Abstract
Processing trials have produced a three-dimensional, thin-walled structure of representative aerospace component geometry, fabricated directly by laser melting of Ti 6Al4V powder. This additive-built form has been subjected to metallographic characterization. The fabrication technique is evaluated as an economic, commercial process that can add features such as bosses or flanges as a hybrid-manufacturing route for existing forms of gas turbine components. The samples were extracted from six locations with different wall thickness, varying forms, and intersecting ligament geometries. A fine-scale Widmanstätten colony microstructure was consistent throughout the structure within grains elongated parallel to the axis of epitaxy. Evidence of limited grain boundary α was detected; however, this was never continuous around individual grains. A moderate Burgers texture was measured employing electron backscatter diffraction (EBSD), which is consistent with the melt/cast titanium alloy forms cooling through the β transus.
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The authors would like to acknowledge the financial and technical support of Rolls-Royce plc in the production of this work.
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Manuscript submitted July 12, 2011.
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Clark, D., Whittaker, M.T. & Bache, M.R. Microstructural Characterization of a Prototype Titanium Alloy Structure Processed via Direct Laser Deposition (DLD). Metall Mater Trans B 43, 388–396 (2012). https://doi.org/10.1007/s11663-011-9599-x
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DOI: https://doi.org/10.1007/s11663-011-9599-x