Page 220 - 3D Fibre Reinforced Polymer Composites
P. 220

Z-Pinned Composites                         209

          small angle (less than -7').   The damage caused to composites by.the insertion of Z-
          fibersTM is still under investigation, and more research is needed to understand the types
          and  amounts  of  damage  caused  in  the  z-pinning  process.  The  limited  amount  of
          information that has been published on damage reveals that the most common types are
          misalignment and fracture of  in-plane fibres (Steeves and Fleck,  1999a).  The in-plane
          fibres of unidirectional tape laminates are misaligned and distorted when pushed aside
          during insertion of Z-fibersTM.  An example of the distortion of fibres around a z-pin is
          shown  in  Figure  9.5.  The misalignment angle of  in-plane  fibres  around  the  pins  is
          dependent  on  a  number  of  factors,  including  the  type  of  composite  (Le.  prepreg,
          thermoplastic, fabric preform), fibre lay-up orientations, and the fibre volume content of
          the  laminate.  Misalignment  angles  of  between  5"  and  15'  have  been  measured  in
          unidirectional tape  composites reinforced  with  Z-fibersTM, compared  to  unreinforced
          tape  laminates with  an  average misalignment  angle of  about 3'.   In  some cases the
          fibres can be so severely misaligned that they break.  The incidence of fibre breakage is
          not known, although it is expected to be small.  Due to the misalignment of  in-plane
          tows,  resin  rich  regions are  formed  at each side of  the pin,  as  shown in Figure  9.5.
          These regions  can  be  up  to  -1  mm  long, and  in  composites reinforced  with  a high
          density of Z-fibersTM these regions may join up to form continuous channels of resin.


























          Figure 9.5 In-plane fibre distortion around a z-pin in a composite.  Note the presence of
          the large resin-rich zones


          9.3 MECHANICAL PROPERTIES OF Z-PINNED COMPOSITES

          The in-plane mechanical properties and  failure mechanisms of  composites reinforced
          with Z-fibersTM have not been studied in detail. The effect of  Z-fiberTM reinforcement
          on  in-plane properties such as flexural modulus and  strength, shear strength, fatigue-
          life, and open-hole tensile and compressive strengths have not been reported, and it is
          an  important  topic  of  future  research  to  determine these  mechanical  properties  and
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