Page 480 - Shigley's Mechanical Engineering Design
P. 480

bud29281_ch08_409-474.qxd  12/16/2009  7:11 pm  Page 455 pinnacle 203:MHDQ196:bud29281:0073529281:bud29281_pagefiles:







                                                                       Screws, Fasteners, and the Design of Nonpermanent Joints  455
                                               Member yield:

                                                                       wt(S y ) mem  4(1)54
                                                                  F =           =        = 144 kip
                                                                          n d       1.5
                                               On the basis of bolt shear, the limiting value of the force is 45.9 kip, assuming the
                                               threads extend into a shear plane. However, it would be poor design to allow the threads
                                               to extend into a shear plane. So, assuming a good design based on bolt shear, the lim-
                                               iting value of the force is 57.8 kip. For the members, the bearing stress limits the load
                                               to 54 kip.


                       Figure 8–25
                       Edge shearing of member.        Bolt

                                                                         d




                                                                    a




                                               Shear Joints with Eccentric Loading
                                               In the previous example, the load distributed equally to the bolts since the load acted
                                               along a line of symmetry of the fasteners. The analysis of a shear joint undergoing
                                               eccentric loading requires locating the center of relative motion between the two mem-
                                               bers. In Fig. 8–26 let  A 1 to  A 5 be the respective cross-sectional areas of a group of
                                               five pins, or hot-driven rivets, or tight-fitting shoulder bolts. Under this assumption the
                                               rotational pivot point lies at the centroid of the cross-sectional area pattern of the pins,
                                               rivets, or bolts. Using statics, we learn that the centroid  G is located by the coordi-
                                               nates  ¯x and  ¯y, where x 1 and  y i are the distances to the ith area center:

                                                                                                  n
                                                               A 1 x 1 + A 2 x 2 + A 3 x 3 + A 4 x 4 + A 5 x 5  1  A i x i
                                                           ¯ x =                              =    n
                                                                    A 1 + A 2 + A 3 + A 4 + A 5    1  A i
                                                                                                  n            (8–56)
                                                               A 1 y 1 + A 2 y 2 + A 3 y 3 + A 4 y 4 + A 5 y 5  1  A i y i
                                                           ¯ y =                              =    n
                                                                    A 1 + A 2 + A 3 + A 4 + A 5    1  A i
                       Figure 8–26                y

                       Centroid of pins, rivets, or     A 2           A  3
                       bolts.
                                                                   A 4

                                                                  G
                                                       A 1
                                                _
                                                y
                                                                       A 5
                                                                           x
                                                 O
                                                          _
                                                          x
   475   476   477   478   479   480   481   482   483   484   485