jmggks
Structural
- Mar 16, 2015
- 29
I have a welded knee brace. The knee brace and a beam above it make up a bracket that supports the runway for an automated crane system in an industrial plating machine.
The axial force through the knee brace resolves into compression and shear at the face of the column. Loading on the weld where the knee brace attaches to the column face will be cyclic but not reversed. When I consider fatigue at this location, is my stress range (1) based on the shear component only or (2) based on the scalar sum of the shear and compression loads or (3) based on the vector sum of the shear and compression loads?
My gut instinct is that only the shear matters to fatigue because (A) compression does not cause fatigue and (B) compression is carried by bearing and does not pass through the weld.
I'm looking for reassurance on this. Fatigue seems like a complex subject. Thanks for your comments.
The axial force through the knee brace resolves into compression and shear at the face of the column. Loading on the weld where the knee brace attaches to the column face will be cyclic but not reversed. When I consider fatigue at this location, is my stress range (1) based on the shear component only or (2) based on the scalar sum of the shear and compression loads or (3) based on the vector sum of the shear and compression loads?
My gut instinct is that only the shear matters to fatigue because (A) compression does not cause fatigue and (B) compression is carried by bearing and does not pass through the weld.
I'm looking for reassurance on this. Fatigue seems like a complex subject. Thanks for your comments.