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Materials Science in Additive Manufacturing                             Mechanical properties of NiTi TPMS



            toward quasi-cleavage fracture mechanisms in RGCS-A4,   treatment at 350°C, the density of dimple and tear ridge in
            RGCS-A6, RGCS-A8, and RGCS-A10.                    the NiTi alloy increased, accompanied by the appearance
              Figure  12  depicts the fracture morphology of SGCS   of micro-cracks, indicative of ductile fracture. Subsequent
            after the compression test. Similar to RGCS-A0, the   heat treatment at 450°C resulted in the emergence
            fracture morphology of SGCS-A0 exhibited characteristics   of substantial microcracks, with the cleavage surface
            typical of river patterns and cleavage steps, without evident   becoming predominant. In addition, grain refinement was
            macroscopic plastic deformation. This observation suggests   observed after solution treatment, leading to a decrease in
            that brittle fracture is the primary fracture mechanism.   the average particle size from 52.43 µm to 15.45 µm.
            After  aging heat treatment, numerous dimpled fractures   3.3. Effect of aging heat treatment on the
            were  observed  in  SGCS-A2  and  SGCS-A4,  indicating  a   superelasticity
            shift toward ductile fracture mechanisms in these samples.
            With aging time exceeding 6  h, the dimples in SGCS   Superelasticity is an important characteristic of NiTi SMA,
            became shallower and fewer in number. Notably, the tear   denoting its capacity to undergo significant deformation on
            ridge observed in SGCS-A6 was significantly higher than   the application of stress to the austenite phase, exceeding
            in SGCS-A8 and SGCS-A10. These results suggest that   its elastic limit strain, and subsequently automatically
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            quasi-cleavage fracture was the fracture mechanism in   reverting to its original shape during unloading.
            SGCS-A6, SGCS-A8, and SGCS-A10.                    Figures 13 and 14 depict the stress-strain curves of RGCS
                                                               and SGCS subjected to 2%, 4%, 6%, and 8% compressive
              Yan  observed a significant presence of ductile dimples   strain  at  100°C,  respectively.  RGCS-A0,  RGCS-A2,
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            on the fracture surface of samples treated with a solid   RGCS-A6,  and  RGCS-A8  exhibited  the  capability to
            solution, indicating the dominance of ductile fracture.   withstand a compressive strain of 8%, accompanied by a
            After compression, the fracture pattern resembled a river-  reduction in unrecoverable strain from 3.12% to 1.27%
            like formation, indicating rapid crack propagation speed.   with increasing aging time. Conversely, SGCS exhibited
            This phenomenon was attributed to the absence of a plastic   commendable superelasticity up to 6% compressive strain,
            zone in the NiTi sample to prevent crack propagation   with a maximum unrecoverable strain not exceeding
            during compression. Bhardwaj  noted that after aging heat   1.35%. However, only the SGCS-A6 and SGCS-A8 samples
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            A                               B                                C














            D                               E                                F


















            Figure 16. Shape memory behavior of rod-shaped gyroid cellular structure (RGCS) under different strains with different aging times. (A) 0 h; (B) 2 h;
            (C) 4 h; (D) 6 h; (E) 8 h; and (F) 10 h.


            Volume 3 Issue 2 (2024)                         15                             doi: 10.36922/msam.3137
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