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International Journal of Bioprinting                                   3D-printed post-otoplasty ear retainer




            loading-unloading method. Test samples were initially   and sharp edges.  The final assembled model, including
            stretched from no stress to 20% strain and then unloaded   the retainer and positioning cover, was completed to
            back to no stress, the cycle of which was repeated five   generate a geometric solid STP (Standard for the Exchange
            times. This procedure was then applied to 40% strain   of Product Dat) STP model of the retainer. The STP
            levels, repeated for five cycles, and subsequently extended   file was subsequently imported into HyperMesh 14.0
            to 60% and 100% strain levels. A 60% strain condition is   software (Altair Company, USA) for mesh partitioning,
            acceptable for the part and was selected for stabilization.   and subsequently exported as a  BDF (Boundary Data
            For each experiment, the fifth loading up to 60% strain was   Format) file for finite element pre-processing using MSC.
            isolated from the broader data set, reset to zero stress and   Patran2019 software (MSC Software Corporation, USA)
            strain, and then utilized as a set of experiments to establish   and finite element post-processing using MSC Nastran
            a material model.                                  2019 software (MSC Software Corporation, USA).
               The volumetric compression test was performed using   The skull, 3D-printed shell, and internal cartilage of the
            cylindrical samples with a height of 2 mm and a diameter   ear are treated as isotropic, homogeneous, and continuously
            of 5 mm; a compression rate of 10 mm/min was used with   linear elastic materials. The facial skin, muscle, and soft
            indenters to compress the specimens. In their undeformed   tissue layers, as well as the soft retainer, are modeled as
            state, the nominal stress of the samples was calculated by   hyperelastic materials capable of large deformations and
            dividing the applied force by the cross-sectional area.   non-linear behavior. 18–20  The properties of the retainer are
                                                               determined through experimental measurements involving
               To evaluate the decrease of stress over time, a stress-
            relaxation test  was  performed. The  stress  relaxation   planar tension, equibiaxial extension, and uniaxial tensile
                                                               tests. Table 1 summarizes the properties used in FEA.
            properties of a material cause the force acting on it to
            gradually weaken during use. The retention rate of stress   The boundary conditions for the finite element model
            directly reflects the material’s corrective efficiency, making   of the ear mold retainer are assumed as follows: a fixed
            stress relaxation tests crucial. Stress relaxation tests were   constraint is applied to the nodes on the lower surface of
            conducted using the ELF 3100 equipment at two strains in   the model base, restricting movement in all six degrees of
            a 37°C water bath: 5% and 20% strains. Each test involved   freedom; a pressure of 14 N was applied vertically to the
            a three-part process: initially stretching the specimen by   outer surface of the hard shell using multi-point constraint
            1.25 mm over 15 s (equivalent to a tensile velocity of 5 mm/  (MPC) technology to simulate the pressure exerted on
            min and a total strain of approximately 5%); 5 s system   the ear structure when wearing the ear mold retainer.
            stabilization and 3 h stretching at 5% strain for observing   This setup allows for further observation of the impact
            stress relaxation. For each material, three replicates were   of wearing the ear mold retainer on the biomechanical
            tested in both conditions. Stress values  were recorded   properties of the human ear. The constrained boundaries
            every 0.02 s. To reduce variations within the samples,   are illustrated in Figure S1, Supporting Information.
            stress relaxation curves were plotted using the percentile
            of residual stress.                                2.6. Clinical assessments
                                                               We conducted a clinical validation to investigate the
            2.5. Finite element analysis                       feasibility of long-term retainer wear in 20 healthy patients.
            The structural characteristics were determined by   The patients were required to wear the retainers for 8 h
            mechanical testing of the BioMed Flex 80A Resin, and   per day for a week, and their satisfaction with the retainer
            these properties were then applied to the structure. Briefly,   was evaluated using the Chinese version of the Quebec
            the model was refined to remove any inconsistencies or   Auxiliary Technology User Satisfaction Assessment
            features that STP (Standard for the Exchange of Product   Scale (C-QUEST 2.0). 21,22  C-QUEST 2.0 encompasses
            Dat) could lead to computational errors, such as small fillets   12 subscales rated on a scale from 1 to 5, where higher

            Table 1. Material properties used in finite element analysis.

             Tissue/structure                          Model              Elastic modulus (MPa)  Poisson’s ratio
             Auricular cartilage                      Liner elastic              9                  0.32
             3D-printed positioning cover             Liner elastic             3500                0.30
             Soft-gel retainer                    Non-liner hyperelastic        Based on the mechanical tests
                                              Hyperelastic (Mooney-Rivlin: C10 =
             Facial skin, muscle, and soft tissue                                0.7                0.45
                                              0.00165; C01 = 0.00335; D1 = 3.653)

            Volume 10 Issue 5 (2024)                       466                                doi: 10.36922/ijb.3986
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