John_Vreede
Chemical
- Sep 12, 2017
- 9
Hi all. My question relates to a bandsaw blade and its failure mode. Its a 1/2" wide x 0.025" thick blade, tensioned to a given stress level (30,000psi (about 250-300lbwt on the cross section left once teeth are ground in) for a bimetal blade or 20,000psi for a carbon steel FlexBack blade). The back roller guides are about 8" apart and the work presses into roughly the middle of that span. So its a simply supported very slender beam, loaded in the middle, that carries significant tension. In use, the back of the blade deflects upward by about 0.040" while still cutting straight.
I'm assuming the blade, as a beam, will be stable up to a certain load, allowing the blade to cut straight and square, then go into lateral torsional buckling. Then the teeth won't be pointing straight down any more and the cut will veer off from the intended line of cut.
My questions are "Does the tension on the compression side of the blade fall to zero before it deflects sideways? If not what is the limiting factor when it does deflect? Is there any way to calculate the tension on the tension side when it goes into buckling?
Regards - jv
I'm assuming the blade, as a beam, will be stable up to a certain load, allowing the blade to cut straight and square, then go into lateral torsional buckling. Then the teeth won't be pointing straight down any more and the cut will veer off from the intended line of cut.
My questions are "Does the tension on the compression side of the blade fall to zero before it deflects sideways? If not what is the limiting factor when it does deflect? Is there any way to calculate the tension on the tension side when it goes into buckling?
Regards - jv