Page 296 - Marks Calculation for Machine Design
P. 296

P1: Shashi
                          January 4, 2005
                                      15:4
        Brown.cls
                 Brown˙C07
                                           STRENGTH OF MACHINES
                  278
                    The equation of the straight line from (N = 1) where the fatigue strength (S f ) is the
                                                        3
                  ultimate tensile strength (S ut ) to the knee at (N =10 ) cycles has the form
                                                    −0.01525
                                            S f = S ut N                       (7.2)
                                                                 3
                  where the fatigue strength (S f ) has the value (0.9 S ut ) at (N =10 ) cycles.
                                                               3
                    The equation of the straight line from the knee at (N = 10 ) cycles where the fatigue
                                                    6
                  strength (S f ) is (0.9 S ut ) to the knee at (N = 10 ) cycles where the fatigue strength (S f ) is
                  (S e ) has the form in Eq. (7.3)
                                                      b
                                               S f = aN                        (7.3)
                  where the coefficient (a) has units of stress and is given by Eq. (7.4)
                                                 (0.9 S ut ) 2
                                             a =                               (7.4)
                                                    S e
                  and the exponent (b) is dimensionless and given by Eq. (7.5)
                                                1    0.9 S ut
                                           b =−   log                          (7.5)
                                                3      S e
                    If the amplitude stress (σ a ) is known, then substitute this value in Eq. (7.5) and solve for
                  the number of cycles (N), which is given in Eq. (7.6) as
                                                      1/b

                                                   σ a
                                              N =                              (7.6)
                                                   a
                  Consider the following example using the above equations for finite life.
                            U.S. Customary                       SI/Metric
                  Example 2. Estimate the following design  Example 2. Estimate the following design
                  information for a machine element made of a  information for a machine element made of a
                  particular steel:                  particular steel:


                  a. Rotating-beam endurance limit (S )  a. Rotating-beam endurance limit (S )
                                          e
                                                                             e
                                                                        5
                                      5
                  b. Fatigue strength (S f ) at 10 cycles  b. Fatigue strength (S f ) at 10 cycles
                  c. Expected life for a stress level of 60 kpsi  c. Expected life for a stress level of 420 MPa
                  where S ut is 90 kpsi and S y is 70 kpsi.  where S ut is 630 MPa and S y is 490 MPa.
                  solution                           solution
                  Step 1. Using the guidelines in Eq. (7.1) where  Step1.  UsingtheguidelinesinEq.(7.1)where
                  the ultimate tensile strength (S ut ) is less than  the ultimate tensile strength (S ut ) is less than
                  100 kpsi, the rotating-beam endurance limit  1400 MPa, the rotating-beam endurance limit
                  (S ) is                            (S ) is


                    e                                 e


                      S = 0.504 S ut = 0.504 (90 kpsi)  S = 0.504 S ut = 0.504 (630 MPa)
                                                         e
                       e
                        = 45.4 kpsi                       = 317.5MPa
                  Step 2. Using Eq. (7.4), calculate the coeffi-  Step 2. Using Eq. (7.4), calculate the coeffi-
                  cient (a) as                       cient (a) as
                         (0.9 S ut ) 2  (0.9 (90 kpsi)) 2   (0.9 S ut ) 2  (0.9 (630 MPa)) 2
                      a =       =                       a =        =
                            S e     45.4 kpsi                 S e      317.5MPa
                         6,561 kpsi 2                       321,489 MPa 2
                       =          = 144.5 kpsi            =           = 1,013 MPa
                          45.4 kpsi                          317.5MPa
   291   292   293   294   295   296   297   298   299   300   301