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3. Microsuspensions                                               143




























            Figure 3.11  U-spring  model with boundary conditions, main degrees of freedom, and
                                     corresponding forces

             As a  result  of  these three  translatory motions of the  shuttle,  the  true
          boundary condition at point 1  in Fig. 3.11 is a forced translation about the x-
          axis. However, as a simplification to the real situation, it may be considered
          that point 1  is  free to move, as  also assumed previously with the bent beam
          microsuspension. Because the force acting at that point is  basically directed
          about the same direction, the errors of considering point 1 as free are expected
          to be small. Three different configurations will be analyzed in the following:
          one with sharp  corners, a  second one where  the short  straight  link of the
          model is substituted by half a circle, and a third variant with filleted corners.

          2.3.1  U-spring with Sharp Corners (Configuration # 1)

             Configuration #  1  is formed of three elastic segments, as  shown in Fig.
          3.12. In order to keep the formulation valid for a generic case, they can have
          different but  constant cross-sections. It  will  also be  considered  that  only
          bending of each of the three segments contribute to the total  strain energy of
          the spring. The in-plane compliances are calculated by applying the loads
              and      as shown  in  Fig.  3.12, and by  calculating the corresponding
          displacements        and    Castigliano’s displacement theorem  is  applied
          again in order to  calculate these displacements.  A compliance  matrix of the
          type shown in Eq. (3.19) can be formulated, whose terms are:
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