Page 230 - Mechanical design of microresonators _ modeling and applications
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                                                 Resonant Micromechanical Systems

                                                             Resonant Micromechanical Systems  229
                                Two paddle microcantilevers that were introduced in Chap. 3 are
                              analyzed next by comparing the free bending and torsional responses
                              provided by the three models. It should be mentioned that model III,
                              the fully compliant, full-inertia model, was derived also in Chap. 3, and
                              therefore only models I and II are formulated here.

                              Paddle microcantilever of  constant thickness. The paddle microcan-
                              tilever whose top view is shown in Fig. 3.8 and which is defined by two
                              segments of constant thickness, and different widths and lengths, is
                              studied now.
                              Model I.  According to model I of Fig. 5.2, the wider segment which is
                              located at the free end in Fig. 3.8 is considered rigid whereas the root
                              segment is the one providing compliance to the system. Likewise, the
                              inertia contribution of only the free-end segment is taken into account.
                                The lumped-parameter bending stiffness comes from only the root
                              segment and is
                                                             Ew t 3
                                                        I       2
                                                       k  =                               (5.1)
                                                        b,e     3
                                                              4l 2
                              The mass of the free-end segment that corresponds to out-of-the-plane
                              bending is

                                                       I
                                                     m b,e  = ȡl w t                      (5.2)
                                                            1 1
                              and therefore the lumped-parameter bending  resonant frequency
                              yielded by model I becomes

                                                       I
                                                     k b,e   t    Ew 2
                                              Ȧ I  =      =                               (5.3)
                                               b,e     I    2l   ȡl l w
                                                     m b,e    2    1 2 1
                                Similarly, the torsional stiffness of the root segment is identical to
                              that of the whole microcantilever, and therefore
                                                          Gw t 3
                                                             2
                                                     k  I  =                              (5.4)
                                                      t,e   3l
                                                              2
                              The torsional mechanical moment of inertia produced by the free-end
                              segment is

                                                               2
                                                                   2
                                                       ȡl w t(w + t )
                                                  I
                                                               1
                                                        1 1
                                                 J t,e  =   12                            (5.5)

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