Abstract

The effect of grain-interior α precipitation on the β texture evolution of the near-β Ti-6246 alloy during through-transus forging was investigated in two-step sequential forgings. The microstructure and texture were analyzed using scanning electron microscopy, electron-backscatter diffraction, and X-ray diffraction. The previous β forging was performed at 1253 K at 0.01/s, while the subsequent forging in the (α + β) region was conducted at 1073 K at 0.01/s. The forging in the β region facilitated the penetration of the interior α phase into β grains and reduced the formation of grain boundary α. The {001} texture intensity increased during the forging in the single β region. By contrast, the increase in the {001} texture intensity was moderate at a lower temperature (1073 K) because the Schmid factor (SF) value of the {110}<111> slip system drastically decreased, but those of the {112}<111> and {123}<111> slip systems increased before α precipitation. During α precipitation for all β forging ratios, the {110}<111> slip system was activated, resulting in a lowering of the {001} texture intensity. The lower the forging temperature before interior α precipitation under a constant total forging ratio, the more the {001} texture intensity was suppressed in the final β texture, accompanied by interior α precipitation.

Highlights

  • Near-β titanium alloys are used for compressor disks in jet engines because of their high strength and high fracture toughness

  • To minimize the formation of harmful continuous α layers at grain boundaries (GBs) in the process, “through-transus” forging has been reported, in which the material temperature is lowered from the β single-phase region to the (α + β) dual-phase region through the β-transus temperature, Tβ, during forging [4]

  • The deformation of the β phase in a single β region results in a strong {001} texture, with the {001} crystal planes perpendicular to the forging direction (FD), whereas {001} and {111} textures develop in the (α + β) region [6]

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Summary

Introduction

Near-β titanium alloys are used for compressor disks in jet engines because of their high strength and high fracture toughness. The through-transus forging leads to the formation of α layers being broken up into individual segments on the GBs. The interior Widmanstätten α phase and spherical α phase precipitate within β grains and grow during deformation in the (α + β) dual-phase region, followed by subsequent cooling [3,5].

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