Page 355 - Marks Calculation for Machine Design
P. 355

P1: Sanjay
                          January 4, 2005
                                      15:14
        Brown.cls
                 Brown˙C08
                              U.S. Customary  MACHINE ASSEMBLY    SI/Metric       337
                    Step 4. Substitute the bolt preload (F preload )  Step 4. Substitute the bolt preload (F preload )
                    found in step 2, and the given joint constant  found in step 2, and the given joint constant
                    (C) and external load (P) in Eq. (8.49) to  (C) and external load (P) in Eq. (8.49) to
                    determine the factor-of-safety against separa-  determine the factor-of-safety against separa-
                    tion (n separation ) as            tion (n separation ) as
                                 F preload                          F preload
                        n separation =                    n separation =
                                P (1 − C)                          P (1 − C)
                                    9,150 lb                           37,950 N
                              =                                  =
                                (2,500 lb)(1 − 0.25)               (11,000 N)(1 − 0.24)
                                9,150 lb                           37,950 N
                              =       = 4.9 ∼ 5                  =       = 4.5
                                           =
                                1,875 lb                           8,360 N
                      Notice that the load factor (n load ) and the factor-of-safety against separation (n separation )
                    are very similar. This is not unexpected.
                      Examples 1 through 4 summarize the steps to determine if a design is safe under static
                    loading conditions. In list form, they are:
                      Example 1: Determine the stiffness of the bolt (k bolt ), or cap screw.
                      Example 2: Determine the stiffness of the members (k members ).
                      Example 3:  Determine the joint constant (C).
                      Example 4:  Determine the load factor (n load ) and factor-of-safety against separation
                                (n separation ).

                      The development of the formulas needed to determine these design parameters might
                    have seemed at times to be excessive. However, it is important for the design engineer to
                    feel comfortable with the formulas in a design analysis, and if only a few basic principles
                    and simple algebra are required to show how these formulas are obtained, it is believed
                    these developments were worthwhile.

                    8.2.6 Fatigue Loading
                    The following discussion on fatigue loading applies only to the bolt or cap screw in a
                    connection, not the members. As the bolt or cap screw will always have a bolt preload
                    (F preload ), the bolt or cap screw will experience fluctuating loading, as was discussed in
                    Chap. 7. The maximum load on the bolt is the total bolt load (F bolt ) given by Eq. (8.39)
                    and the minimum load is the bolt preload (F preload ) given by the guidelines of Eq. (8.26).
                    Therefore, the mean force on the bolt (F m ) is given by Eq. (8.50) as
                                                 F bolt + F preload
                                            F m =                               (8.50)
                                                      2
                      Substitute the total bolt load (F bolt ) from Eq. (8.39) in Eq. (8.50) to give
                                                                 CP
                             (CP + F preload ) + F preload  CP + 2 F preload
                         F m =                   =             =    + F preload  (8.51)
                                       2                2         2
                      Similarly, the alternating force on the bolt (F a ) is given by Eq. (8.52) as
                                                 F bolt − F preload
                                            F a =                               (8.52)
                                                      2
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