 °C (c, d); and at 1300 °C (e, f).
Chemical composition of different phases of the as-manufactured samples in comparison to the initial powder.
| Sample | Phase description | Element content, at. % | ||||
|---|---|---|---|---|---|---|
| Al | Cr | Mo | Nb | Ta | ||
| Initial powder | Overall | 12.0 | 25.0 | 25.0 | 25.0 | 13.0 |
| As-built | Overall | 8.4 | 25.8 | 25.7 | 26.5 | 13.6 |
| TaMoNbCr s.s. | 1.4 | 9.4 | 39.1 | 29.9 | 20.2 | |
| (TaMoNbCr)Al s.s. | 11.8 | 27.6 | 24.8 | 24.3 | 11.5 | |
| HT 1000 °C | Overall | 8.0 | 24.7 | 26.3 | 26.4 | 14.6 |
| TaMoNbCr s.s. | 1.3 | 9.3 | 38.7 | 29.7 | 21.0 | |
| (TaMoNbCr)Al s.s. | 11.7 | 27.4 | 24.3 | 24.2 | 12.4 | |
| HT 1300 °C | Overall | 7.8 | 23.2 | 26.7 | 27.3 | 15.0 |
| TaMoNbCr s.s. | 1.3 | 9.9 | 37.5 | 30.9 | 20.4 | |
| (TaMoNbCr)Al s.s. | 11.8 | 28.5 | 23.4 | 23.8 | 12.5 | |
Fig. 5XRD spectra of the as-manufactured and post-heat-treated samples. a – as-manufactured sample; b – sample heat treated at 1000 °C; c – sample heat treated at 1300 °C.
Evaporation temperatures of the elements composing the examined powders blend under different pressures [39].
| Element | Evaporation temperatures at different pressures, °C | ||
|---|---|---|---|
| At 10−2 mbar | At 10−3 mbar | At 10−4 mbar | |
| Al | 1209 | 1087 | 982 |
| Cr | 1383 | 1254 | 1144 |
| Mo | 2466 | 2258 | 2080 |
| Nb | 2669 | 2439 | 2256 |
| Ta | 3025 | 2776 | 2567 |