Page 125 - Structural Steel Designers Handbook AISC, AASHTO, AISI, ASTM, and ASCE-07 Design Standards
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Brockenbrough_Ch03.qxd  9/29/05  5:05 PM  Page 3.57



                                                           CONNECTIONS


                                                                                          CONNECTIONS  3.57

                                    This results in a conservative connection capacity of

                                                    φR n = 2.06 × 19.6 = 40.4 kips < 51 kips  No good

                                    Alternatively, the direction of the force on each bolt can be found using the instantaneous center
                                    method. The bolt tear-out can then be found along the direction of the force. Though this proce-
                                    dure (Muir and Thornton, 2004) is too complex to show here, it results in an effective bolt value
                                    of 24.8 kips. Thus,

                                                      φR n = 2.06 × 24.8 = 51.0 kips ≥ 51 kips  OK

                                    Determine maximum plate thickness to ensure connection ductility at bolts: The maximum nom-
                                    inal strength of a 1-in-diameter A325X bolt (with the 1.25 factor discussed in Art. 3.1.5) is


                                                                     1
                                                                 ×
                                                                             .
                                                              .
                                                          R = 125 60   2 π  = 58 9 kips/bolt
                                                                     
                                                           n
                                                                     2
                                    For the “moment only” condition, C′= 26.0 from AISC Table 7-9. This results in a moment M of
                                                            M = 58.9 × 26.0 = 1530 in⋅kips
                                    The maximum plate thickness of


                                                            t pmax  =  6 M  =  ( 6 1530 )  =  . 128 in
                                                                 FL 2  50 12  2
                                                                         ()
                                                                  y
                                               1
                                                                                              5
                                    A plate up to 1 / 4-in-thick is allowed for ductility. Thus, proceed with checks for  / 8-in-thick plate.
                                    Design strength for interaction of shear and bending in plate:
                                                                        51 0
                                    • Shear stress on gross section of plate  = f v  =  0 625 . ×12  = 6.80 ksi
                                                                       .
                                    • Plastic section modulus of gross section of plate  = Z gross  =  . 0 625 4 ×12 2  = 22 . in 3
                                                                                           5
                                                                                  .
                                    • Bending stress on gross section of plate  = f b  =  51 0 . 22 5 . ×10 5 .  = 23 8 ksi  2  2
                                                                                                       ≤
                                                                                            23.8
                                                                                   6.80
                                                                                  ×
                                                                                     ×
                                                                                             ×
                                    • Shear and bending interaction on gross section of plate = ( 0.9 0.6 50  ) +( 0.9 50 ) = 0.343 1
                                    • Shear stress on net section in plate = f v  =  0 625 (  51 0 . − ×1 125)  = 10 9 ksi
                                                                                    .
                                                                     .
                                                                        × 12 4
                                                                             .
                                    • Plastic section modulus of net section of plate  = Z net  = 22 1 − (  . 1 125 ) = 14 .  in 3
                                                                                            1
                                                                                .5
                                                                                     3
                                    • Bending stress on net section of plate = f b  =  51 0 . 14 1 . ×10 5 .  = 38 0 ksi
                                                                                .
                                                                                 10 9 .  2  38 0 .  2  ≤
                                                                                    ×
                                                                                             ×
                                                                                           .
                                                                                .
                                    • Shear and bending interaction on net section of plate = ( 075 06 65  ) +( 075 65 ) = 0 746 1.
                                                                                 × .
                                    Plate buckling:
                                                     LF y                      12 50
                                          λ=                      =                            =  0 468
                                                                                                 .
                                                                              +
                                             t  47 500  +112 000,  (/  2  0 625 47 500 112 000 12 2 10 5)] 2
                                                 ,
                                                                                     [/
                                                                                         (
                                                                                           .
                                                             L e 2 )
                                                                     .
                                                                           ,
                                                                             0
                                                                                  ,
                                              p
                                    Since λ= 0.472 ≤ 0.7, buckling does not govern.
                                                                            5
                                    Size weld: For ductility, the weld size must be equal to  / 8 t p = 0.625(0.625) = 0.391 in. Therefore,
                                       7
                                    use  / 16-in fillet welds. Checks show that the welds meet design strength requirements for shear
                                    and bending.
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