Page 477 - Shigley's Mechanical Engineering Design
P. 477

bud29281_ch08_409-474.qxd  12/16/2009  7:11 pm  Page 452 pinnacle 203:MHDQ196:bud29281:0073529281:bud29281_pagefiles:







                 452    Mechanical Engineering Design
                  Figure 8–23

                  Modes of failure in shear
                  loading of a bolted or riveted
                  connection: (a) shear loading;
                  (b) bending of rivet; (c) shear
                  of rivet; (d) tensile failure of
                  members; (e) bearing of rivet
                  on members or bearing of
                  members on rivet; (f) shear
                  tear-out; (g) tensile tear-out.
                                             (a)        (b)       (c)          (d)














                                                (e)            ( f )           (g)

                                              Rupture of one of the connected members or plates by pure tension is illustrated
                                          in Fig. 8–23d. The tensile stress is
                                                                              F
                                                                          σ =                              (8–54)
                                                                              A
                                          where A is the net area of the plate, that is, the area reduced by an amount equal to
                                          the area of all the rivet holes. For brittle materials and static loads and for either duc-
                                          tile or brittle materials loaded in fatigue, the stress-concentration effects must be
                                          included. It is true that the use of a bolt with an initial preload and, sometimes, a rivet
                                          will place the area around the hole in compression and thus tend to nullify the effects
                                          of stress concentration, but unless definite steps are taken to ensure that the preload
                                          does not relax, it is on the conservative side to design as if the full stress-concentration
                                          effect were present. The stress-concentration effects are not considered in structural
                                          design, because the loads are static and the materials ductile.
                                              In calculating the area for Eq. (8–54), the designer should, of course, use the
                                          combination of rivet or bolt holes that gives the smallest area.
                                              Figure 8–23e illustrates a failure by crushing of the rivet or plate. Calculation of
                                          this stress, which is usually called a bearing stress, is complicated by the distribution
                                          of the load on the cylindrical surface of the rivet. The exact values of the forces act-
                                          ing upon the rivet are unknown, and so it is customary to assume that the components
                                          of these forces are uniformly distributed over the projected contact area of the rivet.
                                          This gives for the stress
                                                                               F
                                                                         σ =−                              (8–55)
                                                                               A
                                          where the projected area for a single rivet is  A = td. Here, t is the thickness of the
                                          thinnest plate and d is the rivet or bolt diameter.
   472   473   474   475   476   477   478   479   480   481   482