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THB4  8/15/03  1:01 PM  Page 94

          94                       CAM DESIGN HANDBOOK

                                     Displacement
                                                                 Dwell
                            Velocity


                        y, y', y'', y'''








                 Dwell
                          Cam angle q



                               Jerk                      Acceleration
                 FIGURE 4.3.  The 4-5-6-7 polynomial dwell-rise-dwell cam curve.


                           TABLE 4.2  Curve Comparison
                           Profile           Maximum acceleration

                           Harmonic         ±4.9
                           3-4-5            ±5.8
                           Cycloidal        ±6.3
                           4-5-6-7          ±7.3




          4.5 POLYNOMIAL CURVE GENERAL
          DERIVATION DRD CAM

          The successive derivative control for the DRD cam action can be generalized
                                                    s
                               y =  C q  p  +  C q  q  +  C q  r  +  C q ...
                                        q
                                   p
                                             r
                                                  s
          which can be shown (Stoddart, 1953) having the boundary control conditions equal to zero
          at the endpoints
                                          C qrs ...
                                C =        0
                                  p  ( q - ) - ) -  p) ...
                                        p r (
                                             p s (

                                         C prs ...
                                C =        0
                                  q  ( pq r q s q) ...
                                              (
                                         (
                                      - ) - ) -

                                         C pqs ...
                                C =       0
                                  r  ( pr q r s r) ...
                                      - )(
                                           - ) -
                                              (
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