Page 204 - Cam Design Handbook
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THB7  8/15/03  1:58 PM  Page 192

          192                      CAM DESIGN HANDBOOK

          associated cam profile is the trajectory of the center of the roller follower, which is known
          as the pitch curve. Moreover, if the roller-follower cam is machined with a mill having a
          radius identical to that of its roller, then the pitch curve is identical to the trajectory of the
          cutter  center,  the  curve  needed  for  the  programming  of  the  NC  machine  tool  used  to
          produce the cam disk. Thus, for translating knife-edge and roller followers, the pressure-
          angle a can be obtained by:
                                            s ¢ - e
                                      tana =                            (7.33)
                                              s
          where s¢ is the first derivative of the displacement s with respect to the angle y and e as
          shown in Fig. 7.8.
             On the other hand, for both the knife-edge and the roller-follower, the curvature of the
          pitch curve is given by

                                             N
                                        k =                            (7.34a)
                                          k
                                             D
          where (Angeles and Lopez-Cajun, 1991)
                                 N ∫ (  -   s¢ -  e)(2 s¢ - e)         (7.34b)
                                    s s s¢¢)+ (
          and
                                               2 32
                                    D ∫[ s + ( s¢ - ] .                (7.34c)
                                              e)
                                        2
          7.4.2.4 Oscillating Roller Followers.  For the oscillating roller follower, the formula
          given  below  can  be  used  to  calculate  the  pressure  angle  (Angeles  and  Lopez-Cajun,
          1991)
                                     l rq  sinf +  r(l cosf - ) e
                                      ¢()
                               tana =                                  (7.35a)
                                     rq   cosf - ) -e  r l  sinf
                                      ¢()(l
          where
                                             ¢()
                                            ry
                                      rq                               (7.35b)
                                       ¢() =
                                             ¢()
                                            q y
                                          el fy   f
                                            ¢()sin
                                    ry                                 (7.35c)
                                     ¢() =
                                              r
                                                  f y
                                        ¢() - r
                                      l ef y  2 [1 + ¢()]
                                 ¢() =
                                qy                                     (7.35d)
                                             r  2
          and the parameters involved are shown in Fig. 7.9.
             Finally, the formula for calculating the curvature of the pitch curve of the oscillating
          roller follower is (Angeles and Lopez-Cajun, 1991)
                                  3
                                           (
                                                     +
                                    el (1
                            2
                           e (1 + f¢) - [  +  f¢) +2  f¢)cos f f¢¢sin f]+ l  2
                       k =                                              (7.36)
                        k              2                 32
                                [ e (1 + f¢) - 2 el + f¢)cos f l ]
                                                       2
                                                     +
                                            (1
                                  2
          where the argument y of f¢ and f≤ have been omitted for simplicity.
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