Abstract

Additively-manufactured Ti-6Al-4V (Ti64) exhibits high strength but in some cases inferior elongation to those of conventionally manufactured materials. Post-processing of additively manufactured Ti64 components is investigated to modify the mechanical properties for specific applications while still utilizing the benefits of the additive manufacturing process. The mechanical properties and fatigue resistance of Ti64 samples made by electron beam melting were tested in the as-built state. Several heat treatments (up to 1000 °C) were performed to study their effect on the microstructure and mechanical properties. Phase content during heating was tested with high reliability by neutron diffraction at Los Alamos National Laboratory. Two different hot isostatic pressings (HIP) cycles were tested, one at low temperature (780 °C), the other is at the standard temperature (920 °C). The results show that lowering the HIP holding temperature retains the fine microstructure (~1% β phase) and the 0.2% proof stress of the as-built samples (1038 MPa), but gives rise to higher elongation (~14%) and better fatigue life. The material subjected to a higher HIP temperature had a coarser microstructure, more residual β phase (~2% difference), displayed slightly lower Vickers hardness (~15 HV10N), 0.2% proof stress (~60 MPa) and ultimate stresses (~40 MPa) than the material HIP’ed at 780 °C, but had superior elongation (~6%) and fatigue resistance. Heat treatment at 1000 °C entirely altered the microstructure (~7% β phase), yield elongation of 13.7% but decrease the 0.2% proof-stress to 927 MPa. The results of the HIP at 780 °C imply it would be beneficial to lower the standard ASTM HIP temperature for Ti6Al4V additively manufactured by electron beam melting.

Highlights

  • Licensee MDPI, Basel, Switzerland.Attribution (CC BY) licenseTi64(, are widely used in the automotive [1,2,3], aerospace and biomedical industry for their high strength to weight ratio and biocompatibility

  • The densities following hot isostatic pressings (HIP) at 780 ◦ C and at 920 ◦ C are within uncertainty, but the standard deviation is smaller at the lower temperature

  • Various post-treatments were studied in order to find a way to tailor demonstrated that the mechanical properties of EBM Ti64 parts change significantly as a the microstructure and the mechanical properties of EBM fabricated Ti-6Al-4V

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Summary

Introduction

Especially Ti-6Al-4V )Ti64(, are widely used in the automotive [1,2,3], aerospace and biomedical industry for their high strength to weight ratio and biocompatibility. At ambient conditions, Ti64 is a dual-phase material; primary phase α-Ti (HCP) co-exists with β-Ti (BCC). Increasing utilization of additive manufacturing (AM), enables the fabrication of stronger and lighter parts with more intricate geometries. AM processes yield parts with high density, commonly higher than 99.5% of the theoretical density [4,5]. Two main AM methodologies exist, the addition of material by

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