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                                                                               Fatigue Failure Resulting from Variable Loading  311


                                                               2
                                                                   2
                                                            (1) 33.9 (84) 2                S a  31.4
                                     Answer          S a =               = 31.4 kpsi,  S m =  =     = 31.4 kpsi
                                                               2
                                                                     2
                                                            33.9 + (1) 84 2                r     1
                                               To verify the fatigue factor of safety, n f = S a /σ a = 31.4/8.38 = 3.75.
                                                  As before, let us calculate  r crit . From the third row second column panel of
                                               Table 6–8,
                                                         2(84)33.9 2
                                                    S a =   2     2  = 23.5 kpsi,  S m = S y − S a = 84 − 23.5 = 60.5kpsi
                                                         33.9 + 84
                                                              23.5
                                                         S a
                                                   r crit =  =    = 0.388
                                                         S m  60.5
                                               which again is less than r = 1, verifying that fatigue occurs first with n f = 3.75.
                                                  The Gerber and the ASME-elliptic fatigue failure criteria are very close to each
                                               other and are used interchangeably. The ANSI/ASME Standard B106.1M–1985 uses
                                               ASME-elliptic for shafting.









                            EXAMPLE 6–11       A flat-leaf spring is used to retain an oscillating flat-faced follower in contact with a
                                               plate cam. The follower range of motion is 2 in and fixed, so the alternating component
                                               of force, bending moment, and stress is fixed, too. The spring is preloaded to adjust to
                                               various cam speeds. The preload must be increased to prevent follower float or jump.
                                               For lower speeds the preload should be decreased to obtain longer life of cam and
                                                                                                            1
                                               follower surfaces. The spring is a steel cantilever 32 in long, 2 in wide, and  in thick,
                                                                                                            4
                                               as seen in Fig. 6–30a. The spring strengths are S ut = 150 kpsi, S y = 127 kpsi, and S e =
                                               28 kpsi fully corrected. The total cam motion is 2 in. The designer wishes to preload
                                               the spring by deflecting it 2 in for low speed and 5 in for high speed.
                                               (a) Plot the Gerber-Langer failure lines with the load line.
                                               (b) What are the strength factors of safety corresponding to 2 in and 5 in preload?
                                    Solution   We begin with preliminaries. The second area moment of the cantilever cross section is

                                                                       bh 3  2(0.25) 3         4
                                                                   I =    =         = 0.00260 in
                                                                       12      12
                                               Since, from Table A–9, beam 1, force F and deflection y in a cantilever are related by
                                                         3
                                               F = 3EIy/l , then stress σ and deflection y are related by
                                                                 Mc    32Fc   32(3EIy) c   96Ecy
                                                            σ =     =       =     3      =    3  = Ky
                                                                  I     I         l    I     l
                                                                        6
                                                         96Ec   96(30 · 10 )0.125        3
                                               where K =   3  =         3      = 10.99(10 ) psi/in = 10.99 kpsi/in
                                                          l           32
                                               Now the minimums and maximums of y and σ can be defined by
                                                                    y min = δ     y max = 2 + δ
                                                                    σ min = Kδ    σ max = K(2 + δ)
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