High-Temperature Deformation Behavior of Ti-6Al-2Sn-4Zr-2Mo Alloy with Lamellar Microstructure Under Plane-Strain Compression

High-temperature plane-strain compression of a Ti-6Al-2Sn-4Zr-2Mo (Ti-6242) alloy with a lamellar structure was applied by a thermal simulation machine Gleeble 3800 at a temperature of 1223-1370K and a strain rate of 0.01-10s(-1). Constitutive relations between the flow stress and strain at different temperatures and strain rates were constructed based on the Arrhenius equation. Processing maps based on the dynamic material model at strains of 0.5, 1.0, and 1.25 were also constructed to analyze the mechanism and instability of high-temperature deformation. Dynamic recrystallization was found to occur at 1223-1313K and 0.01-0.1s(-1), with a peak efficiency of power dissipation of 70%. Observations of the microstructure demonstrated that platelets and dynamic globularization were responsible for dynamic softening in the + phase field. Flow instability behaviors occurred at 1263-1343K/1.78-10s(-1), 1233-1283K/0.1-3.16s(-1), and 1353-1373K/0.56-1.78s(-1), and adiabatic shear bands and microcracks were observed in these domains. Thus, for the lamellar Ti-6242 alloy, the recommended hot rolling parameters were 1243-1333K and 0.01-0.1s(-1). Electron backscattered diffraction results revealed that the dynamic restoration mechanism in the phase field was dynamic recovery when the strain rate was as high as 10s(-1).