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Acta Metall Sin  2021, Vol. 57 Issue (6): 767-779    DOI: 10.11900/0412.1961.2020.00286
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Coupling Effect of Pre-Strain Combined with Isothermal Ageing on Mechanical Properties in a Multilayered Ti-10Mo-1Fe/3Fe Alloy
DAI Jincai, MIN Xiaohua(), ZHOU Kesong, YAO Kai, WANG Weiqiang
School of Materials Science and Engineering, Dalian University of Technology, Dalian 116024, China
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DAI Jincai, MIN Xiaohua, ZHOU Kesong, YAO Kai, WANG Weiqiang. Coupling Effect of Pre-Strain Combined with Isothermal Ageing on Mechanical Properties in a Multilayered Ti-10Mo-1Fe/3Fe Alloy. Acta Metall Sin, 2021, 57(6): 767-779.

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Abstract  

Owing to their low density, high specific strength, biocompatibility, and good corrosion resistance, titanium and its alloys have been widely used in the aerospace, biomedical, and marine engineering fields. As engineering applications of titanium alloys continue to develop, especially in special engineering projects, the service safety and stability of titanium alloys must be satisfied under extremely complex conditions. Unfortunately, traditional titanium alloys usually exhibit low plastic-deformation ability and no significant work hardening behavior, which limits their applicability. Improving both the strength and ductility of these materials is expected to broaden their engineering applications. In recent years, β-type (body-centered cubic) titanium alloys have shown good formability and impact toughness, by virtue of their diverse plastic deformation modes and excellent ageing strengthening. Therefore, they are promising candidates for titanium alloys with a good strength-ductility combination. In this work, a multilayered Ti-10Mo-1Fe/3Fe alloy was manufactured by a multi-pass hot rolling and heat treatment, and the coupling effects of pre-strain and isothermal ageing on the mechanical properties of the alloy were studied by various techniques: laser scanning confocal microscopy, XRD, SEM, SEM-EDS, EBSD, a Vickers hardness tester, and a tensile testing machine. After pre-strain and isothermal ageing, the alloy exhibited {332}<113> twins and slip bands alternately multilayered deformation microstructures. The alloy demonstrated a relatively high yield strength and large uniform elongation. The high yield strength resulted from the initial plastic deformation, which was dominated by dislocation slips due to isothermal ω-phase precipitation. The early onset of plastic instability after yielding was hindered by the pre-strain induced twins, and the uniform elongation was enhanced not only by the dynamic Hall-Petch effect caused by further twinning activation, but also by interactions between the twin and layer-interface. As demonstrated on this multilayered alloy with twinning and dislocation-slip coupled deformation, the strength-ductility combination in β-type titanium alloys can be controlled through the coupling effect of pre-strain induced {332}<113> twins and the subsequently precipitated ω phase.

Key words:  β-type titanium alloy      multilayered deformation microstructure      pre-strain induced {332}<113> twin      isothermal ω-phase      mechanical property     
Received:  31 July 2020     
ZTFLH:  TG146.2  
Fund: National Key Research and Development Program of China(2016YFB1100103)
About author:  MIN Xiaohua, professor, Tel: (0411)84708189, E-mail: minxiaohua@dlut.edu.cn

URL: 

https://www.ams.org.cn/EN/10.11900/0412.1961.2020.00286     OR     https://www.ams.org.cn/EN/Y2021/V57/I6/767

Fig.1  Schematics of ST (a), STA (b), STD (c), and STDA (d) samples for Ti-10Mo-1Fe/3Fe multilayered alloys (Black dots represent the ω phase after ageing, coarse and fine lines indicate twins and dislocation slip traces induced by pre-strain, respectively; ST—solution treatment, STA—ST + ageing, STD—ST + deformation, STDA—STD + ageing)
Fig.2  Schematic of tensile specimen for Ti-10Mo-1Fe/3Fe multilayered alloy (t—thickness) (unit: mm)
Fig.3  Vickers hardnesses of ST and STA (473-673 K) samples for Ti-10Mo-1Fe, Ti-10Mo-3Fe, and Ti-15Mo alloys (a), and SEM images of indentation of ST (b) and STA (623 K) (c) samples for Ti-10Mo-1Fe alloy
Fig.4  Nominal stress-strain curves (a, b) and true stress-strain (true σ-ε) and work hardening rate (WHR) curves (c, d) of ST, STA, and STDA samples for Ti-10Mo-1Fe (a, c) and Ti-10Mo-3Fe (b, d) alloys
Fig.5  In situ LSCM images of ST sample after 0 (a, e), 1% (b, f), 3% (c, g), and 5% (d, h) tensile strains for Ti-10Mo-1Fe (a-d) and Ti-10Mo-3Fe (e-h) alloys (The observed plane is normal to the transverse direction (TD), RD—rolling direction, ND—normal direction)
Fig.6  In situ LSCM images of ST (a, e), STD (b, f), STDA (c, g), and STDA-5% (d, h) samples for Ti-10Mo-1Fe (a-d) and Ti-10Mo-3Fe (e-h) alloys (The observed plane is normal to the TD)
Fig.7  Area fractions of twin and slip trace of ST (tensile strain of 1%-5%), STD, STDA, and STDA-5% samples for Ti-10Mo-1Fe and Ti-10Mo-3Fe alloys
Fig.8  XRD spectra (a, b) and lattice parameters of β phase (c) of ST, STD, STA, and STDA samples for Ti-10Mo-1Fe (a) and Ti-10Mo-3Fe (b) alloys
Fig.9  Secondary electron image (a) and elemental distribution images of Ti (b), Mo (c), and Fe (d) measured by EDS along the black line in ST sample for Ti-10Mo-1Fe/3Fe multilayered alloy (The analyzed plane is normal to the TD)
Fig.10  Vickers hardnesses of ST and STA (473-673 K) (a) and ST, STA, STD, and STDA samples (b) for Ti-10Mo-1Fe/3Fe multilayered alloy
Fig.11  Nominal stress-strain curves (a) and true stress-strain and WHR curves (b) of ST, STA, and STDA samples for Ti-10Mo-1Fe/3Fe multilay-ered alloy
Fig.12  Tensile properties of Ti-10Mo-1Fe, Ti-10Mo-3Fe alloys, and Ti-10Mo-1Fe/3Fe multilayered alloy in the present study (a), and relationship between deformation modes and mechanical properties of β titanium alloys (b)
Fig.13  In situ LSCM images (a-d) of ST sample with 0-5% tensile strains and EBSD maps of 5% tensile strained ST sample (e-h) for Ti-10Mo-1Fe/3Fe multilayered alloy (The observed plane is normal to the TD)
Fig.14  In situ LSCM images of ST (a), STD (b), STDA (c), and STDA-5% (d) samples for Ti-10Mo-1Fe/3Fe multilayered alloy (The observed plane is normal to the TD)
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