Page 523 - Shigley's Mechanical Engineering Design
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                                                                         Welding, Bonding, and the Design of Permanent Joints  497
                                               In the absence of a midrange component, the fatigue factor of safety n f is given by

                                                                                 12 000
                                                                           S se
                                     Answer                           n f =   =        = 4.72
                                                                           τ a    2545








                             EXAMPLE 9–6       The 1018 steel strap of Fig. 9–22 has a repeatedly applied load of 2000 lbf (F a = F m =
                                               1000 lbf). Determine the fatigue factor of safety fatigue strength of the weldment.

                                    Solution   From Table 6–2, p. 288, k a = 39.9(58) −0.995  = 0.702. From case 2 of Table 9–2

                                                                    A = 1.414(0.375)(2) = 1.061 in 2
                                               For uniform shear stress on the throat k b = 1.
                                                  From Eq. (6–26), p. 290, k c = 0.59. From Eqs. (6–8), p. 282, and (6–18), p. 287,
                                                              S se = 0.702(1)0.59(1)(1)(1)0.5(58) = 12.0 kpsi

                                               From Table 9–5, K fs = 2. Only primary shear is present:

                                                                          K fs F a  2(1000)
                                                                                         = 1885 psi
                                                                τ = τ =         =
                                                                      m
                                                                 a
                                                                            A      1.061
                                                                       .
                                               From Eq. (6–54), p. 317, S su = 0.67S ut . This, together with the Gerber fatigue failure
                                               criterion for shear stresses from Table 6–7, p. 307, gives
                                                                         ⎡                       ⎤

                                                          1  	  0.67S ut  
 2  τ a   	  2τ m S se  
 2
                                                     n f =               ⎣ −1 +  1 +             ⎦
                                                          2    τ m    S se            0.67S ut τ a
                                                                           ⎧                          ⎫

                                                                     2


                                                          1 0.67(58)  1.885  ⎨           2(1.885)12.0  2 ⎬
                                     Answer          n f =                   −1 +  1 +                   = 5.85
                                                          2   1.885    12.0 ⎩           0.67(58)1.885  ⎭
                       Figure 9–22                 W 4- × 13-in I beam
                                                                           E6010
                                                 1018                  3  in
                                                                       8


                                                                   2 in
                                                                                    2000 lbf
                                                                          1018      repeatedly
                                                                      1  in         applied (0–2000 lbf)
                                                                      2
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