The modified homogenization process has garnered increasing interest in the high-alloyed materials preparation owing to its effectiveness in mitigating segregation and enhancing properties. In this work, the effects of homogenization treatment on the intermetallic phases, solidification structure and mechanical properties of a novel Al-Zn-Mg-Cu-Y alloy are investigated. The results indicate that the Al8Cu4Y phase is formed in the matrix and maintains steady during homogenization. It is confirmed that lower homogenization temperature (400 °C) can promote Al3Zr nucleation, while higher temperature (460 °C) can accelerate the dissolution of MgZn2 phase owing to a higher diffusion coefficient. Compared with single homogenization treatment, a two-stage homogenization (400 °C/16 h + 460 °C/24 h) can achieve a combination result of massive MgZn2 phases dissolution and fine Al3Zr dispersoids precipitation in the alloy. Moreover, the mean grain size ranges from 166.1 to 154.5 μm and its misorientation angle ranges from 39.9 to 40.9° during homogenization, suggesting a certain thermal stability for Al-Zn-Mg-Cu-Y alloy. In addition, Vickers hardness and electrical conductivity show a linear relation with the Zn, Mg and Cu elemental content in the matrix. The alloy demonstrates an improved tensile strength after homogenization, which is mainly related to MgZn2 dissolution and Al3Zr precipitation.
The work developed a series of novel Co-free high-entropy alloys (HEAs), i.e. Fe3.75Cr1.25NiAl0.6-xTix (x = 0, 0.15, 0.30 and 0.40, molar ratio) HEAs abbreviated as Ti0, Ti0.15, Ti0.30 and Ti0.40, respectively. The effects of Ti/Al ratio (Al partially replaced by Ti) on the microstructure and tensile properties were investigated systematically. The Ti0 HEA contains the FCC phase in dendritic regions and the BCC and B2 phases (BCC/B2) in interdendritic regions. Moreover, the spherical ordered B2 nanoparticles are embedded in the BCC matrix. With increasing the Ti/Al ratio from 0 to 1/3, there is a phase transition from B2-NiAl to L21-Ni2AlTi. Furthermore, the morphology of the nanoparticles evolves from spherical to cuboidal. With further increasing the Ti/Al ratio from 1/3 to 1 and 2, the morphology of nanoparticles evolves from cuboidal back to spherical. In addition, the Ti0.40 HEA has σ phases besides FCC, BCC, and L21 phases. The analysis of tensile properties shows that properly adjusting Ti/Al ratios sharply improves the plasticity and slightly improves the ultimate strength, but only causes a limited decrease in the yield strength. Specifically, the Ti0.15 HEA has a superior combination of strength and plasticity, exhibiting a yield strength of 819 MPa, an ultimate strength of 1113 MPa, and a fracture strain of 13.4 %. The SRO, the solid-solution strengthening, the phase transformation, and the shape of nanoparticles were discussed in detail, which reveals the origins of the excellent tensile properties. In addition, the excessive addition of Ti forms the σ phase, leading to a serious brittleness.
These findings are believed to promote the development of low-cost HEAs with BCC/L21 for practical applications.
VNbTa refractory medium-entropy alloy (RMEA) with extraordinary strength-ductility synergy and rolling formability was deemed as an ideal structural material suitable for industrial applications, whereas the tribological performance has been still unclear. Therefore, this work employed a ball-on-disc tribometer to evaluate friction and wear properties of VNbTa alloy at various temperatures. It was surprisingly found that, at 800 °C, the alloy exhibits exceptional tribological performance with the coefficient of friction (COF) of 0.13 and wear rate of 3.9 × 10−6 mm3/Nm. Our results indicated that the mild friction and wear at 800 °C are mainly attributed to the durable lubrication of in-situ molten V2O5 as well as good load-bearing capacity of hard oxide scale.
The susceptibility of titanium aluminides (TiAl) to environmental embrittlement is one of the factors limiting the use of this class of intermetallic alloys. After being exposed to air at high temperatures, the ductility of the material at room temperature is significantly reduced or even completely lost. In the present work the influence of near surface grain refinement on the example of the β-stabilised TNM alloy on the embrittlement behaviour after exposure for 2 h at 700 °C in air is presented and discussed. The main characteristic of the environmental embrittlement is that cracks during tensile tests at room temperature appear on the surface and lead to rapid failure. One of the reasons given in literature for this behaviour is that high tensile stresses form at the sample edge by exposure. Grain refinement of the surface region with a depth of approximately 350 μm displaces crack initiation during tensile testing well below the surface after exposure. The environmental embrittlement phenomenon after short-term exposure does, thus, not occur in this layer-like structure. Various reasons for this behaviour, which include delayed crack formation, stress relaxation during loading and cooling after loading as well as supporting effects, but also the limitations of the treatment method, are discussed in the work.
In this study, Cr3C2/Ni3Al composites containing Cr3C2 particles of different sizes were prepared via hot-press sintering. Subsequently, the effects of the size of the added Cr3C2 particles on the microstructure, hardness, and tribological properties of the Cr3C2/Ni3Al composites were investigated. The results showed that the Ni3Al powder and Cr3C2 particles in the composites exhibited obvious interdiffusion interactions during the hot-press sintering process and formed a new diffusion phase with an M7C3 (M = Cr, Fe, and Ni) structure in the Cr3C2/Ni3Al composites. In addition, the diffusion effect in the composites with small Cr3C2 particles was full, the proportion of the M7C3 (M = Cr, Fe, and Ni) diffusion phase in the composites was greater, and the solid-solution strengthening effect of the matrix phase was evident. The hardness of the Cr3C2/Ni3Al composites was noticeably higher than that of the Ni3Al alloy because of the combination of particle, solid-solution, and refined crystalline strengthening effects. The composite with 5 μm Cr3C2 particles displayed the maximum hardness (56.3 HRC) and best wear resistance. The wear mechanism results indicated that the carbide particles in the composites improved the hardness, carried the load, and blocked the movement of abrasive particles, effectively protecting the matrix from wear. However, when the added Cr3C2 particles were too large, the weak interfacial bond between the chromium carbides and the matrix phases in the composites allowed the chromium carbides to easily crack and fall off, which decreased the wear resistance.