Page 65 - Analysis and Design of Machine Elements
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Strength of Machine Elements
                            Therefore, the safety factor and fatigue strength of the element under variable uniaxial  43
                          stresses is
                                                     √
                                        lim     −1Nv  √   N 0
                                                     √
                               S =       =      =     √        ≥ [S]                         (2.41)
                                ca
                                       max     1   −1 m √ z
                                                     √ ∑
                                                          n    m
                                                           i i
                                                        i=1
                          2.3.6  Fatigue Strength for Combined Stresses with Constant Amplitude
                          During machine operation, an element is most likely subjected to a combination of ten-
                          sion, bending and torsion, so both tensile and shear stresses will generate. Under static
                          stress states, yield occurs when the equivalent stress obtained from the maximum dis-
                          tortion energy theory equals the uniaxial yield strength expressed by
                                 1         2         2         2 1∕2
                                √ [(   −    ) +(   −    ) +(   −    ) ]  =    s              (2.42)
                                                    3
                                               2
                                         2
                                     1
                                                          3
                                                              1
                                  2
                          where the three principle normal stresses are
                                        1  √
                                  =   +       + 4    2                                       (2.43)
                                            2
                                1
                                    2   2
                                  = 0                                                        (2.44)
                                2
                                        1  √  2  2
                                  =   −       + 4                                            (2.45)
                                3
                                    2   2
                            Substituting the three principle normal stresses back into Eq. (2.42), we have
                               (   ) 2  (   ) 2
                                         3  
                                      +       = 1                                            (2.46)
                                    s       s
                            And from Eqs. (2.12) and (2.46), can be further expressed as
                               (   ) 2  ( ) 2
                                            
                                      +       = 1                                            (2.47)
                                           
                                  s       s
                            This relation was validated by experiment when all the stress components are com-
                          pletely reversed and always in the same phase [16]. By introducing a safety factor, the
                          fatigue strength under completely reversed stress can be evaluated by [17]
                               (      ) 2  (    ) 2
                                 S          S   
                                  ca a       ca a
                                        +          = 1                                       (2.48)
                                     −1e       −1e
                            Here we define     −1e  = S and     −1e  = S , which are associated with completely reversed
                                                            
                                            a          a
                          tensile and shear stress, respectively. Therefore, we have
                               (    ) 2  (   ) 2
                                 S ca     S ca
                                      +        = 1                                           (2.49)
                                 S        S
                                             
                            Thus
                                       S S
                                             
                                ca
                               S = √                                                         (2.50)
                                       2
                                      S + S    2
                                         
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