Page 177 - Cam Design Handbook
P. 177

THB6  8/15/03  2:40 PM  Page 165

                               ELEMENTS OF CAM PROFILE GEOMETRY            165

            Solving for the force normal to the cam

                                              L
                                               0
                                   F =         AB                          (6.7)
                                                +
                                      cosa  - m Ê 2  ˆ sina
                                             Ë  B  ¯
            The normal force F is a maximum (equals infinity) which means that the follower will
            jam in its guide when the denominator of Eq. (6.7) equals zero. Therefore,
                                             +
                                          Ê 2 AB ˆ
                                  cosa - m       sin a = 0
                                      m   Ë  B  ¯    m
            The maximum pressure angle without locking the follower in its guide is

                                                B
                                     a = tan -1      .                     (6.8)
                                      m
                                                 +
                                             m (2 AB)
            Let  us  substitute  some  trial  values  to  compare  the  magnitude  of  the  results.  If  we  let
            A = B and assume the values for the coefficient of friction of bronze on steel to be
                                 (
                                                m static) = 015
                                          .
                               m kinetic) = 010  and  (  .
            Substituting in Eq. (6.8), we find the maximum pressure angle for each condition:
                                      B
                          a = tan -1         = 73 degrees for m  = . 010
                           m
                                         +
                                  ( . 010 )(2 BB)
                                      B
                                                             015
                         a = tan -1          = 66 degrees for m  = ..
                          m
                                         +
                                 ( . 015 )(2 BB)
            Note that these values and the derivation of Eq. (6.8) are based on the ideal assumption
            that the follower is perfectly rigid. Thus, the coefficient of friction may actually reach a
            value of 0.25 or more depending on relative elasticity and backlash of the follower. A flex-
            ible stem may “dig” into the lower corner of the bearing. Therefore, the suggested guide
            in practice is to keep the coefficient of friction m, the follower overhang A, and the back-
            lash as small as possible with the bearing length B as large as possible, in the range of
            B = 2A. Generally the safe limiting pressure angle in practice is 30 degrees. However, for
            light loads with accurate low-friction bearings, the author was successful using a pressure
            angle as high as 48 degrees. Note that commercially available ball bushings for the linear
            moving stem have provided low friction and little backlash; see Chap. 10.
               We may observe that the follower jamming is of concern only when the follower moves
            in the direction opposite that of the external load L. As shown in Figure 6.4, jamming
            occurs during the rise period only. During the fall period, the size of the maximum pres-
            sure angle is generally not limited in proper cam design. However, the author has seen
            machine installations in which the follower drove the cam during the fall action. It occurred
            with a chain-driven cam and a spring-loaded follower. The spring force, acting on an exces-
            sive pressure angle of fall, produced detrimental shock and fluctuating action in absorb-
            ing the backlash of the system.
               Also, if the load L o varies according to the inertia acceleration in both the rise and fall,
            the pressure angle should be considered in both. Chapter 9 discusses load fluctuations and
            reflected torque curve which should be an initial point of analysis in all pressure angle
            investigations.
   172   173   174   175   176   177   178   179   180   181   182