Abstract
An analysis pertaining to hot deformation behavior was conducted on two unique titanium alloy microstructures. Each product was manufactured from commercially available blended elemental Ti-6Al-4V powder, consolidated by sintering in vacuum or hydrogen. The initial microstructures produced by these distinctive sintering atmospheres are represented by a coarse lamellar structure (produced by vacuum sintering) and a very fine lamellar structure [produced by Hydrogen Sintering Phase Transformation (HSPT)]. Performance of these materials was assessed by simulating representative titanium breakdown and conversion during thermomechanical processing through elevated temperature compression testing on a Gleeble® 3500 Hydrawedge II® system. Compression tests were performed on cylindrical specimens at sub and near-transus temperatures (850 °C, 900 °C, 950 °C, and 1000 °C) and at moderate strain rates of 0.01 and 0.10 s−1. The very fine lamellar microstructure exhibited similar flow behavior compared to the coarse lamellar structure, although with a typically slightly higher peak stress and greater degree of flow softening. In addition, the microstructure produced by HSPT retained a fine, equiaxed structure upon deformation, making it highly suitable for powder-based thermomechanically processed titanium alloy products.
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