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Chapter 5



            3D Woven Composites








            5.1 INTRODUCTION

            3D woven composite is a new type of  advanced engineering material that is currently
            used in only a few niche applications.  The most significant applications are stiffeners
            for the air induct duct panels on  the Joint Strike Fighter,  aircraft wing joints on the
           Beech Starship, and rocket nose cones.  3D woven sandwich composite reinforced with
           distance fabric is also used in modest amounts, such as floor panels for trains, hard-tops
            for convertible cars, and the deck and top-side structure for a fishing boat. While the
            present use of 3D woven composite is limited, the potential use is impressive and wide-
           ranging  with  various  possible  applications  in  the  aerospace,  marine,  infrastructure,
            military and medical fields.  As described in chapter 1, in the future this composite may
            be used in a diverse variety of  items ranging from jet-engine components to personnel
            body armour to artificial limbs.
              While the future of 3D woven composites appears promising, it is not assured. Many
           challenges are facing the increased application of this material.  A major factor is that
           the cost of 3D woven composites is currently higher than 2D prepreg or fabric laminates
           for many applications.  It was discussed in chapter 2 that the 3D weaving process has
           the potential to  reduce lay-up and  assembly costs  in fabrication, however 3D woven
           fabric  is  not  yet  produced  in  large  commercial  quantities  at  low  cost.  Another
           impediment to the increased use of 3D woven composite in the aircraft industry is the
           high  cost  of  certifying  these  and  other  new  materials  for  primary  load-bearing
           structures.  Until the cost savings and other benefits of  3D woven composite are fully
           appreciated, then aircraft manufacturers will continue using conventional 2D laminates
            in most composite components.
              Another  significant  challenge  is  that  many  designers,  fabricators  and  users  of
           composites are unsure of  the potential benefits of  using  3D  woven  composite. Most
            sectors of the composite industry do not fully appreciate the benefits gained from using
            3D  woven  material,  such  as  reduced  fabrication  cost,  greater  design  flexibility,
           improved impact resistance, and superior through-thickness mechanical properties.  The
           design  and  fabrication  of  3D  woven  composite  is  described  in  Chapter  2  and
            micromechanical  models  for  predicting  their  stiffness  and  strength  are  outlined  in
           Chapter 4.  In  this chapter the in-plane mechanical properties, delamination resistance
            and  impact damage properties of  3D woven composites are described.  In Section 5.2
           the  microstructural features of  3D  woven  composites that  affect the  mechanical  and
            impact properties are described.  This includes a description of microstructural damage
           such as fibre crimping, fibre damage and z-binder distortion that degrade the in-plane
           and through-thickness properties. The mechanical properties and failure mechanisms of
            3D  woven  composites  under  tension,  compression, bending,  interlaminar  shear  and
            fatigue loads are described in Section 5.3.  Following this, the delamination resistance
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