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Original Reports

Low-alloy content Ti-Mo-based alloys with large superelasticity and narrow stress hysteresis for potential biomedical applications

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Pages 759-768 | Received 25 Mar 2024, Published online: 28 Jul 2024

Figures & data

Table 1. Nominal and actual chemical compositions of the studied Ti-8Mo-6Zr-6Sn-(0–5)Al (wt%) alloys.

Figure 1. XRD patterns (a), DSC curves (b) and loading-unlading stress-strain curves (c) of the TMZSA specimens solid-solution treated at 900°C for 30 min. The red dashed lines with arrows below the stress-strain curves in (c) represent the recovery strain due to the shape memory effect.

Figure 1. XRD patterns (a), DSC curves (b) and loading-unlading stress-strain curves (c) of the TMZSA specimens solid-solution treated at 900°C for 30 min. The red dashed lines with arrows below the stress-strain curves in (c) represent the recovery strain due to the shape memory effect.

Figure 2. Comparison maps of stress hysteresis (Δσhys) vs σβα (a) and stress hysteresis (Δσhys) vs alloying element content (b) of 4Al and 5Al alloy specimens in the present study and other typical superelastic Ni-free Ti-Nb-, Ti-Zr(-Hf)- and Ti-Mo-based shape memory alloys subjected to solid-solution treatment (ST), annealing (AN) or aging treatment (AG) [Citation2–4,Citation11,Citation14,Citation16–39]. The σβα represents the critical stress for inducing βα″ martensitic transformation. Alloy compositions in at% in alloys are converted to wt% in (b) for comparison. The red arrows in (a) represent the desired properties of narrow stress hysteresis and high yield strength (σβα) and those in (b) represent the desired alloys with low content of alloying elements and narrow stress hysteresis.

Figure 2. Comparison maps of stress hysteresis (Δσhys) vs σβ→α″ (a) and stress hysteresis (Δσhys) vs alloying element content (b) of 4Al and 5Al alloy specimens in the present study and other typical superelastic Ni-free Ti-Nb-, Ti-Zr(-Hf)- and Ti-Mo-based shape memory alloys subjected to solid-solution treatment (ST), annealing (AN) or aging treatment (AG) [Citation2–4,Citation11,Citation14,Citation16–39]. The σβ→α″ represents the critical stress for inducing β → α″ martensitic transformation. Alloy compositions in at% in alloys are converted to wt% in (b) for comparison. The red arrows in (a) represent the desired properties of narrow stress hysteresis and high yield strength (σβ→α″) and those in (b) represent the desired alloys with low content of alloying elements and narrow stress hysteresis.

Figure 3. Cyclic loading-unloading stress-strain curves obtained at room temperature of the 4Al (a) and 5Al (b) alloy specimens solid-solution treated at 900°C for 30 min. The applied strain of the first cycle is set as 1.5% and is increased by 0.5% in each following cycle. (c) The plot of recovery strain (ϵr) as a function of the applied strain of 4Al and 5Al alloy specimens in the present study and other typical superelastic Ni-free Ti-Mo-based shape memory alloys subjected to solid-solution treatment (ST), annealing (AN) or aging treatment (AG) [Citation4,Citation5,Citation16–18,Citation38,Citation39].

Figure 3. Cyclic loading-unloading stress-strain curves obtained at room temperature of the 4Al (a) and 5Al (b) alloy specimens solid-solution treated at 900°C for 30 min. The applied strain of the first cycle is set as 1.5% and is increased by 0.5% in each following cycle. (c) The plot of recovery strain (ϵr) as a function of the applied strain of 4Al and 5Al alloy specimens in the present study and other typical superelastic Ni-free Ti-Mo-based shape memory alloys subjected to solid-solution treatment (ST), annealing (AN) or aging treatment (AG) [Citation4,Citation5,Citation16–18,Citation38,Citation39].

Table 2. Comparison of σβα, Δσhys and ϵrmax measured by cyclic loading-unloading tensile tests of Ti-8Mo-6Zr-6Sn-(4, 5)Al and typical superelastic Ni-free Ti-Nb, Ti-Zr and Ti-Mo-based shape memory alloys subjected to solid-solution treatment or aging treatment for biomedical applications.

Figure 4. Selected-area diffraction patterns and the corresponding dark-field TEM images taken by the circled diffraction spots for the 4Al (a, a-1) and 5Al (b, b-1) alloy specimens solid-solution treated at 900°C for 30 min.

Figure 4. Selected-area diffraction patterns and the corresponding dark-field TEM images taken by the circled diffraction spots for the 4Al (a, a-1) and 5Al (b, b-1) alloy specimens solid-solution treated at 900°C for 30 min.

Figure 5. A schematic diagram showing the Al content dependence of σβα: (a) β matrix without ωath, (b) β matrix with ωath adapted from Refs. [Citation2,Citation9].

Figure 5. A schematic diagram showing the Al content dependence of σβ→α″: (a) β matrix without ωath, (b) β matrix with ωath adapted from Refs. [Citation2,Citation9].
Supplemental material

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