Handbook of Civil Engineering Calculations

(singke) #1
ECCENTRIC LOAD ON A WELDED
CONNECTION

The bracket in Fig. 61 is connected to its support with a Vi-in (6.35-mm) fillet weld. De-
termine the maximum stress in the weld.

Calculation Procedure:


  1. Locate the centroid of the
    weld group
    Refer to the previous eccentric-load cal-
    culation procedure. This situation is anal-
    ogous to that. Determine the stress by lo-
    cating the instantaneous center of
    rotation. The maximum stress occurs at A
    and B (Fig. 61).
    Considering the weld as concentrated
    along the edge of the supported member,
    locate the centroid of the weld group by
    taking moments with respect to line aa.
    Thus m = 2(4)(2)/(12 + 2 x 4) = 0.8 in
    (20.32 mm).

  2. Replace the eccentric load
    with an equivalent concentric FIGURE 61
    load and moment
    Thus P = 13,500 Ib (60,048.0 N); M -
    124,200 in-lb (14,032.1 N-m).

  3. Compute the polar moment of inertia of the weld group
    This moment should be computed with respect to an axis through the centroid of the
    weld group. Thus Ix = (1/12)(12)^3 + 2(4)(6)^2 = 432 in^3 (7080.5 cm^3 ); / = 12(0.8)^2 +
    2(1/12)(4)^3 + 2(4)(2 - 0.8)^2 = 29.9 in^3 (490.06 cm^3 ). Then J = Ix + / = 461.9 in^3
    (7570.54 cm^3 ).

  4. Locate the instantaneous center of rotation O
    This center is associated with this eccentric load by applying the equation h = J/(eL),
    where e = eccentricity of load, in (mm), and L = total length of weld, in (mm). Thus, e =
    10 - 0.8 = 9.2 in (233.68 mm); L =12 + 2(4) = 20 in (508.0 mm); then h = 461.9/[9.2(2O)]
    = 2.51 in (63.754 mm).

  5. Compute the force on the weld
    Use the equation F = Mr'IJ, Ib/lin in (N/m), where r' = distance from the instantaneous
    center of rotation to the given point, in (mm). AtA and B, r' = 8.28 in (210.312 mm); then
    F= [124,200(8.28)]/461.9 = 2230 Ib/lin in (390,532.8 N/m).

  6. Calculate the corresponding stress on the throat
    Thus, S = PIA = 2230/[0.707(0.25)] = 12,600 lb/in^2 (86,877.0 kPa), where the value 0.707
    is the sine of 45°, the throat angle.

Free download pdf