Additively manufactured Ti‐6Al‐4V microstructure tailoring for improved fatigue life performance
‐transus temperature, (2) a two‐step annealing HT whose first step exceeds the
‐transus temperature and the second step is an anneal below the
‐transus temperature, and (3) a sawtooth HT with temperatures oscillating below the
‐transus temperature. Tensile properties and fatigue crack growth behavior were assessed and compared to wrought Ti‐6Al‐4V. LPBF materials nominally exhibited a 17% yield stress reduction, 1.9% strain‐to‐failure increase, and 9.2% modulus of toughness decrease. Fatigue crack growth curves were used to assess the linear crack growth rate region and approximate fracture toughness (
). Post‐mortem fractography observed striations indicating the crack growth direction frequently changes direction providing an understanding of the slower crack growth rates observed in LPBF materials compared to their wrought counterpart.
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- Published
- May 02, 2024
- Vol/Issue
- 47(7)
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- 2599-2615
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