Page 348 - Cam Design Handbook
P. 348

THB11  9/19/03  7:33 PM  Page 336

          336                      CAM DESIGN HANDBOOK


                                            F
                                                                    Last coil
                                                                    bottoms
                                                  First pair of
                                                 coils bottom
                                                                Next coil
                                                                bottoms
                           d (tension)                           d (compression)








          (a) Shape of spring.          (b) Force-deflection curve.
          FIGURE 11.12.  Variable-pitch coil spring.


          rates can be easily derived from a basic stress analysis. First, choose a simplified geome-
          try that approximates the shape of the element in question. Next, calculate the stress arising
          in the element as a result of the applied load. If it is assumed that the element is acting in
          the region of elastic deformation (a reasonable assumption for the systems in question here
          since they must be designed to survive cyclic motion and loading), the stress can then
          easily be related to strain. Finally, the deflection can be calculated from the strain and the
          spring rate determined from this relationship between force and deflection. This procedure
          is illustrated by a simple example.

          EXAMPLE Suppose a system uses a long rod (Fig. 11.13) loaded axially to transmit force
          between members (this is in fact the case in pushrod engines). The rod does not in fact
          remain perfectly rigid, but deflects as a result of the applied load. The axial stress that
          arises in the rod is given by
                                            F
                                         s =
                                            A
          where A is the cross-sectional area of the rod. In the linear region, the strain is propor-
          tional to the stress through Young’s modulus, so
                                          s   F
                                       e =  =   .
                                          E  EA
          Finally, the strain is simply deflection per unit length, so the deflection of the rod is
                                              FL
                                      d = L e =  .
                                             EA
             The spring rate follows directly from this expression, so for the axially loaded rod
                                          F  EA
                                      K =   =   .
                                          d   L
   343   344   345   346   347   348   349   350   351   352   353