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International Journal of Bioprinting                                   Horsetail-inspired lattice for bone use




            approximately 30%.  Figure 4 shows the computer-aid   During the  compression testing, graphene lubricant was
            design renders (Figure 4A–C) and the pictures of the   also applied on the platens. The steps for preparation of
            printed samples (Figure 4D–F). Nine samples, three each   the specimens and operation of the machines to attain
            in the [100], [110], and [111] directions, were fabricated   the testing results are compliant with ISO 13314:2011(E)
            for the investigation of isotropy as shown in  Figure 4A    testing standard.
            and  D,  Figure 4B and  E, as well as  Figure 4C and  F,
            respectively. Each sample contains approximately    2.4. Finite element analysis validation of
            4 × 4 × 4 lattice matrices. The samples were fabricated   lattice matrices
            using XDM 250 printer manufactured by Suzhou XDM   We also simulated the compression testing described in
            3D Printing Technology Co., Ltd. The printer utilizes SLM   section 2.3 numerically through FEA. The respective lattice
            methodology with Ti-6Al-4V as build material; the process   matrices were re-created in the FEA solver environment,
            conforms to ASTM F2924. Ti-6Al-4V is an ideal choice   and similarly, the material properties based on Ti-6Al-
            for our study as the use of titanium alloys is widespread   4V were applied. 32,33  Johnson–Cook model specific to Ti-
                                                                     34
            in the medical industry for bone-related application given   6Al-4V  was also used to account for damage evolution
            the good biomedical compatibility.  The build process   and plasticity. The FEA solver was set to explicit mode
                                         31
            was conducted in an argon-filled environment with a laser   of simulation to accurately simulate the large strain
            power of 500 W at a spot size of 70 μm. A layer thickness of   deformation  condition.  Compression  was  achieved  by
            30 μm and a scanning speed of 1300 mm/s were also used.   simulating  strain  application  with  an  invariant  bottom
            Intuitively, lattice matrices in directions other than [100]   plate and the lowering of a top plate in the axis of loading in
            would deviate from 20 × 20 × 20 mm nominal dimension.   a smooth step profile under a quasistatic condition. Quasi-
                                                               static compression is affirmed by ensuring that the kinetic
               The printed samples were released from the print
            bed with vacuum applied to minimize the clogging of the   energy is small (lower, by an order of three magnitude)
                                                               compared to the total energy. The displacement and
            substructure. It is to be noted that the samples were also   reaction force in the direction of loading were tracked,
            subjected to heat treatment for at 800°C for 2 h. Additionally,   with the stresses of the elements within the respective
            the compression faces were polished to be perfectly flat
            and parallel to each other. A comparison between the   lattice matrices. The mesh sizes were controlled to achieve
            specifications of the processed samples to that of the as-  approximately  500,000  to  1,000,000  C3D10M  elements
            designed dimensions and φ of 0.2940 is shown in Table 1.  per  lattice  matrix  for  balance  between  computational
                                                               burden and accuracy of representation. We also simulated
               The samples were subjected to compression along the   the compression with a lattice based on solid BCC struts
            build direction using an Instron 5982 universal testing   of 20 × 20 × 20 mm, with similar ϕ as a comparison to
            machine. A video extensometer was used for measuring   the horsetail-inspired lattice. The material and associated
            the initial strain of approximately 2.5% to accurately   model as well as compression parameters were kept similar
            capture the elastic characteristics of the samples. The use   to the rest of the samples.
            of the video extensometer precludes inaccuracies resulting
            from the machine compliance. Additionally, the samples   3. Results and discussion
            were subjected to a quasi-static strain rate of 0.001 s .
                                                         -1
                                                               3.1. General mechanical performance and
            Table 1. Sample specifications subjected to compression testing  directionality characteristics of RVEs
                                                               Figure 5 shows the directionalities of the elastic moduli of the
                     Overall dimension   Overall dimension     lattices when r and t are varied. From the figure, without the
            Direction  as-designed  as-printed    ϕ as         consideration of other factors, the effects of directionality
                     (mm)          (mm)           printed      and the respective E  , given the corresponding r and
                                   20.22 ×20.22 ×20.35                          relative
                                                  0.3026 ±     t  dimensions, were evaluated preliminarily. It can be
            [100]    20.00×20.00×20.00  20.20 ×20.34 ×20.40
                                                  0.0023       observed that the represented characteristics become more
                                   20.32 ×20.32 ×20.42         spherical in shape as  r increases from 0.75 mm to 1.15
                                   20.14 ×21.50 ×21.50         mm and generally lose the spherical profile as increases
            [110]    20.00×21.21×21.21  20.20 ×21.46 ×21.53  0.3083 ±   further. The spherical representation implies the isotropic
                                                  0.0008
                                   20.32 ×21.23 ×21.58         nature of the RVEs. Correspondingly, with the increase in
                                   21.39 ×25.17 ×23.63         wall thickness, the general E relative  increases. The presence
                                                  0.3093 ±     of a systematic characteristic evolution with the change
            [111]    21.21 ×24.49× 23.09  21.35 ×24.86 ×23.59
                                                  0.0008       in geometrical parameters highlights the mechanical
                                   21.35 ×24.90 ×23.45         tunability potential of the RVEs through the variation of


            Volume 10 Issue 4 (2024)                       193                                doi: 10.36922/ijb.2326
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