Abstract
The high-temperature flow behavior of TB8 titanium alloys with two different grain sizes was investigated in this present work. Results show that a significant characteristic of stress drop is visible at the start stage of the hot deformation process when the strain rates are 100 and 10−1 s−1. With the further increasing of strain, the flow stress initially rises to a maximum value and subsequently attains a plateau for the strain rates of 100 s−1 and a slight decrease for the strain rates of 10−1 s−1. Only dynamic recovery occurs under these deformation conditions. When the strain rates drop to 10−3 s−1, the dynamic recrystallization takes place during hot deformation. The values of deformation activation energy and materials constants at different strains were calculated. The processing maps at different strains were established for the fine- and coarse-grained alloys. The optimal processing parameter for hot processing was attained to be 900 °C/10−3 s−1 for fine-grained alloys and 950 °C/10−3 s−1 for coarse-grained alloys, respectively.
Highlights
Titanium alloys with metastable β phase structure exhibit an ultra-high strength, exceptional corrosion resistance, outstanding fracture toughness, and reasonable ductility, which has been extensively used as structural materials in the aerospace field [1,2,3]
There have been few studies about the high-temperature flow behavior of TB8 titanium alloys containing different initial grain sizes. The objective of this present work was to thoroughly understand the effect of initial grain size on hot deformation behavior of TB8 titanium alloys based on the true stress-strain curve, processing maps for hot working, and microstructure analysis
To investigate the initial grain size effect on the hot deformation behavior of TB8 titanium alloy in the single β phase field, the forged bar was firstly subjected to a solution treatment at 900 and 1000 ◦ C
Summary
Titanium alloys with metastable β phase structure exhibit an ultra-high strength, exceptional corrosion resistance, outstanding fracture toughness, and reasonable ductility, which has been extensively used as structural materials in the aerospace field [1,2,3]. TB8 titanium alloy exhibits a larger deformation resistance and a narrow hot-working range during forging process. It is very hard to manufacture TB8 titanium alloy into a product with complicated shape by the means of hot rolling, hot forging, and hot extrusion in actual industrial processes [6,7]. It is well known that the mechanical properties of critical parts are significantly affected by the microstructure of TB8 titanium alloy formed during forging process. It is rather critical to better control the deformation microstructure for TB8 titanium alloy to achieve desired mechanical properties
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