Saturday, July 11, 2015

Analysis and Design of the Fastener

Analysis and retrofitting design of the fastener group for the spreader                 

                                         bar of SM3 disassembly 


Background:
      Try to re-use (or to modify) the existing Mino project spreader bar for SM3
      disassembly project. the capacity of the spreader bar for SM3 project is:
               Overall load Pt = 9.4 tons with span distance Ls = 201 in
               
Applicable codes:
      ASME B30.20; “Below – the – Hook Lifting Devices”
      ASD, AISC 9th edition
     
References:
      ME – 397459
      ME – 397426
      MD – 397452
      “Steel Structures Design and Behavior” by C. Salmon & J. Johnson, 3rd edition

Assumptions:
      Slip critical  connection, single shear
     
Figure 1 of  page 1 is showing that when the applying load P is eccentric to the centroid of the bolt group, this physical configuration is the actual design of the spread bar using for sm3 project.
  

                
Where:
       P = 9,400 lbs, applying load
       L = 47.625 in
       Location A is the geometrical centroid of the bolt group, 6  bolts are located as
       showing in Figure 1. currently, it is assuming: A325, ¾ - 10, UNC
       n = 6
       per Table I –D, part 4 of ASD,  Rav = 7.51 kip (allowable shear load)

Find out the local properties of the fastener group:

      ∑x2 =  4 (4)2 = 64 in2
         ∑y= 6 (2)2 = 24 in2
      ∑x2 +  ∑y2    = 88 in2

The primary shear load Rv of each bolt subject to the applying load P:

     Rv = P/n = 9,400 lbs / 6
          = 1,567 lbs ↓

The secondary torsional shear load of the bolt subject to the moment PL:
   To pick the bolt of the most right top one as showing in figure 1,

Where: Rx = PLy ÷ (∑x2 +  ∑y2)
                  = (9,400 lbs) x (47.625 in) x (2 in) ÷ 88 in2
                  = 10,174 lbs. →

             Ry =  PLx ÷ (∑x2 +  ∑y2)
                  =  (9,400 lbs) x (47.625 in) x (4 in) ÷ 88 in2
                  =  20,349 lbs ↓

The resultant force applying to the most right top bolt:

             R = [(Rv + Ry)2 + Rx2 ]1/2            
                 = [(1,567 + 20,349)2 + (10,174)2 ]1/2  lbs
                 = 23,259 lbs > Rav = 7.51 kip

It is necessary to look for:
      a. Different specifications of the fastener with the same fastener group.      
      b. Another pattern of the fastener group

A.Different specification of the fastener with the same fastener group:
     A1. If using 6 bolts with A325, 1 3/8”- 6 UNC,*   
       then Rav = 25.2 ksi > R = 23.26 ksi,
 *:  The hole ctr. to hole ctr. distance Le = 4.0 in < 3d = 4.13 in

    A2. If using same fastener group with bolt of A490, 1 ¼”- 7, UNC,
 then Rav = 25.8 ksi > R = 23.26 ksi (per Table I-D, part 4 of ASD, 9th edition)
 where: Le = 4.0 in > 3d = 3.75 in

B. Modify the current pattern of the fastener group:
    Figure 2 on page 3 is the new fastener group with adding additional 10 fasteners to
           the original group, it can be found the new properties of the fastener group:

      ∑x2 =  (4 (4)2 + 4 (2)2 + 6 (6)2) in2
                   = (64 + 16 + 216) in2
             = 296 in2
      ∑y= (6(2)2 + 8(3.375)2) in2
                    = 115 in2          


                             


          ∑x2 +  ∑y2    = (296 + 115) in2
                                   = 411 in2
              Also n = 16

The primary shear load Rv of each bolt subject to the applying load P:

     Rv = P/n = 9,400 lbs / 16
          = 588 lbs ↓

The secondary torsional shear load of the bolt subject to the moment PL,
To pick the bolt of the most right top one as denoted as bolt A of Figure 2:


Where: Rx = PLy ÷ (∑x2 +  ∑y2)
                  = (9,400 lbs) x (47.625 in) x (3.375 in) ÷ 411 in2
                  = 3,677 lbs. →

             Ry =  PLx ÷ (∑x2 +  ∑y2)
                  =  (9,400 lbs) x (47.625 in) x (6 in) ÷ 411 in2
                  =  6,536 lbs ↓

The resultant force R applying to the most right top bolt A:

             R = [(Rv + Ry)2 + Rx2 ]1/2            
                 = [(588 + 6,536)2 + (3,677)2 ]1/2  lbs
                 = 8,017 lbs > Rav = 7.51 kip

If the bolt material change to ASTM A490, then  Rav = 9.28 kip

             R = 8.017 kip < Rav = 9.28 kip

Since only 2 bolts of the fastener group will experience shear load of R ~ 8.017 kip, all the rest bolt shear load is less than 7.51 kip, so there are two choices:
1.      The most top right and bottom right bolts use A490, the rest bolts use A325. (3/4 – 10,  UNC.)
2.      Or all of them use A490 bolts (3/4 – 10, UNC)

The conclusions:

There are two ways to modify the current fastener group to meet the new design criteria of spreader bar for SM3 disassembly:

1.      Using (6) A490 high strength structural bolts with spec. of 1¼ - 7, UNC (original is ¾ -10, UNC), or
2.      Using (16) A490 high strength structural bolts with spec. of ¾ -10, UNC.