Effect of Strain Rate on Mechanical Behavior and Microstructure Evolution of Ti-Based T110 Alloy

Recently developed thermally hardenable medium-level alloyed titanium alloy T110 was studied from the viewpoint of microstructure influence on the mechanical behavior under quasi-static and high-strain rate deformation. The globular microstructures of two types differing in aspect ratio of alpha-globules were formed under thermomechanical processing conditions with different reductions (epsilon(total) = 2, and 3) and final annealing at 850 degrees C, 3 h. The thermally hardened state was formed by conventional solid-solution treatment at a temperature of two-phase alpha+beta field (880 degrees C, 45 min), water quenching, and final aging (550 degrees C, 5 h). Stress-strain dependencies were estimated on tension with strain rates varied from 8 center dot 10(-4) to 4 center dot 10(-2) s(-1), as well as compression with a strain rate of 10(-3) s(-1) (quasi-static) and under high-strain rates varied from 870 s(-1) to 3520 s(-1); the deformation with high-strain rates has been achieved using split Hopkinson pressure bar (SHPB) technique. The tested material was also assessed using strain energy (SE) parameter. A parallel study of the microstructure and crystallographic texture formed during testing allowed to propose a reliable deformation and fracture mechanisms, depending on the stress state (tension, compression) and strain rate. A special role of the initial microstructure is noted, which determines the plasticity of the tested alloy, the sites of pore nucleation, features of crack growth, as well as the localization of deformation, which is determined by the mode and rate of loading. It is established and explained why the best balance of strength and ductility, and thus, the highest SE values in the all tests carried out were ensured by the alloy in the state with a more uniform microstructure of globular morphology (after the rolling with reduction epsilon(total) =3), which, in turn, provided general superiority over the widely used Ti-6Al-4V alloy.