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3. Microsuspensions                                               149








         The out-of-the-plane definition stiffness is found by applying a  force   at the
         free point of the spring in Fig. 3.16, perpendicularly to the plane of the figure.
         This stiffness is the ratio of the applied force and the resulting deflection to its
         equation is:








         2.3.3   U-spring with Filleted Corners (Configuration # 3)


             Configuration # 3  is sketched in Fig.  3.17 where the middle segment is
         composed of two quarter-circles encompassing  a  straight  line such  that overall,
         this spring configuration is made up of five segments.





















                      Figure 3.17 U-spring design with circularly-filleted corners

             For a thin configuration where the radius-to-width ratio R/w is larger than
          10, and  in the case  where all  segments have the  same constant cross-section,
          the in-plane compliances can be determined by  following the procedure that
          has been used for the other U-spring configurations. Their expressions are:
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