Abstract
Tribological properties of Al19Fe20-xCo20-xNi41Mo2x (x=0, 1, 2, 3, 4, 5) eutectic high-entropy alloys (EHEAs) were investigated in this research. Results show that EHEAs with trace Mo addition can form the face-centered cubic (fcc)+B2 eutectic microstructure, whereas EHEAs with relatively higher Mo content can form fcc+B2+μ dendritic microstructure. Mo element is beneficial to the strength enhancement of L12 phase and the ductility improvement of B2 phase. However, with increasing the Mo content to x>2, the resultant Mo-rich μ phase degrades the strength and plasticity of EHEAs. Al19Fe18Co18Ni41Mo4 EHEA has the optimal combination of high strength and high ductility. Increasing Mo content can improve the oxidation resistance of EHEAs. With increasing the Mo content, EHEA forms a tribo-oxide layer with improved oxidation resistance during sliding process, and the friction coefficient is monotonically decreased. This research provides guidance for the investigation of tribological properties of Al19Fe20-xCo20-xNi41Mo2x EHEAs.
Combining eutectic alloy with high-entropy alloys (HEAs), the eutectic high-entropy alloys (EHEAs
The eutectic microstructure of Al19Fe20Co20Ni41 EHEA consists of the ordered face-center cubic (fcc) phase (L12 phase) and ordered body-centered cubic (bcc) phase (B2 phase). It is found that the Mo addition is beneficial to the strength enhancement of L12 phas
Tribological performance is an important mechanical property for structural materials. It is reported that the forma-tion of eutectic lamellar microstructure is beneficial to increase the hardness, thereby improving the wear resis-tanc
The Al19Fe20-xCo20-xNi41Mo2x EHEAs with x=0, 1, 2, 3, 4, and 5 (at%) were denoted as Mo0, Mo2, Mo4, Mo6, Mo8, and Mo10 specimens, respectively. These EHEAs were synthesized by vacuum arc melting in furnace under high-purity argon protection. The purity of all raw materials was above 99.99%. The raw materials were put into the water-cooled copper hearth and remelted at least six times to ensure the chemical homogeneity. The mass of each alloy ingot is about 25 g and the central part of the ingot was selected for analysis. The specimens were cut by the electric discharge machine wire cutter into the ones with size of 5 mm×5 mm×5 mm. All specimens were ground by SiC sandpaper (2000#) and cleaned by ethanol through the ultrasonic cleaner.
The phase structure analysis was conducted through Rigaku SMARTLAB9 X-ray diffractometer (XRD, 40 kV, 150 mA). The morphology and composition were investigated by FEI Nova Nano 450 scanning electron microscope (SEM) coupled with energy dispersive spectrometer (EDS). Compression tests were conducted by AG-X Plus 250 kN/50 kN universal testing machine under deformation rate of 2 and 0.5 mm/min at room temperature. The reciprocating dry friction tests were conducted at room temperature (25 °C). The Si3N4 ceramic balls with 5 mm in diameter were used as the friction pair, the friction load was 5 N, the friction amplitude was 5 mm, the friction frequency was 2 Hz (linear velocity was 0.02 m/s), and the test duration was 30 min. Before tests, the alloy surface was polished. The wear morphology was observed by SEM.
Mo has a negative binary enthalpy of mixing and relatively low valence electron concentration (VEC), compared with other constitutional elements. Fig.1 shows the VEC values, mixing enthalpy ΔHmix, mixing entropy ΔSmix, and atomic size diffe-rence δ of the Al19Fe20-xCo20-xNi41Mo2x (x=0, 1, 2, 3, 4, 5) EHEAs. It can be seen that with increasing the Mo content, the mixing enthalpy ΔHmix, mixing entropy ΔSmix, and atomic size difference δ are increased, whereas VEC value is decreased. Hence, the microstructure and phase stability of Al19Fe20-xCo20-xNi41Mo2x EHEAs may be changed with the composition variation. With increasing the Mo content, the Al19Fe20-xCo20-xNi41Mo2x EHEAs have relatively large atomic size difference. Based on the solid-solution phase formation rules of HEAs, with increasing the Mo content, the ordered phase tends to precipitate in the solid solution, such as the intermetallic compounds in the matri


