Page 194 - Plastics Engineering
P. 194

Mechanical Behaviour of  Composites                             177
                value VI. From Fig. 3.5 the value of  VI is obtained from








                  In practice the maximum volume fraction, V,,   which can be  achieved in
                unidirectional fibre composites is about 0.8. Designers must therefore arrange
                for volume fractions to be in the range V1  + V,.   It should also be noted that
                in commercial production it is not always possible to achieve the high standards
                of  manufacture necessary to obtain full benefit from the fibres. It is generally
                found that although the stiffness is predicted quite accurabzly by equation (3.5),
                the strength is usually only about 65% of  the value calculated by  the rule of
                mixtures. For fibre reinfonxmeint systems other than unidirectional fibres, these
                values can be reduced even more. To allow for this a constant ‘k’ is sometimes
                included in the fibre contribution to equation (3.6).
                  Example 3.4  Far  the  PEEWcarbon  fibre  composite  referred  to  in
                Example 3.2 calculate the values of  V1  and Vht if it is known that the ultimate
                tensile strength of  PEEK is 62 MN/m2.

                  Solution From equation (3.7)

                                  a,,   - a;       0.062 - 0.058
                                              -
                         Vent  =              -                   = 0.19%
                                   f Ornu - 0;   2.1 + 0.062 - 0.058
                and from equation (2.46)
                                     u,,  - U&  - 0.062 - 0.058
                                v1  =        -               = 0.2%
                                     ofu - 0;    2.1 - 0.058

                (ii)  Properties Perpendicular to Longitudinal Axis
                  The properties of  a unidirectional fibre will  not  be  nearly  so good in  the
                transverse direction compared with the longitudinal direction. As  a material
                in  service is likely to be subjected to stresses and strains in  all directions it
                is  important to  be  aware  of  the  properties in  all directions. The transverse
                direction will, of course, be the weakest direction and so it is necessary to pay
                particular attention to this.
                  The transverse modulus, Ec~, may be determined in a manner similar to that
                described earlier for the longitudinal modulus. Consider a unidirectional fibre
                composite subjected to a transverse force, Fc~, in the direction perpendicular
                to the fibre axis.
   189   190   191   192   193   194   195   196   197   198   199