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                                                 Resonant Micromechanical Systems

                              246   Chapter Five
                                out-of-the-plane  translation about the  z axis (which is achieved through
                                bending of the root flexible segments about the y axis).
                                  The torsional stiffness is provided by the two root segments and is explic-
                                itly given in Eq. (5.28). The mechanical torsional moment of inertia is pro-
                                duced by only the middle segment. When we consider that this segment is a
                                relatively thin plate, its moment of inertia about its central (symmetry) axis
                                                               3
                                is, as indicated by Beer and Johnston  for instance,
                                                                2
                                                             mw 2
                                                       J   =                              (5.40)
                                                        t,C   12
                                Because of the fact that the bridge system of Fig. 5.20b will rotate about the
                                x axis, the moment of inertia about that axis will be, according to the parallel
                                axes theorem,

                                                        2     2      2
                                                     mw 2  mw 2   mw 2
                                               J   =     +      =                         (5.41)
                                                t,e   12     4      3
                                The torsional resonant frequency of this microbridge becomes

                                                          t    Gw 1
                                                  Ȧ  = 2                                  (5.42)
                                                   t,e   w    ȡl l w
                                                           2   1 2 2
                                By using the nondimensional parameters

                                                       w 2       t
                                                             ƍ
                                                  c  =       c =                          (5.43)
                                                   w   w     t   w
                                                        1         1
                                the following torsional frequency ratio can be formulated:
                                                  Ȧ *
                                                    t,e      2
                                                  Ȧ   =           2                       (5.44)
                                                              ƍ
                                                    t,e  1+ (c c )
                                                              t/ w
                                where Ȧ * t,e  is the torsional resonant frequency  of  the  symmetric paddle
                                microbridge shown in Fig. 4.19. Figure 5.21 is the three-dimensional plot of
                                the resonant frequency ratio expressed in Eq. (5.44). It can be seen that for
                                the selected parameter ranges this frequency ratio remains almost constant
                                and equal to 2, which indicates that the torsional resonant frequency of the
                                symmetric paddle bridge (Fig. 4.19) is twice the frequency of the asymmetric
                                bridge shown in Fig. 5.20a.

                                Example: Study the free response of the four-arm microbridge sketched in
                                Fig. 5.22, and compare it to the resonant behavior of a regular symmetric
                                microbridge such as the one shown in Fig. 4.19. Assume the central segment
                                is rigid and the legs are massless and compliant. Also assume the geometry




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