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                                   Microhinges and Microcantilevers: Lumped-Parameter Modeling and Design

                               Microhinges and Microcantilevers: Lumped-Parameter Modeling and Design  135
                              studied in Chap. 2, it is possible to determine its axial, torsional, and
                              bending resonant frequencies by applying the algorithms developed for
                              two-segment configurations. It can be shown that the axial stiffness
                                                                       4
                              (the axial compliance  is given in Lobontiu,  for instance), which is
                              connected to the free end 1 being derived with respect to the fixed end
                              2 and is found by using the series connection Eq. (3.22), is
                                                            Et
                                k a,e  =                                                 (3.78)
                                                                                  /
                                               1 /
                                                                           /
                                      2 (2R + w )  w (R + w ) arctan 1+4R w íʌ 4
                                                           1
                                                    1
                                                                             1
                              The effective axial mass is
                                             m a,e  = ȡtR(0.352R +0.667w )               (3.79)
                                                                       1
                              The corresponding axial resonant frequency is
                                              0.707 E /  ȡR(0.352R +0.667w )
                                                                           1
                                  Ȧ   =                                                  (3.80)
                                   a,e
                                                                             1 /
                                                1 /
                                         (2R + w )  w (R + w ) arctan 1+4R/w í ʌ 4
                                                            1
                                                      1
                                The torsional stiffness is calculated by means of Eq. (3.20) in terms
                              of the axial stiffness expressed in Eq. (3.78). The effective  torsional
                              mechanical moment of inertia is
                                                            ȡtR
                                   J t,e  =
                                                   3
                                                                                2
                                                             2
                                                                            2
                                         12 0.403R +1.019R w +0.667w (w + t )            (3.81)
                                                               1
                                                                            1
                                                                         1
                                                         2
                                                     2
                                         +0.352R(3w + t )
                                                     1
                              The torsion-related resonant frequency is
                                               /
                                              G {ȡR (2R + w )
                                                           1
                                      1.414t
                                              /  w (R + w ) arctan  1+4R w íʌ 4 }
                                                                                 /
                                                                         /
                                                                            1
                                                  1
                                                        1
                                Ȧ   =                                                    (3.82)
                                 t,e
                                                            2
                                                                               2
                                                                           2
                                                  3
                                            0.403R +1.019R w +0.667w (w + t )
                                                                           1
                                                              1
                                                                        1
                                                       2
                                                           2
                                            +0.352R(3w + t )
                                                       1
                                The direct linear (out-of-the-plane) bending stiffness of a long (Euler-
                              Bernoulli) configuration is
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