TY - JOUR
T1 - Microstructure refinement via single-step heat treatment in LPBF-fabricated TA15 alloy for high strength and ductility
AU - Shi, Ruixing
AU - Tian, Jiaqiang
AU - Zheng, Diling
AU - Hou, Le
AU - Wang, Meng
AU - Wang, Jincheng
AU - Lin, Xin
AU - He, Feng
N1 - Publisher Copyright:
© 2026 The Authors.
PY - 2026/5/1
Y1 - 2026/5/1
N2 - The Ti–6.5Al–2Zr–1Mo–1V (TA15) alloy fabricated by laser powder bed fusion (LPBF) generally exhibits high strength but limited ductility, mainly owing to the dominance of α′ martensite within coarse columnar prior-β grains. Achieving effective microstructure refinement via feasible and cost-effective heat treatment remains a critical goal for improving ductility. However, conventional heat treatment routines often lead to coarser α lath structures relative to the as-built martensite or require complicated processing routes. In this work, using a simple one-step annealing treatment, we successfully refined the microstructure of LPBF-fabricated TA15 alloy, significantly enhancing ductility with only a minor loss in strength. Following annealing at 800∼850 °C for 2 h and subsequent furnace cooling, a well-refined lamellar α+β microstructure was obtained. Compared with furnace cooling, water quenching further tailors the retained β phase into distinct layers of considerable thickness. This refined microstructure delivers an excellent strength–ductility synergy: a tensile strength of 1058 MPa accompanied by a ductility of 20.4%, far exceeding the 10.2% elongation of the as-built alloy. Such abnormal microstructure refinement during single-step annealing is attributed to the temperature-dependent competition between α′ martensite decomposition and thermal coarsening. Specifically, within 800∼850 °C, the decomposition of α′ martensite plays a dominant role in microstructure evolution, giving rise to lamellar refinement. This work demonstrates that a simple one-step annealing process can effectively regulate the as-built microstructure and achieve an outstanding mechanical balance, providing a practical and efficient approach for optimizing the mechanical performance of LPBF-manufactured TA15 components.
AB - The Ti–6.5Al–2Zr–1Mo–1V (TA15) alloy fabricated by laser powder bed fusion (LPBF) generally exhibits high strength but limited ductility, mainly owing to the dominance of α′ martensite within coarse columnar prior-β grains. Achieving effective microstructure refinement via feasible and cost-effective heat treatment remains a critical goal for improving ductility. However, conventional heat treatment routines often lead to coarser α lath structures relative to the as-built martensite or require complicated processing routes. In this work, using a simple one-step annealing treatment, we successfully refined the microstructure of LPBF-fabricated TA15 alloy, significantly enhancing ductility with only a minor loss in strength. Following annealing at 800∼850 °C for 2 h and subsequent furnace cooling, a well-refined lamellar α+β microstructure was obtained. Compared with furnace cooling, water quenching further tailors the retained β phase into distinct layers of considerable thickness. This refined microstructure delivers an excellent strength–ductility synergy: a tensile strength of 1058 MPa accompanied by a ductility of 20.4%, far exceeding the 10.2% elongation of the as-built alloy. Such abnormal microstructure refinement during single-step annealing is attributed to the temperature-dependent competition between α′ martensite decomposition and thermal coarsening. Specifically, within 800∼850 °C, the decomposition of α′ martensite plays a dominant role in microstructure evolution, giving rise to lamellar refinement. This work demonstrates that a simple one-step annealing process can effectively regulate the as-built microstructure and achieve an outstanding mechanical balance, providing a practical and efficient approach for optimizing the mechanical performance of LPBF-manufactured TA15 components.
KW - Heat treatment
KW - Laser powder bed fusion
KW - Mechanical properties
KW - Microstructure
KW - TA15 titanium alloy
UR - https://www.scopus.com/pages/publications/105038621957
U2 - 10.1016/j.jmrt.2026.05.094
DO - 10.1016/j.jmrt.2026.05.094
M3 - 文章
AN - SCOPUS:105038621957
SN - 2238-7854
VL - 42
SP - 8120
EP - 8131
JO - Journal of Materials Research and Technology
JF - Journal of Materials Research and Technology
ER -