Page 271 - Microsensors, MEMS and Smart Devices - Gardner Varadhan and Awadelkarim
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MECHANICAL   SENSORS     251

  transverse  load  shown earlier  (Figure 8.2l(b)).  In this  case,  the  deflection is  not linearly
  related  to the  applied  load  but  a  solution  can be  obtained  from  the  buckling  equation  of
  Euler where
                                                                       (8.24)
                                 dy 2     E mI m

  The  solution for  a bridge  of  length /  fixed  at both  ends is a sinusoidal one where


                            AJC  =  A sin(y/Fy/E mI my)                (8.25)

  where  A is  a constant. The  beam will buckle when the  load  reaches  a critical  value of

                                       2
                                   = 7i E mI m/l 2                     (8.26)
                                F c
  In a similar  manner, analytical equations that relate the static deflection of a microstructure
  of  different  geometry  to  point  and  distributed  loads  and  indeed  rotations  caused  by  an
  applied  moment  or  torque can be found.
     Therefore,  the  important  mechanical  parameters  and  properties  in  the  design  of  static
  microstructures  can be  summarised  as  shown in  Table  8.5.



  8.4.3  Microshuttles and Dynamics

  The  dynamics  of  microstructures  are  also  very  important  for  several  reasons.  First,  the
  dynamic  response of a cantilever beam,  microbridge, or diaphragm  determines the  band-
  width of the microsensor,  that is, the time taken for the structure to respond to the  applied
  static  load  or follow a dynamic load.  Second,  the kinetics  of the  structure can  be used in
  inertial  sensors  to  measure  linear  and  angular  accelerations.  Finally,  there  is  a  class  of
  mechanical  sensors  based  on a microstructure or a microshuttle that is  forced  to  resonate
  at  some  characteristic  frequency.
     In  an  inertial  or resonant  sensor,  the  cantilever  beam  (or bridge)  is redesigned  so that
  the  mass  is  more  localised  and  the  supports  more  convoluted.  Figure  8.22  shows  the
  basic  design  of  an  inertial  or  so-called  microflexural type  of  structure  together  with  its
  equivalent  lumped-system  model.


           Table 8.5  Some  important  mechanical  parameters  and  material properties
           in  defining  the  static deflection  of  microstructures

           Parameters/properties                 Nature
           Point/distributed  force,  torque,  stress, pressure  Load  applied/measurand
           Width, breadth, thickness, length     Size of  structure
           Young's modulus, yield  strength, buckling  Material  properties
             strength, Poisson's ratio,  density
           Spring constant, strain, mass, moment of inertia  Calculable parameters
           Lateral/vertical  deflection,  angular  deflection  Response
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