Abstract

Dislocation interactions were investigated in near-alpha titanium alloy Ti6242Si after low cycle fatigue. Samples from the gauge section and the crack initiation site on the fracture surface were studied. Grain pairs with different crystallographic orientations were analysed from the gauge section to understand the dislocation interactions near the boundary. Deformation was primarily caused by planar slip, localized into slip bands in primary alpha (αp) grains. Direct slip transfer was observed within grains having similar orientations. In contrast, slip transfer resulted in a different kind of dislocation nucleation in the neighboring hard grain where there was misorientation between the grains, with the observation of cross-slip. Strain transfer was observed between highly misoriented grain pairs. Crack nucleation occurred on an αp grain by basal plane splitting, due to the large tensile stress developed by a double ended pile-up. This kind of pile-up is suggested to result from the incomplete reversibility of dislocation motion during load reversals. The observation of superjogs on the basal dislocations in the crack nucleated αp grain provides a rationale for why cracks nucleate near, rather than on, the basal plane.

Highlights

  • The alloy was generally found to mainly deform by planar slip in αp grains; a typical pile-up observed in an αp grain is shown in Fig. 2, which is a BF-STEM micrograph of a sample taken from the gauge section when the beam direction is B = [10 0]

  • The dislocation interactions of near alpha titanium alloy Ti6242Si were studied after low cycle fatigue

  • The alloy mainly deforms by planar slip in αp grains and the two phase region αs+β acting as a barrier for slip transmission

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Summary

Introduction

Near-α titanium alloys such as Ti6242Si are employed in high temperature aero-engine compressors due to their combination of specific toughness, creep resistance and. The component is exposed to a variety of loading regimes during service, for e.g., high stresses in the low cycle fatigue regime may be experienced at the thrust peak associated with take-off. This continues to compromise design [5, 6] and is very important to understand.

Material and experiments
Dislocation interactions in the gauge section
Dislocation interactions on the fracture surface
Conclusions
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