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                                          Microbridges: Lumped-Parameter Modeling and Design

                              192   Chapter Four
                              component, namely, the second (left) segment, if the reference frame
                              origin is chosen at the right fixed end, as shown in Fig. 4.15. A similar
                              approach was taken, as already mentioned, in analyzing two-segment
                              microhinges in Chap. 3, where only the properties of one basic segment
                              of the two were utilized. The subscripts (2) and (1) have been employed
                              to  denote  the left and the right segments, respectively. To simplify
                              notation, no subscript is used here, but all compliances, for instance,
                              are those of the second mirrored  segment of Fig. 4.15, taken  with
                              respect to point 2 (which is assumed free) when point 3 is fixed. In the
                              end,  the generic formulation produces the bending  and  torsional
                              resonant frequencies that are associated with the midpoint (point 2) of
                              the two-segment microbridge of Fig. 4.15.
                              Bending resonant frequency. The lumped-parameter bending-related stiff-
                              ness and effective mass  are determined  here  for the entire flexible
                              structure of Fig. 4.15. To express the lumped-parameter stiffness at
                              point 2, which is the ratio of a force applied at that point about the z
                              direction to the resulting out-of-the-plane deflection, the following two
                              steps have to be undertaken:

                              ●  Calculation of the force and moment reactions at fixed point 1 when
                               a force is applied about the z axis at midpoint 2 in terms of that force
                               by using compliances
                              ●  Calculation of the deflection produced at midpoint 2 under the action
                               of the force applied at that point
                              Both  steps need to  utilize  the compliance transforms presented  in
                              Chap. 3 which enable us to express compliances in terms of switched
                              and arbitrarily translated reference frames.
                                The lumped-parameter bending stiffness that is associated with
                              midpoint 2 can be expressed as

                                                               1
                                   k b,e  =                                              (4.88)
                                         1+2(c í 1)c C + (c í c l /2) 2C + (2c í c l)C
                                               1     1  l   2   1       c    2   1   r
                              The constants c  and c  which enter Eq. (4.88) are
                                                   2
                                            1
                                            a b + a b              a b + a b
                                             12 1
                                                                            12 2
                                                                     22 1
                                                    11 2
                                        c =                    c =                       (4.89)
                                         1
                                                                2
                                                      2
                                             a a   í a 12           a a   í a 2
                                                                             12
                                                                     11 22
                                              11 22
                                               ʾ    ʿ         ʾ  ʿ         ʾ   ʿ
                              where      a  = C + C    a  = C + C    a  = C + C          (4.90)
                                          11   r   r    12   c   c    22   l   l
                                                   l     ʿ       íl    ʿ
                              and            b =      í C   b =      + C
                                              1     ʿ    c   2     ʿ   l                 (4.91)
                                                 2C r            2C c
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