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THB13  9/19/03  7:56 PM  Page 445

                                CAM SYSTEM DYNAMICS—RESPONSE               445

                         1.0
                                                               8
                                     y
                         0.8                         y ≤       6
                        y = 1 – 3 1 / 3x  2  + 5x  4  – 2 2 / 3x  5  0.6  y ¢≤  2 y ≤ = 6 2 / 3 + 60x  2  – 53 1 / 3x  3
                                                               4


                                                               0
                         0.4
                                                               –2
                                                               –4
                         0.2
                                                               –6
                                                               –8
                           0
                            0     0.2    0.4   0.6    0.8   1.0
                                             x
                       FIGURE 13.24. Simplest polynomial for DRRD profiles combining zero
                       acceleration at the start and zero velocity with finite acceleration at junc-
                       ture of rise and return phases.





                                   1.0
                                               y
                           60      0.8                        y ≤
                           40
                        y ¢≤ = 240x  2  – 300x  3  –20 0  y = 1 – 2.5x  2  + 4x  5  – 2.5x  6  0.6  y ¢≤
                           20


                                   0.4
                          –40
                          –60      0.2


                                    0
                                      0     0.2    0.4   0.6   0.8
                                                     x
                       FIGURE  13.25. Effect  of  changing  2-4-5  polynomial  of  Fig.  13.24
                       to  2-5-6  to  obtain  near  equivalence  of  maximum  positive  and  negative
                       accelerations.
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