Microstructure and Mechanical Properties of Ti-6Al-4V Additively Manufactured by Electron Beam Melting with 3D Part Nesting and Powder Reuse Influences

• Published in: Journal of Manufacturing and Materials Processing Vol. 6; no. 1; p. 21
• Main Authors: Wanjara, Priti, Backman, David, Sikan, Fatih, Gholipour, Javad, Amos, Robert, Patnaik, Prakash, Brochu, Mathieu
• Format: Journal Article
• Language: English
• Published: Basel MDPI AG 01.02.2022
• Subjects: Additive manufacturing; Aircraft; Design; Discount coupons; Ductility; Electron beam melting; Fatigue strength; Geometry; Industrial applications; Investigations; Lasers; Machining; Mechanical properties; Microstructure; Morphology; Nesting; Oxygen; Oxygen content; powder bed fusion; Raw materials; Specifications; Surface finish; Surface layers; Tensile properties; Tensile strength; Three dimensional printing; titanium alloy; Titanium base alloys; United States > US; Japan
• ISSN: 2504-4494; 2504-4494
• DOI: 10.3390/jmmp6010021

To better support the transition to more industrial uses of additive manufacturing, this study examined the use of an Arcam Q20+ industrial 3D printer for producing heavily nested Ti-6Al-4V parts with both in-specification (IS) and out of specification (OS) oxygen content in reused grade 5 powder chemistries. Both the OS and IS powder chemistries were evaluated to understand their impact on build integrity and on static and fatigue performance. The results from our evaluations showed that controlling the bed preheat temperature in the Q20+ to relatively low values (326–556 °C) was effective in limiting microstructural coarsening during the long build time and enabled adequate/balanced performance vis à vis the tensile strength and ductility. Overall, the tensile properties of the IS Ti-6Al-4V material in the as-built and machined states fully met the requirements of ASTM F2924-14. By contrast, the ductility was compromised at oxygen levels above 0.2 wt.% (OS) in Ti-6Al-4V produced by EBM. Removal of the surface layer by machining increased the consistency and performance of the IS and OS Ti-6Al-4V materials. The fatigue behaviour of the EBM Ti-6Al-4V material was in the range of properties produced by casting. Due to the strong influence of both the surface finish and oxygen content on the fatigue strength, the IS Ti-6Al-4V material exhibited the highest performance, with results that were in the range of parts that had been cast plus hot isostatically pressed.