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                                   Microhinges and Microcantilevers: Lumped-Parameter Modeling and Design

                              112   Chapter Three
                                                              z




                                      3          2         1
                              x


                                           1 2        1 1
                              Figure 3.6 Two-segment microcantilever.

                              calculated in generic form with respect to the free end 1. The assump-
                              tion is applied here that both segments have variable widths w  and
                                                                                          1
                              w  but constant thicknesses t  and t .
                                                               2
                               2
                                                         1
                                The axial stiffness is
                                                             1
                                                   k   =
                                                    a,e   (1)   (2)                      (3.15)
                                                         C a  + C a
                                      (1)
                                              (2)
                              where  C a  and  C a  are  the axial compliances  of the two segments:
                              (1) denotes the 1-2 portion and (2) denotes the 2-3  portion in the
                                                                                 (1)
                              schematic representation of Fig. 3.6. The compliance C a  is calculated
                                                             (2)
                              with respect to point 1 whereas C a  is determined with respect to point
                              2. The  local frames of the two segments composing the member of
                              Fig.  3.6 are  placed at points 1 and  2, respectively.  Equation (3.15)
                              reduces to Eq. (2.45) when l  = l  = l/2, w  = w  (constant), and t  = t ,
                                                                                         1
                                                        1
                                                                    2
                                                                                             2
                                                                         1
                                                            2
                              which proves the validity of the former equation.
                                The lumped-parameter effective inertia fraction corresponding to the
                              free axial vibrations is expressed as
                                           l 1                    l + l 2
                                                                  1
                                                                                  2
                               m a,e  = ȡ t 1ฒ  w (x) f a (1) (x)  2  dx + t 2ฒ  w (x) f a (2) (x) dx  (3.16)
                                                                       2
                                             1
                                          0                      l
                                                                 1
                                                               (2)
                                                        (1)
                              The distribution functions  f a  and  f a  are assumed to be different for
                              the two segments. When l 1  = l 2  = l/2, w 2  = w 1  (constant), and t 1  = t 2 ,
                              Eq. (3.16) simplifies to Eq. (2.49), which characterizes a constant-cross-
                              section microcantilever. The axially related resonant frequency can be
                              calculated by means of Eqs. (3.15) and (3.16) and the definition Eq. (2.1).
                                The  torsional  stiffness  formally  resembles the axial one and is
                              expressed as


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