Page 388 - Cam Design Handbook
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THB12  9/19/03  7:34 PM  Page 376

          376                      CAM DESIGN HANDBOOK

          F sh = torque on shaft, lb/in (Nm)
           F y = compressive contact force in the radial direction between the cam surface and the
               follower, lb (N)
                                             2
           I c = mass moment of inertia of the cam, lb/in /RAD (N/m/RAD)
           k r = follower return spring rate, lb/in/RAD (N/m)
           k s = drive system flexibility lb/in/RAD (N/m/RAD)
           m = follower mass, lb (kg)
           Q = variable reflected follower inertia ratio
          Q m = maximum reflected inertia ratio
           R = radius from cam center to follower roller center, in (m)
           T = drive system torque at cam speed, lb/in (N-m)
            t = time, sec
            x = follower displacement, in (m)
            .
            x = follower velocity (dx/dt) in/sec (m/s)
                                 2
                                              2
                                          2
                                    2
            x ¨ = follower acceleration (d x/dt ) in/sec (m/s )
           x¢= cam slope (dx/dq c), in (m)
                                          2
                                      2
           x≤= rate of change of cam slope (d x/dq c ), in (m)
           x f = final or total displacement of rise, in (m)
            y = normalized cam position, in (m)
           b = variable cam drive system windup ratio
           b m = maximum cam drive system windup ratio
           g = variable follower radial force ratio
           g m = maximum follower radial force ratio
           h = limiting linear frequency ratio
           q c = cam angular position, rad
            .
           q c = cam angular velocity, rad/sec
           ¨
           q c = cam angular acceleration, rad/sec 2
           q f = final or total duration of rise, rad
           q i = input power source position, rad
            .
           q i = input power source speed, rad/sec
            f = cam surface pressure angle, rad
           w b = base natural frequency rad/sec
           w l = limiting linear natural frequency, rad/sec
           w n = variable natural frequency, rad/sec
             The  system  takes  account  of  camshaft  flexibility  and  leads  to  a  set  of  nonlinear
          equations owing to the fact that the driving-cam function is no longer a known function
          of time.
             In Fig. 12.10, where q i(t), the input shaft rotating at a known angular rate, is not equal
          to the cam angle, q c , or q i π q c . This is due to camshaft flexibility; k s is the camshaft spring
          rate and the cam-follower rise is x. A convenient method of formulation is derivable from
          Lagrange’s equations as follows:
                                         2 ˙
                                             Iq
                                  T =  1  Mx +  1 ˙  2
                                     2      2  c
                                              2
                                  V =  1 2  k (q  c  - ) +  1 2  k x  2
                                            q
                                                  s
                                             i
                                       s
                                       -
                                  L =  T V.
          The follower is constrained by the cam function
                                            q
                                        x =  x()
                                             c
          where q i = q i(t), by the Lagrange multiplier method
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