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0-07-145538-8_CH02_76_08/30/05



                                    Basic Members: Lumped- and Distributed-Parameter Modeling and Design

                              76   Chapter Two
                              axial vibration is determined by means of Eqs. (2.87), (2.88), and (2.98)
                              as
                                                         3w + w 2
                                                           1
                                                 m   =             m                    (2.103)
                                                  a,e   6(w + w )
                                                           1    2
                              Again, Eq. (2.103) reduces to Eq. (2.49) when w 2 ĺ w 1 , as expected,
                              because the trapezoid configuration transforms into a constant rectan-
                              gular cross section to one for this limit condition. The axial vibration
                              resonant frequency is therefore

                                                 2 3       E(w — w )
                                                               2
                                                                    1
                                           Ȧ   =                                        (2.104)
                                            a,e   l   ȡ(3w + w )ln(w 2/  w )
                                                           1
                                                               2
                                                                         1
                                The torsional resonant  frequency is determined similarly with
                              respect to the free end. The torsional stiffness is obtained from the axial
                              one,  according to Eq. (2.85). The inertia fraction  corresponding to
                              torsional  vibrations  is  determined according to Eqs. (2.90), (2.91),
                              (2.92), and (2.98) as
                                                    2
                                              3
                                                                         2
                                                               2
                                                                    3
                                       ȡlt 10w +6w w +3w w + w +5t (3w + w )
                                                                                 2
                                                                             1
                                                    1
                                                       2
                                                            1 2
                                                                   2
                                              1
                                 J t,e  =                   720                         (2.105)
                              When w 2 ĺ w 1 , Eq. (2.105) changes to Eq. (2.55), which defines the
                              torsional moment of inertia for a constant-cross-section microbar. The
                              torsional resonant frequency can be calculated as
                                           4 15t            G(w í w )
                                                                    1
                                                                2
                                     Ȧ   =
                                      t,e    l           3    2          2
                                                   ȡ 10w +6w w +3w w
                                                        1     1  2    1 2               (2.106)
                                                           2
                                                      3
                                                   +w +5t (3w + w ) ln(w  2/  w )
                                                      2        1    2         1
                                Another trapezoid microcantilever is sketched in Fig. 2.26a and b
                              where the width w is constant and the thickness varies linearly from
                              t  at the free end to t  at the fixed root.
                               1
                                                 2
                                The axial stiffness of this microcantilever is
                                                        Ew(t — t )
                                                                 1
                                                             2
                                                  k a,e  =                              (2.107)
                                                         l ln(t 2/ 1
                                                               t )
                              When t 2 ĺ t 1 , Eq. (2.107) reduces to Eq. (2.45), which gives the axial
                              stiffness of a constant rectangular cross-section microcantilever.
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