The application relates to the technical field of
alloy materials, in particular to a high-strength
alloy material and a preparation process thereof. The application overcomes the problem that the mechanical properties and high-
temperature resistance of
alloy materials in the prior art cannot be considered simultaneously. The alloy component obtained by the application comprises Al-Li-Cu-Zr-Sc-Yb-In-Ag, and a hot-pressed alloy is obtained through high-temperature
zirconium melting-low-temperature
lithium pressing
smelting, hierarchical homogenization, deformation
heat processing, deep cooling and pre-strain
dislocation network induction technology; then a bimodal structure coexisting with equiaxed fine crystals and elongated
fiber crystals is constructed through gradient instantaneous annealing, and a dense
carbon atom layer is deposited on the surface by combining
chemical vapor deposition technology. The alloy material obtained by the application has good
fatigue resistance and
corrosion resistance, and is suitable for large thin-walled stressed components of
aerospace vehicles and high-temperature protection fields.