Page 178 - Cam Design Handbook
P. 178

THB6  8/15/03  2:40 PM  Page 166

          166                      CAM DESIGN HANDBOOK



          1
                               0.31                  0.53
            0           b          0           b         0          b
               (a) Parabolic.     (b) Simple Harmonic.  (c) 3-4-5 Polynomial.




          4.5
                          1                          0.75
                               0.43
            0          b           0          b         0         b
           (d ) Cubic no.1.       (e) Modified sine.  (f ) Trapezoidal
                                                            modified trapezoidal
                                                            4-5-6-7 Polynomial.

          1.3
                                0.69
                                                        0.44
            0           b          0           b            0         b
             (g) Circular arc.  (h) Cycloidal comparison of.  ( i ) Modified cycloidal radial cam.
          FIGURE 6.5  Side thrust comparison of cam curves.


             Let us discuss the side thrust effect on different cam curves. In Fig. 6.4, it has been
          shown that the greater the pressure angle, the greater the magnitude of the side thrust on
          the follower. During action, the side thrust varies continuously, depending on the cam
          curve used. Let’s compare cam curves on the basis of the magnitudes of the side thrust
          they produce. Fig. 6.5 presents such a comparison for a number of cam curves under the
          same  conditions,  i.e.,  equal  base  circle  size,  equal  range  of  cam  rotation  b,  and  equal
          loading condition. In addition, all cams had unity lift and unity follower weight. Also, the
          maximum side thrust of the parabolic curve is to serve as a basis of comparison with the
          side thrust of all other curves.
             From Fig. 6.5, it is apparent that the trigonometric function and the modified trigono-
          metric function curves are superior to the others, and that the trapezoidal, the modified
          trapezoidal, and the 4-5-6-7 polynomial curves produce about the same magnitude of side
          thrust. The cubic no. 1 curve and the circular-arc-tangent curve give the greatest amount
          of side thrust.


          6.3.3 Pressure Angle Forces—Oscillating Roller Follower
          The oscillating roller follower is generally an improvement over the translating type in
          that the distribution of forces allows a much larger limiting pressure angle for satisfactory
          performance. Thus, with an oscillating follower, a smaller cam may be used. It is sug-
          gested for best performance and highest accuracy that the trace point arc of motion should
          pass near or through the cam center. Also, by proper location of the follower pivot, it
          becomes virtually impossible to jam the follower, no matter how steep the cam surface.
          The extreme limiting condition is to make the pressure angle small enough to prevent the
   173   174   175   176   177   178   179   180   181   182   183