Fig.2 shows XRD patterns of Al19Fe20-xCo20-xNi41Mo2x EHEAs with x=0, 1, 2, 3, 4, 5. It can be seen that the as-prepared Mo0 EHEA is composed of B2+fcc dual-phase microstructur

Fig.3 SEM morphologies of different Al19Fe20-xCo20-xNi41Mo2x EHEAs: (a) x=0; (b) x=1; (c) x=2; (d) x=3; (e) x=4; (f) x=5
Specimen | Phase | Element | ||||
---|---|---|---|---|---|---|
Al | Fe | Co | Ni | Mo | ||
Mo0 | fcc | 13.72 | 24.96 | 20.68 | 40.64 | - |
B2 | 21.52 | 19.67 | 17.53 | 41.28 | - | |
Mo2 | fcc | 11.38 | 24.03 | 20.97 | 40.27 | 3.35 |
B2 | 25.61 | 16.54 | 15.42 | 42.07 | 0.36 | |
Mo4 | fcc | 10.14 | 23.94 | 20.83 | 40.79 | 4.29 |
B2 | 22.13 | 16.70 | 15.79 | 44.39 | 0.99 | |
Mo6 | fcc | 10.33 | 23.83 | 20.10 | 37.77 | 7.97 |
B2 | 21.90 | 16.32 | 14.58 | 44.80 | 2.40 | |
μ | 5.33 | 20.91 | 20.57 | 24.12 | 29.07 | |
Mo8 | fcc | 12.62 | 20.41 | 17.59 | 37.56 | 11.82 |
B2 | 24.18 | 14.15 | 12.60 | 45.16 | 3.91 | |
μ | 6.15 | 21.88 | 19.14 | 24.60 | 28.23 | |
Mo10 | fcc | 10.87 | 22.64 | 18.89 | 38.91 | 8.69 |
B2 | 23.79 | 15.48 | 13.50 | 45.53 | 1.70 | |
μ | 7.13 | 21.52 | 19.43 | 28.82 | 23.10 |
Fig.4 shows the compressive engineering stress-engineering strain curves of the Al19Fe20-xCo20-xNi41Mo2x EHEAs at room temperature. The mechanical compressive properties of Al19Fe20-xCo20-xNi41Mo2x EHEAs at room temperature are shown in
Specimen | Yield strength, σs/MPa | Ultimate compressive strength, σp/MPa | Elongation, ɛp/% |
---|---|---|---|
Mo0 | 751 | 2593 | 40.5 |
Mo2 | 770 | 2679 | 40.9 |
Mo4 | 703 | 2793 | 39.6 |
Mo6 | 931 | 2545 | 30.7 |
Mo8 | 1056 | 2486 | 26.1 |
Mo10 | 1291 | 2439 | 22.1 |

which are all higher than the tensile properties in Ref.[

Fig.5 Coefficients of friction of different Al19Fe20-xCo20-xNi41Mo2x EHEAs

Fig.6 Cross-sectional morphologies (a) and 3D confocal laser scanning images (b–g) of wear tracks of different Al19Fe20-xCo20-xNi41Mo2x EHEAs: (b) Mo0; (c) Mo2; (d) Mo4; (e) Mo6; (f) Mo8; (g) Mo10

Fig.7 SEM microstructures (a–c, g–i) and magnified images (d–f, j–l) of wear tracks of different Al19Fe20-xCo20-xNi41Mo2x EHEAs: (a, d) Mo0; (b, e) Mo2; (c, f) Mo4; (g, j) Mo6; (h, k) Mo8; (i, l) Mo10
1) The Mo addition can significantly improve the yield strength and wear resistance of Al19Fe20Co20Ni41 eutectic high-entropy alloys (EHEAs).
2) With x=0–2, the Al19Fe20-xCo20-xNi41Mo2x EHEAs show face-centered cubic (fcc)+B2 near-eutectic microstructures. With x=3–5, the Al19Fe20-xCo20-xNi41Mo2x EHEAs present fcc+B2+μ dendritic microstructures.
3) The strength and plasticity simultaneously increase with minor Mo addition, whereas the plasticity significantly decreases after the appearance of μ phase.
4) Al19Fe16Co16Ni41Mo8 EHEA has good mechanical properties with fine wear resistance, which is attributed to the optimal addition of Mo element.
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