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Ti6Al4V alloy patient-customized implants (PCI) are often fabricated using laser powder bed fusion (LPBF) and annealed to enhance the microstructural, physical and mechanical properties. This study aims to demonstrate the effects of annealing on the physio-mechanical properties to select optimal process parameters.

Test samples were fabricated using the Taguchi L9 approach by varying parameters such as laser power (LP), laser velocity (LV) and hatch distance (HD) to three levels. Physical and mechanical test results were used to optimize the parameters for fabricating as-built and annealed implants separately using Grey relational analysis. An optimized parameter set was used for fabricating biological test samples, followed by animal testing to validate the qualified parameters.

Two optimized sets of process parameters (LP = 100 W, LV = 500 mm/s and HD = 0.08 mm; and LP = 300 W, LV = 1,350 mm/s and HD = 0.08 mm) are suggested suitable for implant fabrication regardless of the inclusion of annealing in the manufacturing process. The absence of any necrosis or reaction on the local tissues after nine weeks validated the suitability of the parameter set for implants.

To help PCI manufacturers in parameter selection and to exclude annealing from the manufacturing process for faster implant delivery.

To the best of the authors’ knowledge, this is probably a first attempt that suggests LPBF parameters that are independent of inclusion of annealing in implant fabrication process.

Additive manufacturing of metallic scaffolds using laser powder bed fusion is challenging because of the accumulation of extra material below overhanging and horizontal surfaces. It reduces porosity and pore size and increases the effective strut size. These challenges are normally overcome by using volumetric energy density (VED) values lower than the optimum values, which, however, results in poor physio-mechanical properties. The purpose of this study is to assist scaffold manufacturers with a novel approach to fabricate stronger yet accurate scaffolds.

This paper presents a strategy for laser exposure that enables fabricating titanium-6–aluminum-4–vanedium (Ti6Al4V) alloy scaffolds with the required properties without compromising the geometric features. The process starts from computer-aided design models sliced into layers; dividing them into core (upper) and downskin (lower) layers; and fabrication using hybrid VED (low values for downskin layers and high values for core layers).

While exposing the core layers, laser remelted the downskin layers, resulting in better physio-mechanical properties (surface roughness, microhardness and density) for the whole strut without affecting its dimensional accuracy. A regression equation was developed to select the downskin thickness for a given combination of strut thickness and core VED to achieve the desired range of properties. The proposed approach was validated using microstructure analysis and compression testing.

This paper is expected to be valuable for the manufacturers of Ti6Al4V scaffolds, in achieving the desired properties.

This is probably the first time the hybrid VED approach has been applied for obtaining scaffolds with the desirable physio-mechanical and geometrical properties.