Page 111 - Mechanical design of microresonators _ modeling and applications
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                                   Microhinges and Microcantilevers: Lumped-Parameter Modeling and Design

                              110   Chapter Three

                                                       12l ln(w 2/  1
                                                                w )
                                                  C =                                      (3.6)
                                                   r
                                                          3
                                                       Et (w í w )
                                                             2   1
                                By applying now Eqs. (3.2), the compliances of the microcantilever shown in
                                Fig. 3.4b are obtained (when the fixed and free ends interchange and the
                                compliances are determined with respect to the new free end) as
                                            3                       2
                                                                            w )
                                          6l  (w í w )(w í 3w ) +2w ln(w  2/  1
                                                        1
                                                     1
                                                2
                                                              2
                                                                    2
                                       Ҡ
                                     C =                                                   (3.7)
                                       l                 3        3
                                                       Et (w í w )
                                                            2
                                                                 1
                                                   2
                                                12l w í w + w ln(w    w )
                                            Ҡ         1   2    2    2/  1
                                           C =                                             (3.8)
                                            c
                                                         3
                                                       Et (w í w ) 2
                                                            2    1
                                Equations (3.7) and (3.8) are also obtained when one is directly calculating
                                                ƍ
                                                       ƍ
                                the compliances C l   and C c  by applying the definition equations of linear
                                direct and cross  compliances of Chap. 2 and  by starting  the  required
                                integrations from the thicker end (assumed free).
                              3.2.2  Compliances in arbitrarily translated
                              reference frames
                              At times, integrals that are of the form pertaining to the axial, torsion,
                              and bending compliances need to be calculated with respect to reference
                              frames that are translated at a specific distance from one end of the
                              member. These  compliances, as shown in  the following, can  be ex-
                              pressed in terms of the normally defined compliances. Figure 3.5 shows
                              a generic microcantilever whose compliances, evaluated with respect to
                              a translated frame x 1 O 1 y 1 , need to be expressed in terms of the compli-
                              ances calculated with respect to the reference frame xOy.
                                The relationships between the two coordinates as well as between
                              their corresponding differentials are
                                                 x = a + x 1   dx = dx 1                  (3.9)
                              It can be shown that the bending-related compliances calculated with re-
                              spect to the translated frame x 1 O 1 y 1  can be expressed in terms of the nor-
                              mal ones that are formulated in the endpoint reference frame xOy as
                                                                       ҡ
                                                            ҡ
                                     ҡ
                                                    2
                                   C = C +2aC + a C        C = C      C = C + aC         (3.10)
                                     l   l      c     r     r    r     c    c    r




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