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                                          Microbridges: Lumped-Parameter Modeling and Design

                              182   Chapter Four
                                     patch           1p
                                                                   tp


                                         substrate                 11
                                    t1
                                                      l
                              Figure 4.12  Side view of dissimilar-length bimorph microbridge.

                                                 lp/2





                                           l/2
                              Figure 4.13  Half-model of dissimilar-length bimorph microbridge.

                              4.3.2  Multimorph microbridges of
                              dissimilar-length layers
                              A  dissimilar-length bimorph microbridge is shown in side  view  in
                              Fig.  4.12. Constructively,  the  microbridge is similar to the bimorph
                              microcantilever of Fig. 3.35. The particular case is only studied here
                              where the patch layer is positioned symmetrically with respect to the
                              midspan, and therefore l 1 = (l — l p )/2. The bending and torsional reso-
                              nant frequencies are determined for this configuration by again con-
                              sidering a half-length microbridge which is formed of two portions: one
                              of length l 1  at the root and the other of length l p /2 extending from the
                              root region (see Fig. 4.13).
                                In bending, the half-length model is fixed at one end and guided at
                              the opposite one, as shown in Fig. 4.13. The stiffness with respect to the
                              midpoint of Fig. 4.12 – the guided end in Fig. 4.13 – is calculated by
                              applying a force at that point on the half-model and by calculating the
                              corresponding deflection by means of Castigliano’s displacement
                              theorem, for instance. The resulting stiffness is
                                              96E I (EI ) l E I    + (l í l )(EI )
                                                                         p
                                                  1 y1
                                                         y e p 1 y1
                                                                              y e
                                    k  =
                                     b,e     2 2  4             2       2
                                           E I l +2l (l í l )(2l í ll + l )E I (EI )     (4.50)
                                             1 y1 p   p    p        p   p  1 y1   y e
                                                  4
                                          +(l í l ) (EI ) 2
                                                      y e
                                                p
                              In Eq. (4.50) the rigidity (EI y ) e  is calculated according to Eq. (3.148) over
                              the length l p /2 and by incorporating the substrate and patch elastic and
                              geometric properties. Equation (4.50) reduces to

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