2019
DOI: 10.1016/j.matchar.2018.10.027
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Automated image mapping and quantification of microstructure heterogeneity in additive manufactured Ti6Al4V

Abstract: In Additive Manufacturing AM, each volume of material experiences a complex thermal history due to both short-range effects, from the repeated overlap of the thermal field from each heat source pass, and long-range variation in the thermal boundary conditions, related to the part geometry and build height. With an  +  alloy, like Ti64, this can lead to significant local variation in the transformation microstructure, which can contribute to heterogeneity in the mechanical properties of a component. In order … Show more

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Cited by 32 publications
(22 citation statements)
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References 40 publications
(157 reference statements)
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“…[3][4][5] In the WAAM process, following each deposition pass, the solidified material below the fusion zone is heated to above the b-transus temperature to a depth equivalent to that of about 4 to 5 added layers and transforms on cooling to a basket weave lamellar a microstructure, with a small volume fraction of retained b. [6,7] There is also typically a thin layer of grain boundary a which delineates the prior b-grain boundaries. Heat-affected zone (HAZ) bands, associated with a temperature rise from re-heating in the range from above~800°C to the b-transus temperature (~980°C [6] ), are also generated by each heat source pass.…”
Section: B Waam Microstructuresmentioning
confidence: 99%
“…[3][4][5] In the WAAM process, following each deposition pass, the solidified material below the fusion zone is heated to above the b-transus temperature to a depth equivalent to that of about 4 to 5 added layers and transforms on cooling to a basket weave lamellar a microstructure, with a small volume fraction of retained b. [6,7] There is also typically a thin layer of grain boundary a which delineates the prior b-grain boundaries. Heat-affected zone (HAZ) bands, associated with a temperature rise from re-heating in the range from above~800°C to the b-transus temperature (~980°C [6] ), are also generated by each heat source pass.…”
Section: B Waam Microstructuresmentioning
confidence: 99%
“…Ti6Al4V is designed for a good balance of strength, ductility, fatigue and fracture properties. Ti6Al4V has been used as an important structural material in advanced aircraft since the 1960s [14]. Nippon Steel and the Sumitomo Metal Corporation acquired qualifications in 1985 from Rolls-Royce and started commercial production of titanium alloys for aircraft engines.…”
Section: General Informationmentioning
confidence: 99%
“…Alloying elements in titanium can be categorized into α-stabilizers, β-stabilizers or neutral additions, depending on which phase the elements tend to stabilize, or whether they effectively increase or decrease the solid-state α-β transus temperature of titanium [14]. α-stabilizers, including the substitutional element (aluminum) and the interstitial elements (oxygen, nitrogen and carbon), strongly increase the threshold temperature at which the α phase is stable, even if the solute content increases.…”
Section: Crystal Structurementioning
confidence: 99%
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