Page 217 - Cam Design Handbook
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THB7  8/15/03  1:58 PM  Page 205

                                GEOMETRY OF PLANAR CAM PROFILES            205


                           s y  s y    s y   s y    s y   s  y            (7.78)
                                                     ¢¢¢() = ¢¢¢().
                           ¢() = ¢(),
                                        ¢¢() = ¢¢(),
               On the other hand, the tangent of the pressure angle was derived in Angeles and Lopez-
            Cajun (1991) as
                                              s ¢()
                                                y - e
                                     tanay () =      .                    (7.79)
                                               s  y ()
               Now, substituting Eqs. (7.77) and (7.78) into Eq. (7.79) yields
                                               ¢()
                                              sy - e
                                     tanay () =      .                    (7.80)
                                              sy ()+ c
               If, moreover, y 1 and y 2 are the values at which the pressure angle attains a maximum
            a M and a minimum a m , the corresponding extremality conditions take the form
                                     ¢¢() - ¢()tan
                                    sy    s y    a  M  = 0               (7.81a)
                                     1
                                           1
                                    sy    sy     a m  = 0                (7.81b)
                                     ¢¢() - ¢()tan
                                           2
                                     2
            with s i = s(y i), for i = 1, 2, and s¢ i(y i) and s≤ i (y i) defined likewise. The problem thus
            reduces to solving two independent nonlinear equations, (7.81a) and (7.81b), for the two
            unknowns y 1 and y 2. Furthermore, we have, from Eq. (7.80),
                                  ctana += ¢ -  s  1  tana m              (7.82)
                                          e s
                                       M
                                              1
                                  ctana += ¢ -  s  tana  .                (7.83)
                                          e s
                                       M      2   2   m
               Equations  (7.82)  and  (7.83)  thus  suggest  a  graphical  solution  of  the  optimization
            problem at hand, for each of these equations represents a line in the c-e plane.
               The optimum values of c and e are found as the coordinates of the intersection of these
            two lines, as illustrated in Fig. 7.14, where we have assumed that a m =-a M and a M = 30°.
            Moreover, the optimum values c opt and e opt can be obtained by solving for these parame-
            ters from Eqs. (7.82) and (7.83), namely,
                                                s
                                    s ¢ -s tan a  - ¢ +s tan a
                                c  =  1  1   M   2   2    m              (7.84a)
                                opt
                                         tan a  - tan a
                                             M      m
                                   (
                             -tanas  ¢ -s  tana  )+ tana  (s ¢ -s  tana  )
                        e  =      m  1  1    M      M  2   2    m  .     (7.84b)
                         opt
                                         tana  - tana
                                             M      m
               Finally, from the geometry of the translating cam mechanism, the optimum radius of
            the base circle of the optimum cam is
                                              2
                                       b  =  e +  c 2                     (7.85)
                                        opt   opt  opt
            which can be readily computed using Eqs. (7.84a and b).
               Now we apply the foregoing relations to the size-minimization of the cam plate of a
            quick-return mechanism. This mechanism is a mechanical transmission that produces a
            slow feed motion under a load in one direction, followed by a fast return stroke under no
            load in the opposite direction. Quick-return mechanisms are frequently used in manufac-
            turing  processes,  e.g.,  in  pick-and-place  operations,  metal-cutting,  and  metal-forming.
            Cam mechanisms are well suited for this type of task, because they can readily produce
            such a type of motion. The required motion for this case is the dwell-rise-dwell-return dis-
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