Page 273 - Plastics Engineering
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256                                             Processing of  Plastics

                                              D
                                       Pitch =n  tan 0
                                                       ,  e   ~
                                                                                 r









                                                                                KD







                                                     \  \  'WA\\

                                                      AIPI
                                              Fig. 4.9  Development of screw


                          The total output is the combination of  drag flow, back pressure flow  and
                        leakage. So from (4.3),  (4.7) and (4.8)
                                                     nDH3 sin2 I$ dP   n2D2J3   dP
                           Q = $T~D~ sin4cos4 -                             tan+--    (4.9)
                                     NH
                                                         12~  dL       12~e     dL
                          For many  practical purposes sufficient accuracy is obtained by  neglecting
                        the leakage flow term. In addition the pressure gradient is often considered as
                        linear so
                                                     dP    P
                                                         -
                                                     _- -
                                                     dL    L
                        where  'L'  is the length of  the extruder. In practice the length of  an extruder
                        screw can vary between 17 and 30 times the diameter of the barrel. The shorter
                        the screw the cooler the melt and the faster the moulding cycle. In the above
                        analysis, it  is  the  melt  flow  which  is  being  considered  and  so  the  relevant
                        pressure  gradient  will  be  that  in  the  metering zone.  However, as  shown in
                        Fig. 4.2 this is often approximated by P/L. If all other physical dimensions and
                        conditions are constant then the variation of output with screw flight angle, 4,
                        can be studied. As shown in Fig. 4.10 the maximum output would be obtained
                        if  the screw flight angle was about 35°C. In practice a screw flight angle of
                        17.7" is frequently used because
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