Page 299 - IJB-9-4
P. 299

International Journal of Bioprinting              Design and biomechanical analysis of porous tantalum prostheses



            Table 1. Pore structure information and compressive mechanical properties of standard porous tantalum cylinders
             Sample          Wire diameter   Pore diameter    Porosities            Mechanical properties (MPa)
                             (μm)            (μm)             (%)             Young’s modulus   Yield strength
             300/1200        300             1200             93.71            1302.83 ± 76.96   23.25 ± 0.06
             450/900         450               900            82.37            4998.09 ± 69.74   106.36 ± 0.17
             450/1200        450             1200             88.11            2968.83 ± 31.76   76.19 ± 0.65
             450/1500        450             1500             91.60            2907.64 ± 14.04   49.14 ± 0.64
             600/900         600               900            76.46            5719.32 ± 100.61  172.71 ± 1.67
             600/1200        600             1200             83.32            4660.56 ± 187.07  109.19 ± 1.40
             600/1500        600             1500             87.24            3743.04 ± 36.77   78.45 ± 1.01

            arthroplasty, severe pain forced him to receive a revision   2.3.2. Boundary conditions
            surgery. The CT imaging data of the patient were collected   A general analysis of static mechanics with binding contact
            and provided by Southwest Hospital of Army  Medical   between the tantalum prosthesis and the tibia was used.
            University. Specifically, the two-dimensional image data   In this case, the lower end of the tibia was fixed in all
            of the full length of the patient’s lower extremities, i.e.,   direction, while the load was uniformly distributed over
            from the pelvic position to below the ankle position,   the tibia plateau at the upper end of the prosthesis. Based
            were collected using a spiral CT machine (Siemens Inc,   on the patient’s weight (71 kg), a uniform force of F1 =
            Germany) with a scanning angle of 360° at the Southwest   350 N was applied to the upper end of the prosthesis to
            Hospital of Army Medical University. The scan layer   simulate the normal standing posture on two legs, and
            thickness and kilovoltage peak (kVp) were set as 1.5 mm   a uniform force of F2 = 700 N was applied to simulate
            and 140 kV, respectively. Medical image processing   the patient’s standing posture on single leg and climbing
            software  Mimics  20.0  (Materialise  NV, Belgium)  and   stairs postures. The boundary conditions for the FE model
            Geomagic Studio 2013 (Geomagic Inc, USA) were utilized   considering both the load and the restriction of movement
            to reconstruct the patient’s 3D tibia bone model. Based   are illustrated in Figure 1d.
            on  the  constructed  tibia  bone  model,  a  patient-specific
            prosthesis geometrically matching the bone defect site in   2.3.3. Maximum strain calculation
            the tibia was designed by using CAD design software NX   The maximum strain  (ε) of  the tibia was  employed to
            12.0 (Siemens PLM, USA).                           indicate the biomechanical response of the tibia. The ε was
                                                               calculated using ε = σ/E, where σ is the von Mises stress of
            2.3. Finite element simulation                     bone tissue adjacent to the prosthesis and E is the Young’s
            The finite element models of the prosthesis and tibia   modulus of bone tissue.
            were constructed and simulated using finite element
            simulation software ABAQUS 6.12 (SIMULIA, USA). Ten-  3. Results
            node secondary tetrahedral element (C3D10) was used   3.1. Mechanical test
            in this study. Before presenting the results, a mesh study   Figure 2 shows the fabricated standard cylinders of porous
            was conducted to solve the mesh dependence problem.   tantalum  and  their  typical  compression  stress–strain
            Four mesh sizes of the tibia were employed to compare   curves. The initial nonlinear phase of the stress–strain
            the stress situation. The mesh size resulting in minimum   curve should be a result of some small uneven struts
            computational time was regarded as appropriate.    yielding locally [33-35] . The Young’s modulus was represented
                                                               by the slope of the linear range of the curves. The yield
            2.3.1. Material properties                         strength was defined as the stress at 0.2% offset strain since
            The material property of the porous tantalum prosthesis   the yield points were not clear . The Young’s modulus and
                                                                                      [36]
            was  defined  as  an  isotropic  homogeneous  material.  The   yield strength of the samples are summarized in Table 1.
            Young’s modulus of the prosthesis was assigned according
            to the equivalent Young’s modulus of tantalum samples   The  pore  size  and  wire  diameter  were  observed
            obtained from uniaxial tests in section 2.1. Poisson’s   to significantly influence the mechanical properties
            ratio was 0.3. The material property of the patient’s tibia,   of the 3D-printed porous tantalum. Specifically, for a
            according to previous reports [31,32] , was assigned as cortical   predetermined pore size, both the Young’s modulus and yield
            bone with an elastic modulus of 20,000 MPa and Poisson’s   strength increased with the increasing wire diameter. On
            ratio of 0.3.                                      the other hand, for a predetermined wire diameter, both the


            Volume 9 Issue 4 (2023)                        291                         https://doi.org/10.18063/ijb.735
   294   295   296   297   298   299   300   301   302   303   304