Page 72 - Plastics Engineering
P. 72

Mechanical Behaviour of Plastics                                55

                 Also, the classical elastic equation for the end deflection of  a cantilever is:
                                                       WL3
                                          deflection, 6 = -                   (2.12)
                                                       3EI
                 Combining (2.11) and (2.12) gives

                                                     36d
                                            strain, E  = -                    (2.13)
                                                     2L2
                 so
                                         2(40)* x 0.005
                                     d=                = 2.7 mm
                                             3x2
                 (ii) The short-term stress in the material is obtained from the short-term modulus
                 which is given in this question (or could be obtained from the creep/isometric
                 curves, i.e. at 10 seconds, E = 8 x  106/0.5% = 1.6 GN/m2 or from the appro-
                 priate isometric curve).

                               stress = EE = 1.6 x  lo9 x  0.005 = 8 MN/m2

                 (iii) After  1  week (6.1 x  lo5 seconds), the isometric curves (Fig. 2.8) derived
                 from the creep curves show that  at  a  strain of  0.5% the  stress would  have
                 decayed to about 3.3 MN/m2.
                   Example 2.2 A polypropylene beam is  100 mm long, simply supported at
                 each end and is subjected to a load W at its mid-span. If the maximum permis-
                 sible strain in the material is to be 1.5%, calculate the largest load which may
                 be applied so that the deflection of the beam does not exceed 5 mm in a service
                 life of  1 year. For the beam I  = 28 mm4 and the creep curves in Fig. 2.5 should
                 be used.

                   Solution The central deflection in  a beam loaded as shown in Fig. 2.12  is
                 given by

                                              a=-  WL3
                                                  48EI
                                                  48EI6
                                             w=-
                                                    L3


                                                W






                                Fig. 2.12  Simply supported beam with central load
   67   68   69   70   71   72   73   74   75   76   77