Abstract

Titanium alloys have a high strength-to-weight ratio, fatigue performance and excellent corrosion resistance, and therefore are widely used in the aerospace sector due to their ability to withstand severe mechanical and thermal stresses in service. There are numerous cases where it would be desirable to use different titanium alloys in defined subcomponent regions to improve performance and efficiency. Conventional processing routes do not permit components to be produced with multiple titanium alloys and thus, design efficiency and optimization of component properties is compromised or over-engineered. In this study, a hybrid solid-state consolidation route is presented whereby field assisted sintering technology (FAST) is exploited to diffusion bond (DB) dissimilar titanium alloy powders in defined regions—a process termed FAST-DB. Titanium alloy powders Ti-6Al-4V (Ti-64) and Ti-6Al-2Sn-4Zr-2Mo (Ti-6242) were bonded using FAST in order to study the tensile deformation behavior and strain localization across a dissimilar alloy solid-state bond. FAST-DB was carried out at the sub- and super- beta transus temperatures of both alloys to generate dissimilar microstructure morphologies across the bond. In all cases, diffusion bonds showed excellent structural integrity with no defects and a smooth hardness profile across the bond. The deformation characteristics of the bonds was studied using two different tensile test approaches. The first approach used ASTM standard specimens to measure the mechanical properties of FAST-DB samples and study the location of the tensile failure. The second approach used a microtester and optical Digital Image Correlation to capture the grain interaction in the bond region under tensile loading. The work demonstrated that the diffusion bond remains intact and that tensile failure occurs in Ti-64 (i.e. the lower strength alloy) and is independent of the grain crystal orientation. The results from this study will provide materials engineers confidence in nesting FAST-DB technology in future near net shape manufacturing routes.

Highlights

  • TITANIUM alloys are widely used in the aerospace sector due to their high strength-to-weight ratio, corrosion resistance and ability to operate at relatively high temperatures.[1,2,3,4] For example, 25-30 pct of the weight of a gas turbine aero-engine is made up of titanium alloys such as Ti-6Al-4V (Ti-64), Ti-6Al-2Sn-4Zr-2Mo (Ti-6242) and Ti-6Al-2Sn-4Zr-6Mo (Ti-6246).[2]

  • The standard tensile test samples were machined from two separated field assisted sintering technology (FAST)-diffusion bond (DB) discs of 250 mm diameter while the optical Digital Image Correlation (DIC) samples were machined from one FAST-DB disc of 60 mm diameter

  • Microstructure of FAST-DB consolidated preforms The microstructure obtained for the subtransus (TDB1) and the supertransus (TDB2) FAST-DB samples are shown in Figures 5(a) and (b)

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Summary

Introduction

TITANIUM alloys are widely used in the aerospace sector due to their high strength-to-weight ratio, corrosion resistance and ability to operate at relatively high temperatures.[1,2,3,4] For example, 25-30 pct of the weight of a gas turbine aero-engine is made up of titanium alloys such as Ti-6Al-4V (Ti-64), Ti-6Al-2Sn-4Zr-2Mo (Ti-6242) and Ti-6Al-2Sn-4Zr-6Mo (Ti-6246).[2]. 3064—VOLUME 52A, JULY 2021 cost and the high Buy-to-Fly ratio (BTF), which can exceed 10:1.[5] Aerospace titanium alloy components used in demanding environments require a good combination of creep and fatigue resistance, yet are designed and manufactured from a single titanium alloy with a similar microstructure and set of properties in different subcomponent regions. The performance of titanium components could be improved by using a tailored creep resistant or fatigue resistant titanium alloy in defined subcomponent regions. The ability to manufacture a component with dissimilar alloys in site-specific, subcomponent regions would enable designers to optimize the performance of titanium forged components. There is a drive to move towards near-net shape manufacturing with low METALLURGICAL AND MATERIALS TRANSACTIONS A material wastage in order to reduce the excessive BTF of titanium aerospace parts

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