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                                   Microhinges and Microcantilevers: Lumped-Parameter Modeling and Design

                              132   Chapter Three
                              For a ĺ 0, Eq. (3.73) simplifies to Eq. (2.55), which is the effective tor-
                              sional mechanical moment of inertia of a constant-cross-section mem-
                              ber, whereas for  a ĺ R and  b ĺ R, the long, elliptically  filleted
                              cantilever  becomes  a circularly filleted one, and  indeed, Eq. (3.73)
                              changes to Eq. (3.63), as it should. The lumped-parameter torsional
                              resonant frequency is found by combining the corresponding stiffness
                              and inertia fractions, and its equation is
                                                          3
                                                                   2
                                                      /
                                                 (G / ȡ) {a b 0.832b +4.56bRw 1
                                        21.91lt
                                                 +4.381(3w + t ) +40w l (w + t )}
                                                                        3
                                                                            2
                                                           2
                                                                               2
                                                              2
                                  Ȧ   =                   1            1   1             (3.74)
                                   t,e
                                                /
                                          (l í a) w + a (2b + w )
                                                  1
                                                              1
                                          /  w (4b + w ) arctan 1+4b w íʌ 4 b
                                                                             / /
                                                                     /
                                              1
                                                                        1
                                                     1
                                The bending stiffness for a long, elliptically filleted cantilever is found
                              by means of the series connection rule of Eq. (3.22) as
                                                            Et 3
                                 k  =
                                  b,e
                                                            2
                                       4(l í a) 3 /  w +3a(l í a) 4(2b + w )
                                                                      1
                                                  1
                                                                  3
                                        /  w (4b + w ) í ʌ b +0.75a 14.283b 2
                                                         /
                                                   1
                                           1
                                                                                         (3.75)
                                                          2
                                       +16.566bw +3.14w
                                                  1       1
                                                                            /
                                       í4(2b + w ) w (4b + w ) arctan 1+4b w  1 /  b 3
                                                            1
                                                     1
                                                1
                                           2                                   2
                                                                   /
                                       +6a (l í a) (2b + w ) ln(1+2b w ) í 2b  / b
                                                                     1
                                                         1
                              When any of the two segments composing the elliptically filleted mi-
                              crocantilever of Fig. 3.19 is relatively short, and shearing effects need
                              be taken into account, the shearing-affected compliances have to be
                              used in formulating the corresponding bending stiffness. The effective
                              inertia fraction associated with the free bending vibrations is
                                                                           2
                                                       2
                                                                              5
                                           ȡt (1208.75l í 498.31la + 54.959a )a b
                                                       7
                                              + 12,672l w                                (3.76)
                                                         1
                                    m   =
                                      b,e                        6
                                                          53,760l
                              Again, when shearing effects are important, the shearing-affected dis-
                              tribution function has to be utilized, instead of the normal one, and an
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