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Materials Science in Additive Manufacturing                             Mechanical properties of NiTi TPMS




















                                                     Figure 9. (Continued).

            while maintaining strength, with RGCS-A6 and RGCS-A8   the maximum compressive strength of RGCS-A6 only
            demonstrating the highest yield strength.          exhibited a modest increase of 22.23%, reaching 29.38 MPa
              In contrast, the aging heat treatment shortened the   compared to RGCS-A0. These results indicate a significant
            yield plateau of SGCS, leading to a rapid transition   enhancement in the mechanical properties of rod-shaped
            through the yield stage and prompt initiation of fracture   gyroid structures due to aging heat treatment.
            on reaching its strength limit. The failure strain of RGCS   Five evenly distributed points were extracted from the
            increased from 10% to 15%, while that of SGCS decreased   DIC strain cloud diagram, from top to bottom, to analyze
            from 10% to approximately 5%. These results indicate that   the  compression  process of  the  gyroid,  as  depicted  in
            aging heat treatment improved the plasticity and strength   Figures 7 and 8. Except for RGCS-A0, the strain at point
            of RGCS but increased the brittleness of SGCS. Due to   P0 from RGCS-A2 to RGCS-A10 consistently exceeded
            age hardening, the strength of SGCS increased while   that of the other four points after 45 s. Notably, the strain
            its  plasticity  and  toughness  declined, causing it  to  enter   at the P0 point of samples A4, A6, and A8 surpassed 2%,
            the compression fracture stage more rapidly, consistent   as shown in Figure 7. The upper unit of RGCS experienced
            with age hardening principles.  Figure  3A illustrates the   the most significant compression deformation. Conversely,
            precipitation of the NiTi  phase in the matrix after aging   the strain at the five extraction points of SGCS exhibited
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            heat  treatment,  impeding  dislocation  movement  within   a synchronous upward trend within  20 s  in  Figure  8,
            the alloy and thereby enhancing both yield strength and   indicating that the overall structure underwent rapid,
            compressive strength. Furthermore, the LPBF process   uniform elastic deformation during the compression
            introduced sample defects such as micropores, with SGCS   process. Twenty seconds later, the rate of strain increased
            exhibiting greater sensitivity to defects compared to RGCS,   more rapidly at points P2, P3, and P4 in the middle
            leading to faster progression to the compression fracture   compared to the other points, except for SGCS-A8.
            stage. This study demonstrates enhanced plasticity for   Figures  9  and  10 display the strain contours of the two
            RGSC after aging heat treatment while maintaining nearly   structures analyzed using DIC. The compressive shear
            unchanged strength.                                failure of RGCS was attributed to the significant stress near
                                                               the diagonal of the structure. Zhang  discovered that the
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              The compressive elastic modulus is depicted in Figure 6C.   initial fracture of the uniform gyroid rod structure occurred
            The elastic modulus of RGCS-A0 was 564.89 MPa, while   on the diagonal rod at the corner with higher stress and
            that of SGCS-A0 was 1011.74 MPa. Compared with the   strain levels. The first fractures occurred at the bottom
            untreated samples, the elastic modulus of RGCS decreased,   of the cell and then extended to the upper layer. Most
            whereas that of SGCS increased after aging heat treatment.   fractures were observed on the diagonal rod, while very few
            At 2 h of aging, the minimum elastic modulus recorded for   occurred on the horizontal rod. Chen  discovered that the
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            RGCS-A2 was 361.52 MPa, whereas the maximum elastic   homogeneous gyroid structure developed a 45° shear band
            modulus observed for SGCS-A2 was 1262.82 MPa.
                                                               along the cube diagonal and fractured due to the localized
              Figure  6D illustrates the compressive strength. Both   shear stress aligned with the loading direction at a 45° angle.
            RGCS and SGCS demonstrated higher compressive      The text explained that the uniform gyroid structure was
            strength after aging heat treatment compared to the   prone to failure when diagonal yield deformation occurred.
            untreated samples. The maximum compressive strength of   However, the angle of the fracture zone of RGCS was slightly
            SGCS-A4 reached 69.48 MPa, marking a 61.39% increase   larger than 45°, and the position showed an offset near the
            over the compressive strength of SGCS-A0. Conversely,   diagonal.  The  RGCS-A2  and  RGCS-A6  displayed  a  45°


            Volume 3 Issue 2 (2024)                         10                             doi: 10.36922/msam.3137
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