1. Introduction
Fig. 1. Schematic of the duration of irradiation studies in MAX/MAB phase materials based on incomplete results. |
2. Irradiation resistance and mechanisms of MAX/MAB phases
2.1. Irradiation resistance and mechanisms of Ti-based MAX phases
2.1.1. Temperature effect
Fig. 3. Structural evolution of Ti2AlC after irradiation and annealing: (a-b) Raman spectra of Ti2AlC irradiated and annealed at different temperatures, with irradiation fluxes of 1×1015 ions ⋅cm-2,1.5×1016 ions ⋅cm-2 in that order; (c-d) Ti2AlC and Ti3SiC2 irradiated at different temperatures and annealed by GIXRD. Reproduced with permission from Ref. [65]. Copyright 2017 Elsevier. |
2.1.2. Influencing factors
Fig. 4. Structural transformation of Ti2AlN and Ti4AlN3 with increasing irradiation fluence: (a-d) SADP plots of Ti2AlN irradiated with 70 keV He ions; (e-h) SADP plots of Ti4AlN3 irradiated with 70 keV He ions. Reproduced with permission from Ref. [72]. Copyright 2019 Elsevier. |
2.1.3. Antisite defect
2.1.4. Phase transition
Fig. 5. α to β phase transition: (a-b) Rietveld refinement of XRD of Xe ion irradiated samples, a for α-Ti3SiC2, b with both α and β-Ti3SiC2; (c) Schematic structure of α and β-Ti3SiC2. Reproduced with permission from Ref. [75]. Copyright 2010 Elsevier. |
2.2. Irradiation resistance and mechanisms of Cr/Zr/Nb/V/Ta-based MAX phases
Table 1 Calculated point defect formation energies for MAX phase in eV. [84]. Copyright 2017 Elsevier. Reproduced with permission from Ref. |
| Reaction | V3AlC2 | Zr3AlC2 | Ta3AlC2 | Ti3AlC2 |
|---|---|---|---|---|
| MM→VM+Mi | 7.40 | 6.12 | 7.43 | 7.32 |
| AlAl→VAI+Ali | 6.31 | 1.46 | 5.84 | 3.40 |
| CC→VC+Ci | 2.73 | 3.47 | 2.87 | 3.17 |
| MM+AlAl→MAl+AlM | 2.71 | 3.46 | 3.85 | 3.27 |
| MM+CC→MC+CM | 9.80 | 10.60 | 17.36 | 10.52 |
| AlA1+CC→AlC+CAl | 9.36 | 8.43 | 10.67 | 9.26 |
| Ali+VM→AlM | -5.38 | -2.39 | -4.44 | -4.20 |
| Ci+VM→CM | -1.15 | 0.14 | 1.35 | -0.48 |
| Mi+VAl→MAl | -5.62 | -1.72 | -4.97 | -3.25 |
| Ci+VAl→CAl | 0.21 | 0.46 | 0.58 | 0.31 |
| Mi+VC→MC | -0.63 | 0.86 | 5.72 | 0.51 |
| Ali+VC→AlC | 0.12 | 3.04 | 1.39 | 2.39 |
| Mi+AlAl→MAl+Ali | 0.68 | -0.27 | 0.87 | 0.15 |
| Mi+CC→MC+Ci | 2.10 | 4.33 | 8.58 | 3.68 |
| Al1+MM→AlM+Mi | 2.03 | 3.73 | 2.99 | 3.12 |
| Ali+CC→AlC+Ci | 2.85 | 6.51 | 4.25 | 5.55 |
| Ci+MM→CM+Mi | 7.70 | 6.26 | 8.78 | 6.84 |
| 18) Ci+AlAl→CAl+Ali | 6.51 | 1.92 | 6.42 | 3.71 |
Fig. 6. Deposition of C on the near-surface of Cr2AlC during irradiation: (a) Raman spectra of Cr2AlC irradiated with 100 keV He ions at different fluences; (b) RBS spectra of Cr2AlC irradiated with He ions at different fluences. Reproduced with permission from Ref. [93]. Copyright 2019 Elsevier. |
Fig. 7. (a-f) Backscattered SEM images of Zr2AlC under different ion irradiation conditions; (g) Schematic representation of the types of defects produced by irradiated Zr2AlC; (h-i) Migration paths and potential barriers of He atoms in Zr3Al3C5. Reproduced with permission from Ref. [101,102]. Copyright 2019, 2021 Elsevier, respectively. |
2.3. Irradiation resistance and mechanisms of doped/entropy-enhanced MAX phases
2.3.1. Doped multi-component MAX phase
