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Open Access

Systematic research on thermal-deformation behavior and mechanism for a mono-phase near-β titanium alloy TC18

Jiangli GUOaLiang HUANGa( )Kezhuo LIUaShiqi GUOaChangmin LIb
State Key Laboratory of Materials Processing and Die & Mould Technology, School of Materials Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074, China
China National Erzhong Group Deyang Wanhang Die Forging Co. LTD., Deyang 618000, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Thermal-deformation behavior and mechanism of a near-β titanium alloy TC18 in the mono-phase zone were studied by isothermal-compression experiments. The flow behavior of the alloy is predicted by an Arrhenius-constitutive equation considering strain. From the hot-working diagram, the unstable region primarily concentrates in high-strain-rate region, and is dominated by Deformation Bands (DBs) and Adiabatic Shear Bands (ASBs). The numbers of DBs and ASBs increase with temperature, and DBs are the precursors to ASB. Obvious Dynamic Recovery (DRV), Discontinuous Dynamic Recrystallization (DDRX), and Continuous Dynamic Recrystallization (CDRX) exist in the stable region. The predominant microstructural evolution mechanisms at large strains shift from the synergistic effect of CDRX and DDRX below the inflection point temperature and at low strain rate, and the inhibitory effect of DDRX on CDRX above the inflection point temperature and at low strain rate, to the synergistic effect of both at medium strain rate, accompanied by enhanced DRV, and finally to DBs and ASBs at high strain rate. The main microtexture components for the deformed alloy are ηbcc fiber, εbcc fiber, αbcc fiber, γbcc fiber, and ξbcc fiber. The deformation microtexture is weakened owing to the stochastic orientation distribution of DRX grains.

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Chinese Journal of Aeronautics

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Cite this article:
GUO J, HUANG L, LIU K, et al. Systematic research on thermal-deformation behavior and mechanism for a mono-phase near-β titanium alloy TC18. Chinese Journal of Aeronautics, 2026, 39(6). https://doi.org/10.1016/j.cja.2025.104043

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Received: 11 March 2025
Revised: 07 May 2025
Accepted: 12 May 2025
Published: 24 December 2025
© 2026 The Authors. Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).