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     Zolfagharian, et al.
           density ρ  appropriate sensitivities for a particular   properties [25,27] ,  and  inserting  Equation  (13)  in
                   e
           element can calculated as follows [27,29,30] :      Equation (12), the sensitivity could be determined:
            obj ,e    1  (    e T   K u  T  u   u  e   u  u K  K  u e   )   Obj ,e  1  p  1 −  T  ,   (14)
                                                  T
                                                                                       ) 
                                                                                               e
                                                                                       1
             e    2V   e   e e   e  ∂  e  e  e  e   e        e  =  −  2V e  (E −  2  E p  e  uK u
                                                                                                  0,ee
                      e
                                                        (5)
             Applying the system equation Ku = f to a single   2.2 Sensitivity filtering
           element considering the design variable yields the    The  checkerboard  structure  issue  caused  by
           following partial differential form:                direct use of the selected sensitivities was sorted
                       e  + K  u  K e  u  =    f e    (  6)  out  using  higher  order  elements,  despite  longer
                    e   e   e  e   e                     calculation time. Sensitivity filtering is utilized by
             Since the external load does not depend on the    applying  an  increased  limit  to  the  checkerboard
           density values, Equation (6) yields:                structure  and  smoother  contours,  as  shown  in
                                                               Figure  2 .  Using  this  approach  resulted  in
                                                                        [26]
                  ∂K          ∂u
                     e  u + K    e  = 0                 (7)    poorly defined contours instead of checkerboard
                  ∂ρ e  e    e  ∂ρ e                           patterns. Digital pixel structures are adapted to the
             Accordingly, Equation (7) can be rearranged to:   finite element mesh to allow the image processing
                                                                                                             .
                                                               results to be directly applied to TO problem
                                                                                                        [31,32]
                               K
                  K e  ∂ u e  =− ∂ ∂ρ  e  u             (8)    in Figure 3, the SIMP method was implemented
                                                                 As  shown  in  the  flowchart  of  TO  algorithm
                                   e
                     ∂ρ
                        e
                                e
             Transposing Equation (8) leads to:                to  solve  the  optimization,  in  which  design
                     ∂ u  T    ∂ K     T                   variables  are  defined  based  on  the  densities  of
                   K e  ∂ρ    =−  ∂ρ  e  u e       (9)    the  discretized  elements [33-35] .  The  mechanical
                         e
                               
                  
                               
                                                               loadings  and  constraints  of  the  optimization
                         e
                                     e
                                                               problem  were  modeled  through  loading  and
             Using the symmetric stiffness matrix, Equation    boundary  conditions,  as  shown  in  Figure  l.
           (9) can be expressed as follows:                    The  aim  is  to  maximize  the  deflection  of  the
                                                               actuator  by  optimization  of  the  configuration  of
                  ∂u T e  K =−�  u T  ∂K e             (10)    the  printed  layers.  The  optimization  problem  is
                  ∂ρ e  e     e  ∂ρ e                          solved iteratively by incorporating the sensitivity
             Inserting Equations (10) and (9) into Equation    guidance. Subsequently, a volume constraint is set
           (5), the strain energy density sensitivity becomes:  to minimize the structural stiffness of the actuator
                                                                                                         [36]
           ∂Π        1      ∂K           ∂K          ∂K        and ensure the convergence of the algorithm . In
              obj e,  =  (−u T  e  u  + u T ∂  e  u  − u T  e  u  )    addition, a standard method of moving asymptotes
            ∂ρ e    2 V e  e  ∂ρ e  e  e  ∂ ρ e  e  e  ∂ρ e  e  was  employed  for  each  material  density  to
                                                       (11)    conform to the volume constraint imposed into the
             which simplifies to:                              optimization.
                  Π          1    ∂K
                    Obje,  =−   u T   e  u  .          (12)
                   ∂ρ e     2 V e  e  ∂ρ e  e
             Differentiation  of  the  material  law,  Equation
           (2) results in:
                  ∂K e  =  K ( E − )     p−1           (13)
                                   Epρ
                  ∂ρ e     0, e  2  1    e
             Having  obtained  u by  solving  the  system  of   Figure  2.  Schematics  of  two-material  topology
                                e
           equations with a distributed density and material   optimization filtering.
                                       International Journal of Bioprinting (2020)–Volume 6, Issue 2        53
     	
