Page 141 - Microsensors, MEMS and Smart Devices - Gardner Varadhan and Awadelkarim
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ISOTROPIC  AND ORIENTATION-DEPENDENT WET ETCHING


                80                          300


                60 -
                                            200
                40


                20 -


                 0
                  0   200  400  600  800
                    Insertion pressure (kPa)
                          (a)
     Figure  5.4  (a) Damaged area against insertion pressure and (b) tensile strength against area
     damaged  (Han et al. 1992)


     Mechanical  Testing:
                                      2
     Patterned  samples,  nominally (8 x  8) mm ,  were  interlocked  by  applying  a  load  to  the
     upper substrate; the insertion pressure  is monitored by placing the entire assembly on an
     electronic  force  scale.  The bond  strength  of  the  mating  structures  is  then  characterised
     by  direct  measurements  of  the  tensile  load  needed  to  induce  failure.  Bond  strength  is
     determined by applying a tensile load through a pulley and measuring the force necessary
     for  separation.  Separation  of  the  samples  (failure)  is  always accompanied  by  damaged
     areas  only  on  some  regions  of  the  mating surfaces, implying that  the  samples  are only
     interlocked  over  these  damaged  regions.  The  fraction  of  the  damaged  area  is  found  to
     be proportional  to the insertion pressure (Figure 5.4(a)).  Also, the tensile load  necessary
     to  induce  failure  is  proportional  to  the  fraction  of  the  damaged  area  (Figure  5.4(b)).
     Extrapolation  of  the  straight  line  plot  of  the  area  damaged  against  the  tensile  strength
     to  100 percent  interlocking  yields a tensile  strength  of  approximately  1.0 MPa.

     Failure  Analysis:
     The  analysis assumes a simple  cantilever model  as shown in Figure  5.5.
       In  the  figure,  F n  is  the  interaction  force  between  the  tabs  and  /  is  the  length  of  the
     tab. The bending  stress,  a,  is given by
                                        M(x)y
                                 a(x)  =                              (5.2)

     where  x  is  measured  from  the  edge  of  the  tab  that  is  attached  to  the  substrate,  the
                                                                    3
     bending  moment  M(x)  is  given  by  F n(l  -  x)  I z  is the moment  of inertia  (bh /12) of
     the rectangular  cross-sectional  area of width b  and thickness  h  about the centroidal  axis
     (z-axis), and y  is the distance  from  the neutral plane. The maximum bending stress a max
     occurs  when x  = 0 and y  = ±h/2  and is given by
                                        6/y
                                                                      (5.3)
                                           2
                                        bh
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