Topic 6.7a: Welded Joints - Example 1

Two steel plates are shown in Diagram 1. The top plate is .5 inch thick and 10 inches wide, and is to be welded to the bottom plate with a 45o fillet weld. The top plate is to be welded completely across end AG and partially along sides AB and FG.

A.) Determine the minimum inches of weld need to carry the 90,000 lb. load and specify how many inches of weld should be placed along each side AB and FG.
B.) Determine the number of inches of weld needed to make the weld strength as great as the plate strength.

The allowable stresses are as follows;
Weld Material: = 15,000 lb/in2 ; t = 24, 000 lb/in2
Plate Material: = 14,000 lb/in2 ; t = 28,000 lb/in2
Dimensions: AB = GF = 20 inches; CD = 4 inches; DE = 6 inches

Solution:
Part 1. We first determine the minimum inches of weld needed to carry the 90,000 lb. load by using the weld formula and setting the load the weld can carry before failing to 90,000 lb..
Pweld = (.707 t * L) *all , or
90,000 lb = (.707 * .5" * L) * 15,000 lb/in2 = (5,300 lb./in.)*L; then solving for L
L = 90,000 lb./(5,300 lb./in.) = 16.98 inches.
This is the minimum inches of weld needed to carry the load, however since the 90,000 pound load is not applied symmetrically to the plate, we can not apply the weld symmetrically. That is, if we try to put equal amounts of weld on sides AB and GF, the weld will fail in this case. To determine how the weld should be distributed, we once again apply static equilibrium conditions.

Part 2. In Diagram 2 we have shown the weld distributed with an amount LAB on side AB, LGF on side GF, and 10 inches of weld completely across the end AG. The lengths LAB , LGF , and the 10 inches of weld must sum to 16.98 inches ( the minimum inches of weld needed). The maximum force these weld can resist with is given by FAB = (5,300 lb./in.)* LAB , FGF = (5,300 lb./in.)* LGF , and FAG = 5,300 lb/in * 10" = 53,000 lb. as shown in Diagram 2.

We now apply static equilibrium conditions to the top plate:
Sum of Forces: 90,000 lb. - (5,300 lb./in.)* LAB - (5,300 lb./in.)* LGF - 53,000 lb. = 0
Sum of Torque about G: -90,000 lb.* (6") + (5,300 lb./in.)* LAB * (10") + 53,000 lb. * 5" = 0
(Notice that the force FGF does not produce a torque about point G, since its line of action passes through point G.)
Solving the torque equation for LAB = 5.19 inches, we can then solve for LGF since LAB + LGF + 10" must sum to 16.98 inches. Therefore LGF = 16.98" - 5.19" - 10" = 1.79" This is how the weld must be distributed in order to carry the 80,000 lb. load (and satisfy static equilibrium conditions).

Part 3.. We assume the plate is loaded in tension, and so the strength of the plate is Pplate = product of cross sectional area of plate and the allowable tensile stress for the plate material, or Pplate = (w * t ) t . We then set this equal to the strength of the riveted joint and solve for the length of weld needed.
Pweld = (.707 t * L) *all = Pplate =(w * t ) t , or
(.707 t * L) *all = (w * t ) t , and then
(.707 *.5" * L) * 15,000 lb/in2 = (10" * .5" ) 28,000 lb/in2 , then solving for L
L = 26.4 inches
This is the minimum inches of weld needed to make the weld as strong as the plate (in tension). We can not state how the weld should be distributed, since we are not dealing with a specific loading.

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