| Literature DB >> 35454623 |
Xiqiang Ren1, Yungang Li1, Yanfei Qi1, Bo Wang2.
Abstract
Refractory high entropy alloys have broad application prospects due to their excellent comprehensive properties in high temperature environments, and they have been widely implemented in many complex working conditions. According to the latest research reports, the preparation technology of bulk and coating refractory high entropy alloys are summarized, and the advantages and disadvantages of each preparation technology are analyzed. In addition, the properties of refractory high entropy alloys, such as mechanical properties, wear resistance, corrosion resistance, oxidation resistance, and radiation resistance are reviewed. The existing scientific problems of refractory high entropy alloys, at present, are put forward, which provide reference for the development and application of refractory high entropy alloys in the future, especially for plasma-facing materials in nuclear fusion reactors.Entities:
Keywords: preparation technology; properties; radiation resistance; refractory high entropy alloys
Year: 2022 PMID: 35454623 PMCID: PMC9030642 DOI: 10.3390/ma15082931
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.748
Elemental characteristics and function of RHEAs components.
| Element Composition of RHEAs | Melting Point (°C) | Density at RT (g/cm3) | Main Performance | |
|---|---|---|---|---|
| Refractory metal elements | Mo | 2610 | 10.22 | Hardness [ |
| Nb | 2468 | 8.57 | Hardness [ | |
| Ta | 2996 | 16.65 | Strength [ | |
| V | 1902 | 6.11 | Strength [ | |
| W | 3410 | 19.35 | Hardness [ | |
| Ti | 1660 | 4.51 | Oxidation resistance [ | |
| Zr | 1852 | 6.51 | Oxidation resistance [ | |
| Hf | 2227 | 13.31 | Hardness, Yield strength [ | |
| Cr | 1857 | 7.19 | Oxidation resistance [ | |
| Re | 3180 | 21.04 | Plasticity, Creep resistance [ | |
| Non-refractory metal elements | Al | 660 | 2.7 | Oxidation resistance [ |
| Si | 1414 | 2.33 | Oxidation resistance [ | |
| Co | 1495 | 8.9 | Yield strength [ | |
| Ni | 1453 | 8.9 | corrosion resistance [ | |
Note: RT-room temperature.
Figure 1TEM images of bulk NbMoTaWVCr0.6 RHEAs sintered at different temperatures: (a) 1400 °C, (b) 1500 °C, (c) 1600 °C, (d) SAED pattern of grain A in (b), corresponding to a BCC structure, (e) SAED pattern of grain B in (b), corresponding to a C15 Laves phase (cubic), (f) SAED pattern of grain C in (b), corresponding to Ta2VO6 (tetragonal phase), (g) SAED pattern of grain D in (c), corresponding to a C14 Laves phase (hexagonal) [54]. (Reprinted with permission from Ref. [54]. Copyright 2018 Elsevier).
The chemical compositions (in at.%) and constituent phases (%) of bulk NbMoTaWVCr0.6 RHEAs sintered at 1500 °C and 1600 °C [54]. (Reprinted with permission from Ref. [54]. Copyright 2018 Elsevier).
| Nominal Composition | 1500 °C | 1600 °C | |||||
|---|---|---|---|---|---|---|---|
| BCC PHASE | t-(Ta,V)O2 | C15 Laves | BCC Phase | t-(Ta,V)O2 | C14 Laves | ||
| Nb | 16.67 | 16.04 | 2.45 | 17.83 | 16.37 | 2.16 | 16.65 |
| Mo | 16.67 | 17.28 | - | 3.59 | 16.70 | - | 3.01 |
| Ta | 16.67 | 15.38 | 24 | 18.92 | 16.18 | 22.43 | 22.31 |
| W | 16.67 | 17.91 | - | 7.47 | 17.68 | - | - |
| V | 16.67 | 16.17 | 12.96 | 11.58 | 16.02 | 13.41 | 13.17 |
| Cr | 16.67 | 17.21 | - | 40.58 | 17.04 | - | 44.82 |
| O | - | - | 60.57 | - | - | 61.97 | - |
Figure 2Schematic diagram of laser cladding.
Figure 3Schematic diagram of magnetron sputtering.
Figure 4Characterization of WTaTiCrV RHEAs films on Si substrate with SEM-surface morphology and EDS elemental mapping of surface.
Room-temperature yield strength (σ0.2), peak strength (σp), and plastic strain (εp) of the as-cast TixNbMoTaW RHEAs [69]. (Reprinted with permission from Ref. [69]. Copyright 2017 Elsevier).
| RHEAs | σ0.2 (MPa) | σp (MPa) | εp (%) | |
|---|---|---|---|---|
| TixNbMoTaW | Ti0 | 996 | 1148 | 1.9 |
| Ti0.25 | 1109 | 1197 | 2.5 | |
| Ti0.5 | 1211 | 1578 | 5.9 | |
| Ti0.75 | 1304 | 1593 | 8.4 | |
| Ti1 | 1455 | 1910 | 11.5 | |
Note: the molar ratio x = 0, 0.25, 0.5, 0.75 and 1.
Figure 5The SEM images of fracture surfaces of NbMoTaW RHEAs and TixNbMoTaW RHEAs [69]: (a) intergranular fracture; (b) transgranular fracture. (Reprinted with permission from Ref. [69]. Copyright 2017 Elsevier).
Electrochemical properties of materials, in phosphate buffer solution, at 37 °C [81]. (Reprinted with permission from Ref. [81]. Copyright 2016 Elsevier).
| Materials | TiZrNbTaMo | Ti6Al4V | 316 L SS | CoCrMo |
|---|---|---|---|---|
| −607 ± 55 | −571 ± 11 | −234 ± 13 | −320 ± 30 | |
| 0.89 ± 0.06 | 0.96 ± 0.21 | 0.83 ± 0.03 | 0.42 ± 0.19 | |
| - | - | 675 ± 30 | 435 ± 23 |
Note: Ecorr = corrosion potential, Ip = passive current density, Epit = pitting potential.
Figure 6Potentiodynamic polarization curves of materials in phosphate buffer solution at 37 °C [81]. (Reprinted with permission from Ref. [81]. Copyright 2016 Elsevier).
Figure 7Energy-dispersive X-ray mapping for the microstructures of the oxides, developed at 1200 °C for 24 h [82]. (Reprinted with permission from Ref. [82]. Copyright 2020 Elsevier).
Figure 8BSE images of NbMoCrAl after 3 h (a) and 24 h (b) of exposure to air at 1000 °C. A higher magnification BSE image of the metal/oxide interface of (b) is displayed in (c) [85]. (Reprinted with permission from Ref. [85]. Copyright 2019 Elsevier).
Figure 9Hardness versus depth for irradiated and un-irradiated samples of (a) HfTaTiVZr high entropy alloy and (b) 304 stainless steel (SS304) [86]. (Reprinted with permission from Ref. [86]. Copyright 2019 Elsevier).