Fig. 8. Structural changes and He ion irradiation behavior of Zr -doped Ti3SiC2 : (a) charge density distribution, in order of Ti3SiC2, Zr-Ti1, and Zr-Ti2; (b) sites occupied by He in the MAX phase; (c) solvation energies of He in the interstitial sites; and (d) charge density distributions of doped He, in order of Ti3SiC2-He,Zr-Ti1- He, Zr-Ti2-He. Reproduced with permission from Ref. [116]. Copyright 2022 Elsevier. |
2.3.2. Entropy increasing multi-component MAX phase
Fig. 9. (a-b) Schematic representation of (TiVNbZrHf) 2SnC supercell structure and atomic arrangement. Reproduced with permission from Ref. [120]. Copyright 2022 Elsevier. |
Fig. 10. In situ SAED maps of (a-h) Ti2SnC and (i-p) (TiVNbZrHf2SnC under 800keVKr2+ irradiation. Reproduced with permission from Ref. [120]. Copyright 2022 Elsevier. |
2.4. Irradiation resistance and mechanisms of MAB phase
Fig. 11. Atomic structure of (a) CrB, (b) Cr3 B4, (c) Cr2 B3, (d) Cr2AlB2, (e) Cr3AlB4, and (f) Cr4AlB6; (g-j) Cr-based MAB phases with one and two Al layers, and the configurations of their Cr interstitials before and after relaxation. Reproduced with permission from Ref. [132,133]. Copyright 2022 Elsevier and 2022 American Chemical Society, respectively. |
Fig. 12. (a-l) TEM and HRTEM images of MoAlB and Fe2AlB2 irradiated at 150∘C,7.5×1016 ions cm-2 (left column), 150 ∘C,1.5×1017 ions cm-2(middle column) and 150∘C,7.5×1017 ions cm-2 (right column); (m) Schematic structures of MoAlB and Fe2AlB2. Reproduced with permission from Ref. [139]. Copyright 2020 Elsevier. |
Table 2 Comparison of main advantages and disadvantages of irradiation resistance between MAX phases and MAB phases studied so far. |
| Phase type | Subclass | Main Advantages | Main Disadvantages |
|---|---|---|---|
| MAX | Ti-based MAX phases | Easy defect recovery at high temperatures; strong resistance to amorphization and hardening; high n values enhance phase stability. | C-axis expansion; antisite defects hard to annihilate; He in A-layer causes embrittlement; phase transition. |
| Cr-based MAX phases | Strong corrosion/oxidation resistance; self-healing ability. | Prone to irradiation hardening; softening at low doses; amorphization at high doses. | |
| Zr/Nb/V/Ta-based MAX phases | Zr: good neutron transparency. V: phase transformation against amorphization. | Zr: easy amorphization at room temperature; cracking; high-temperature phase decomposition. Others: scarce research; difficult preparation. | |
| doped/entropy-enhanced MAX phases | High amorphization threshold; difficult defect aggregation; strong defect accommodation capacity; swelling resistance. | Possible phase decomposition at high doses; performance highly dependent on entropy and element selection. | |
| MAB | single B-chain with double Al layer (111-type MAB phases) single B-chain with single Al layer (212-type MAB phases) single B-ring (Cr3AlB4) | Strong neutron absorption of MoAlB and WAlB; Resistance to D erosion; Inhibition of He bubble growth. Stronger resistance to amorphization than 111-type; high defect recovery rate. Best defect recovery and anti-amorphization capabilities among MAB phases. | Difficult defect recovery; thermal shock cracking; poor stability. High He bubble density; prone to embrittlement. |
| double B-ring (Cr4AlB6 ) | Medium amorphization threshold; B-ring restrains interlayer peeling; high γ-ray attenuation rate. | Harder defect recombination than single B-rings; high Frenkel defect concentration. |
3. Neutron irradiation damage of MAX/MAB phase
