Showing posts with label design. Show all posts
Showing posts with label design. Show all posts

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.