2016
DOI: 10.1016/j.msea.2015.09.060
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Tracking microstructure, texture and boundary misorientation evolution of hot deformed and post-deformation annealed Ti–6Al–4V alloy

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Cited by 30 publications
(4 citation statements)
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“…Or, it may well be a product of the thermomechanical history during production of the base material prior to the EBM welding process. Significant effort is applied during manufacturing to ensure the breakup of these structures in an attempt to avoid deleterious effects on crack initiation and fatigue [35]. As these microstructural features coincide with the residual stress protrusion, it is highly probable that the two findings are interrelated.…”
Section: Discussionmentioning
confidence: 99%
“…Or, it may well be a product of the thermomechanical history during production of the base material prior to the EBM welding process. Significant effort is applied during manufacturing to ensure the breakup of these structures in an attempt to avoid deleterious effects on crack initiation and fatigue [35]. As these microstructural features coincide with the residual stress protrusion, it is highly probable that the two findings are interrelated.…”
Section: Discussionmentioning
confidence: 99%
“…Due to the requirements of the overlap ratio of the laser beam scanning distance and the thickness of the powder bed, the overlap region and the edge of the molten pool are reheated and melted during the preparation of new layers. This process similar to annealing results in recrystallization of LAGBs previously formed and transformation into HAGBs [31]. However, the short remelting time prevents the solidified layer from being completely recrystallized, which is an important reason for the retention of LAGBs [32,33].…”
Section: Phase and Microstructurementioning
confidence: 99%
“…The globularization of titanium alloy with lamellar colony during hot working can obtain fine and homogeneous microstructure extensively used in aerospace field, which can ensure both optimal creep and optimal fatigue properties [2,3]. The inhomogenous globularization [4] often leads to the formation of microdefects (mixed grains, microstructure heredity and macrozone [5,6]) which seriously affect mechanical properties of aviation components. Therefore, precise control on globularization of titanium alloy with lamellar colony would exert a great significance for optimizing hot-working parameters, predicting and regulating microstructure and improving properties of titanium alloy products.…”
Section: Introductionmentioning
confidence: 99%
“…The thermal mechanical process is very sensitive to hotworking parameters and microstructure parameters, thus resulting in the difficulty in precisely controlling globularization. The detailed characteristics are described as follows: (a) complex and diverse morphologies (initial widmanstatten alpha [4], secondary alpha [28] and fine acicular martensitic alpha [29]) lead to the difference in globularization dynamics; (b) the meso-scale heterogeneous deformation (strain localization at lamellar-scale, strain partitioning behavior at colony-scale, macro-deformation bands at polycrystal-scale [15]); (c) the complex coupling effects of hot-working parameters and microstructure parameters (flow softening due to loss of interfacial coherency [3], evolution of geometry necessary dislocation(GND) at alpha/beta interface [29], the effect of lattice rotation [14,30] on meso-scale heterogeneous deformation). In general, an in-depth understanding of the effects of hot-working parameters and microstructure parameters can allow better control globularization of titanium alloy with lamellar colony.…”
Section: Introductionmentioning
confidence: 99%