Fig. 13. (a) Weibull modulus and strength distribution of pre-irradiated Ti3SiC2 material; (b) average strength of pre-irradiated and irradiated specimens at selected temperatures; (c) variation of the lattice parameter of the samples at different temperatures and damage doses. Reproduced with permission from Ref. [148]. Copyright 2017 Elsevier. |
4. Ion Irradiation damage of MAX/MAB phase
4.1. Heavy ion radiation damage
4.1.1. Conventional heavy ion
4.1.2. Self-Ion
4.2. He ion radiation damage
Fig. 14. Variation of (a) size and (b) density of Ti2AlC irradiated defects as a function of irradiation dose and temperature during 1 MeV Kr ion irradiation. Reproduced with permission from Ref. [158]. Copyright 2018 Elsevier. |
4.2.1. Sites of action and limitations
Fig. 15. Phase transformation pattern of Ti3AlC2 irradiated by C ions: (a) Schematic diagram of the phase transition structure and path; (b) microstrain and phase ratio of samples irradiated with different fluences at RT; (c-d) microstrain and phase ratio of samples irradiated with different temperatures at fluences of 1×1016 ions cm-2 and 1×1017 ions cm-2, respectively. Reproduced with permission from Ref. [79]. Copyright 2020 Elsevier. |
Fig. 16. (a) Interlayer migration paths of He atoms diffusing along the c-axis: |
4.2.2. Performance loss and recovery
Table 3 He-irradiation-induced damage. |
| Year | Composition | Conditions | Damage | Ref. |
|---|---|---|---|---|
| 2014 | Ti3AlC2 | 500keV;300∘C,500∘C or RT | He bubbles, dislocations, and microstrains | [179] |
| 2017 | Ti3AlC2 | 400keV;500∘C or RT | oriented cracks, surface exfoliation | [174] |
| 2017 | Zr/V2AlC | 500keV;RT;450∘C annealed | reduced the adhesion of the coating | [175] |
| 2018 | Ti3SiC2 | 110 keV ; RT, or 450∘C | crystal damage, phase decomposition, phase transition | [177] |
| 2018 | Ti3SiC2 | 110keV;RT;430∘C,750∘C, or 1050∘C annealed | phase decomposition and recovery, He bubbles | [172] |
| 2019 | Ti2AlC | 100keV;RT-750∘C | lattice distortion, He bubbles, microcracks | [176] |
| 2020 | Cr2AlC | 100keV;RT;700∘C or 600∘C annealed | irradiation hardening | [178] |
| 2021 | Ti2AlC | 110keV;RT;450∘C,600∘C or 700∘C annealed | laminations, dislocations, non-nanocrystalline phases, reversible phase transition, C enrichment | [171] |
| 2021 | Ti3SiC2 | 110 keV ; RT or 750∘C | highly disordered (RT), stable lattice (750∘C ), elongated He bubbles | [173] |
| 2023 | Ti3SiC2 | 110keV;RT;1100∘C annealed | large-sized He bubbles, phase transition, Si layer damage | [83] |
4.3. H ion radiation damage
4.3.1. H diffusion
4.3.2. H/He synergies
5. Electron irradiation damage of MAX/MAB phase
Fig. 17. Migration energy barriers for H atoms: (a) intact Cr2AlC; (b) Cr2AlC containing Al vacancies. Reproduced with permission from Ref. [91]. Copyright 2023 Elsevier. |
6. Conclusions and perspective
6.1. Entropy regulation
Fig. 18. Structural evolution by electron irradiation: (a-h) SAED maps taken with the electron beam parallel to [0 001] for Ti3AlC2 after irradiation times of 0 s, $150\text{ }\mathrm{s},300\text{ }\mathrm{s},600\text{ }\mathrm{s},1010\text{ }\mathrm{s},1370\text{ }\mathrm{s},1730\text{ }\mathrm{s}$, and 2090 s, in that order; (i-k) Schematic diagrams of defect generation and atomic rearrangement. Reproduced with permission from Ref. [188]. Copyright 2020 Elsevier. |
