Fillet Welds Loaded in the Plane of Part Joins

1. Loading by axial force F x

Resultant Shear Stress

where:

 

F x

axial force [N, lb].

 

A

throat area of the weld group [mm 2 , in 2 ].

2. Loading by bending moment M

Shear stress in the weld investigated point

where:

 

u

constant

   

- for calculation in metric units u = 1000

   

- for calculation in English units u = 12

 

M

bending moment [Nm, lb ft]

 

r

radius vector of investigated weld point related to the weld group center of gravity [mm, in]

 

J

polar moment of inertia of weld group [mm 4 , in 4 ]

3. Loading by bending force F Y

In any weld point, a stress caused by shearing force F Y and bending moment M F originates. Its size determines the formula:

M F = F Y r F [Nmm, lb in]

where:

 

F Y

bending shearing force [N, lb]

 

r F

arm of bending force to the weld group center of gravity [mm, in].

Shear stress caused by shearing force

where:

 

F Y

bending shearing force [N, lb]

 

A

throat area of the weld group [mm 2 , in 2 ].

Shear stress caused by bending moment

- stress x-component

- stress y-component

where:

 

M F

bending moment [Nmm, lb in]

 

r Y

distance of investigated weld point to the weld group center of gravity in the y-axis direction [mm, in]

 

r X

distance of investigated weld point to the weld group center of gravity in the x-axis direction [mm, in]

 

J

polar moment of inertia of weld group [mm 4 , in 4 ]

Resultant shear stress in the investigated point of weld

where:

 

τ XM

x-component of shear stress caused by bending moment [MPa, psi]

 

τ Y

shear stress caused by shearing force F Y ' [MPa, psi]

 

τ YM

y-component of shear stress caused by bending moment [MPa, psi]

4. Loading by common force F

In any weld point, a common force F causes adequate stress to the stress which would arise by combined loading from bending moment M F and the pair of shearing forces F X ', F Y ' with action point in the weld group center of gravity, while applies:

M F = F r F [Nmm, lb in]

F X' = F cos ϕ [N, lb]

F Y' = F sin ϕ [N, lb]

where:

 

F

acting force [N, lb]

 

r F

arm of bending force to the weld group center of gravity [mm, in]

  ϕ

direction angle of acting force [°]

Shear stress caused by shearing force F X'

Shear stress caused by shearing force F Y'

where:

 

A

throat area of the weld [mm 2 , in 2 ]

Shear stress caused by bending moment

- stress x-component

- stress y-component

where:

 

M F

bending moment [Nmm, lb in]

 

r Y

distance of investigated weld point to the weld group center of gravity in the y-axis direction [mm, in]

 

r X

distance of investigated weld point to the weld group center of gravity in the x-axis direction [mm, in]

 

J

polar moment of inertia of weld group [mm 4 , in 4 ]

Resultant shear stress in the investigated point of weld

where:

 

τ X

shear stress caused by shearing force F X' [MPa, psi]

 

τ XM

x-component of shear stress caused by bending moment [MPa, psi]

 

τ Y

shear stress caused by shearing force F Y ' [MPa, psi]

 

τ YM

y-component of shear stress caused by bending moment [MPa, psi]

5. Calculation of comparative stress σ S

Comparative stress is determined from calculated partial stresses according to the formula:

while for the x-component of stress that actuates in the investigated point of weld, perpendicularly to the weld direction, the α X = α 3 formula is applied. In the opposite case α X = α 4 . The same applies for the y-component of the stress actuating perpendicularly to the weld direction, that is α Y = α 3 or α Y = α 4 .

where:

 

τ X

shear stress caused by shearing force F X' [MPa, psi]

 

τ XM

x-component of shear stress caused by bending moment [MPa, psi]

 

τ Y

shear stress caused by shearing force F Y ' [MPa, psi]

 

τ YM

y-component of shear stress caused by bending moment [MPa, psi]

 

α 3

conversion factor of weld joint for fillet end weld [-]

 

α 3

conversion factor of weld joint for fillet end weld [-]