Page 426 - Cam Design Handbook
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THB13  9/19/03  7:56 PM  Page 414

          414                      CAM DESIGN HANDBOOK

                                    m  Ê  a cos ( nT)+  b sin ( nT) ˆ
                              X = Â  Á  n        n     ˜.              (13.27)
                                  2
                                 F
                                  2  Ë      F -  n 2   ¯
                                             2
                                   n=0       2
          The required integration of Eq. (13.22) and Eq. (13.25) can now be performed exactly.
          The 2m + 1 coefficients can then be determined from the two equations, Eq. (13.23), and
          the 2m + 1 - 2l extremum conditions
                              dP   dP  dP
                                 =   =    =  0,  i 1= ◊◊◊,  , ml       (13.28)
                                                       - .
                              da  da   db
                                0   i    i
          Using  this  approach,  one  can  design  an  entire  cam  profile  at  once,  thereby  obtaining
          maximum control of the motion and its harmonic content. Alternatively, for greater gen-
          erality, one can design segments of low vibration motion by requiring that
                                       ¢()
                                                        p
                             yT () =  X ,  y T =  X¢, for 0  £  T £ ,  (13.29)
                               k    k    k    k       k
          in order to minimize R, see Eq. (13.5). These segments can then be pieced together to give
          a desired motion.
             To obtain an optimum cam profile design to satisfy any particular case requires per-
          forming several designs using different values of A 2/A 1 and A 3/A 1 to find the design that
          appears to give the best compromise between optimizing response for accuracy of dis-
          placement and velocity responses and minimaxed acceleration.
             As an example we consider the design of a unit rise dwell-rise-dwell motion designed
          to operate over the range F 2 ≥ 9. Three motions designed in this way are tabulated in
          Table  13.2  and  their  associated  acceleration  and  residual  vibration  characteristics  are
          shown in Figs. 13.9 and 13.10, respectively. These motions were obtained using values of
                                             -7
                                   -8
          A 1 = A 2 = 1 and A 3 = 0.0, 5 ¥ 10 , and 7 ¥ 10 in Eq. (13.22) for examples 4, 5, and 6,
          respectively.
             We again observe that for large values of F 2, the residual vibration of a family of cam
          profiles increases as the peak acceleration is decreased. In this section we have not imposed
          the constraints on the magnitude of jerk (i.e., y≤¢) or continuity of y≤ which are generally
                                                            ¯
                                            ¯
          suggested by rules of thumb. In the absence of these constraints we observe that the peak
          value of jerk is relatively high and that the acceleration begins and ends with definite dis-
          continuities that are small but increasing as A 3 increases. Nonetheless the high-speed vibra-
          tion characteristics of these motions represent a significant improvement over those of the
          cycloidal motion, and the accuracy of this predicted performance has been assured by con-
          trolling the harmonic content of the motion. The existence of such motions is contrary to

                             TABLE 13.2  Problem Solutions (Figs. 13.9 and
                             13.10)
                                    No. 4       No. 5       No. 6
                                    0.500000   0.500000    0.500000
                             a 0
                                   -0.583802  -0.543883   -0.466909
                             a 1
                                    0.095326   0.034106   -0.082227
                             a 3
                                   -0.012015   0.011519    0.054570
                             a 5
                                    0.000491  -0.001741   -0.005434
                             a 7
                                    0.000000  -0.002399   -0.098142
                             b 2
                                    0.000000   0.002835    0.078912
                             b 4
                             b 6    0.000000  -0.001293   -0.021730
                                    0.000000   0.000152    0.001378
                             b 8
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