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Zhang, et al.
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           Figure 27. (A) Schematic of successive series of cyclic loadings. (B) “n” can be sub-sectioned into three parts. The actual temperature that
           includes actual fluctuations in parts I and II is shown by , while the mean temperature with no fluctuation in parts I and II is shown by  [123]
           (Reprinted from International Journal of Mechanical Sciences, 185, P. Bayati, A. Jahadakbar, M. Barati, et al., toward low and high cycle
           fatigue behavior of SLM-fabricated NiTi: Considering the effect of build orientation and employing a self-heating approach, 105878,
           Copyright (2020), with permission from Elsevier).

           unit cells (octahedron, cellular gyroid, and sheet   A              B              C
           gyroid). The CAD images and their products are shown
           in  Figure  28. It seems that under the same volume
           fraction, compared with the traditional octahedral unit
           cell structure, triple periodic minimal surfaces (TPMS)
           show excellent static mechanical properties and fatigue
           life, and the lamellar cyclotron structure shows the
           highest fatigue life. Both  TPMS have continuously
           varying curvatures, minimizing staircase effect, and
           reducing crack initiation. Simultaneously, the residual
           particles on the downward-facing surface act as stress
           concentrators, allowing cracks to initiate [127] . For the
           octahedral unit cell, the surface area in contact with the
           powder bed during processing is the largest and more
           residual particles are attached. The spiral design consists
           of thicker struts at the same volume fraction, resulting
           in a lower surface area. Based on the above factors,   Figure  28. (A) Octahedron.  (B) Cellular  gyroid. (C) Sheet
           the  TPMS structure performs better in the practical   gyroid [126]  (Reprinted from Journal of the Mechanical Behavior of
           application of SLM-NiTi.                            Biomedical Materials, 70, M. Speirs, H. B. Van, H. J. Van, et al.,
                                                               fatigue behavior of NiTi shape memory alloy scaffolds produced
           4.5. Damping properties                             by SLM, a unit cell design comparison, 53–59, Copyright (2017),
                                                               with permission from Elsevier).
           The damping capacity is the ability to eliminate sudden
           shocks and oscillations [128] . It is a very critical feature in
           various applications, including biomedical  equipment   the  internal  friction  (tan  δ)  measured  at  an  oscillation
           (such as dental and spinal implants) and the automotive   frequency of 1 Hz (a) and the temperature dependence of
           industry (dampers) . Wang  et  al.  used two sets of   tan δ and Young’s modulus at an oscillation frequency of
                                         [9]
                           [6]
           SLM parameters  to  generate layered  NiTi  samples,   90 kHz (b), indicating that even without the influence of
           in  which  alternate  layers  have  different  Ni/Ti  ratios,   transient effects, the layered structure samples also exhibit
           so they have different transformation temperatures,   good damping  characteristics.  Table  2 summarizes  the
           which lead to austenite/martensite  alternating  structure   recent researches related to the mechanical properties of
           in  a  specific  temperature  range.  During  the  cooling   SLM-NiTi.
           process in a wide temperature range (~130 K), austenite   After  design,  AM,  surface  modification [66,129] ,
           gradually  transforms into martensite,  thereby obtaining   drug loading [130] , and a series of characterizations of
           better  damping performance  at both low (1 Hz) and   AM-NiTi implants are required, which are summarized
           high (90 kHz) oscillation frequencies. Figure 29 shows   in Figure 30.

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