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Materials Science in Additive Manufacturing                             Mechanical properties of NiTi TPMS




            Table 1. The processing parameter for laser powder bed   15 cycles. After the cycles, the sample was heated in a water
            fusion                                             bath at 100°C for 3 min. The ratio of height changes before
                                                               and after heating to the original height was measured, and
            Parameters                                Value
                                                               the shape memory recovery ratio (η) was calculated using
            Laser power (W)                            240     Equation II. The loading and unloading speeds were both
            Laser speed (mm/s)                         600     set at 0.5 mm/min.
            Hatch spacing (mm)                         0.1     η = (h −h )/(h −h )×100%                    (II)
            Layer thickness (mm)                      0.03          3  2  2  1
            Remelting power (W)                        60        where h  is the height of the sample before testing, h  is
                                                                        1
                                                                                                           2
            Remelting speed (mm/s)                     200     the height of the sample after the end of the cycle, and h  is
                                                                                                           3
                                                               the height of the sample after heating, all in mm.
                                                                 Microhardness of the aged samples was measured using
            Table 2. Process parameters of aging heat treatment
                                                               a Vickers microhardness tester (HV-1000, CVOK Co., Ltd.,
            Sample no.  Shape  Temperature   Aging   Cooling   China) with a 1000 gf load applied for 15 s.
                                  (°C)    time (h)  method
            RGCS-A0   Rod-shape    -        -    -             2.6. DIC test
            RGCS-A2   Rod-shape   400       2    Air cooling   The deforming behavior of the gyroid structure was
            RGCS-A4   Rod-shape   400       4    Air cooling   analyzed  using  VIC-3D  (Related Solutions  Co. Ltd.,
            RGCS-A6   Rod-shape   400       6    Air cooling   United States of America). A white paint was sprayed on
            RGCS-A8   Rod-shape   400       8    Air cooling   the surface as a background in advance, and random black
                                                               spots were sprayed after drying for DIC data acquisition
            RGCS-A10  Rod-shape   400       10   Air cooling   and analysis. During  the static  compression  test,
            SGCS-A0   Sheet-shape  -        -    -             deformation was captured by a data acquisition camera
            SGCS-A2   Sheet-shape  400      2    Air cooling   (camera resolution=3376 × 2704 pixels), with a camera
            SGCS-A4   Sheet-shape  400      4    Air cooling   sampling frequency of 1 Hz. Subsequently, the collected
            SGCS-A6   Sheet-shape  400      6    Air cooling   images during the structural deformation process were
            SGCS-A8   Sheet-shape  400      8    Air cooling   calculated and analyzed using DIC software. To achieve a
            SGCS-A10  Sheet-shape  400      10   Air cooling   more accurate analysis of the deformation of the Gyroid
            Abbreviations: RGCS: Rod-shaped gyroid cellular structure;    structure, the non-interest region of the gyroid’s internal
            SGCS: Sheet-shaped gyroid cellular structure.      holes was removed from the initial image to identify the
                                                               region of interest (ROI), and the strain cloud diagram of
            Furthermore, the phase transformation temperatures   the maximum principal strain was obtained.
            of the aged sample were measured using a differential   2.7. Fracture morphology
            scanning calorimeter (DSC) operating with a heating and
            cooling rate of 10°C/min in a helium atmosphere within a   The fracture morphology of RGCS and SGCS was analyzed
            temperature range of 0 – 80°C.                     using SEM (TESCAN CLARA, TESCAN, Czech Republic)
                                                               with an acceleration voltage of 10 kV.
            2.5. Mechanical properties and functional
            properties test                                    3. Results and discussion
            Compression test was conducted using a CMT5105     3.1. Effect of aging time on microstructure and
            testing machine (SUST Co., Ltd., China) at room    phase transformation behavior
            temperature. The superelasticity test was conducted in   The metallographic structure of the NiTi minimum surface
            an electronic  universal  testing  machine equipped  with   structure after different aging times in the X–Z direction
            a high-temperature test chamber (CMT5105GD, SUST   is depicted in  Figure  2. The  figure illustrates that the
            Co., Ltd., China). The temperature was raised above the   microstructures of the samples exhibited coarse columnar
            end  temperature  of  reverse  martensitic  transformation,   crystals. During the LPBF process, samples were printed
            and the recoverable strain and unrecoverable strain were   layer by layer from bottom to top, resulting in significant
            determined based on the stress-strain curve obtained from   temperature gradient changes that facilitated vertical
            loading the sample from 0% to 8% strain with a 2% strain   grain growth and columnar crystal formation. The crystal
            increment.  The  SME  test  involved  loading  the  sample   size of sample A0, as measured using ImageJ software,
            to a 6% strain at room temperature and unloading it for   was 56.46 ± 10.92 µm. In contrast, samples aged for 2 h,


            Volume 3 Issue 2 (2024)                         4                              doi: 10.36922/msam.3137
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