The influence of annealing treatment on the mechanical properties and interfacial characteristics of a TA1/Al5083 bimetal composite was investigated in this research. The bimetal composite plates were prepared by explosive welding and annealing at temperatures ranging from 400 to 550 °C at intervals of 50 °C for 3 h. Uniaxial tensile and shear tests were employed to study the influence of the annealing treatments. Uniaxial tensile tests indicate that the tensile strength and elongation display a tendency to first improve and then decrease with increasing annealing temperature. No obvious necking phenomenon is observed in the composite sheet annealed at 400 and 450 °C, and extremely short cracks appear in the interfacial transition zone, while localized necking and delamination phenomena are found to occur in the composite sheet annealed at 500 and 550 °C. The ultimate tensile strength and elongation of specimens annealed at 450 and 500 °C is improved, while specimens annealed at 5
In the present study, the laser melting deposition (LMD) technology was adopted to fabricate FeCoCrNiMn and FeCoCrNiMnAl0.75 high entropy alloys (HEAs). Then, laser welding method was used to join the HEAs in forms of similar (FeCoCrNiMnAl/FeCoCrNiMnAl and FeCoCrNiMnAl0.75/FeCoCrNiMnAl0.75) and dissimilar (FeCoCrNiMnAl0/FeCoCrNiMnAl0.75) combinations, respectively. Ultra-depth field microscope and electron backscatter diffraction detection were used to observe the macro-morphology and microstructure, respectively. It was found that the width of the weld bead and heat-affected zone with higher aluminium content was larger. In both base metals and welded joints, aluminium promoted the face-centered cubic (FCC) phase transfer into body-centered cubic (BCC), significantly refined the grain and the dislocation density of HEA is also increased, which increased strength and hardness, and decreased ductility. Highlights The FeCoCrNiMn/FeCoCrNiMn, FeCoCrNiMn/FeCoCrNiMnAl0.75, FeCoCrNiMnAl0.75/F