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FEA of welded constructions 2

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netjack

Mechanical
Jul 11, 2001
13
Hi all,
We simplify our FE model (shell and beam elements) for welded constructions to analyze the entire system. That means we model welded parts as uni-block (i.e. continous parts). After this global analysis, we will analyze the welded parts by incorporating the weld as well in detail. But, analyzing only a small region at a time and in 3D.

1. Is this method correct?
2. There is Weaver company which has FE Weld tool. It reads shell FE results and predict necessary weldings. I don't want to design the welds but want to know whether the current welds are OK or not. How can I do that?

Regards
 
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netjack,
your question is actually very wide ranging and there is no one answer - or rather the answer is "it depends on ..."

1) What you are designing and the types of welds. This will influence if there is a design code (eg British Standards, API ..) available.

2) The factor of safety that is required, do you need a minimum weight design. If you do then design codes may not be the best way to go.

3) What are the modes of failure that are being designed for. Static strength, collapse load, fatigue, creep ... All of these will require different approaches.

4) Are weld defects being assessed?

As an example if you are designing against fatigue failure using BS7608, only nominal (direct and bending) stresses are required and so the global shell model will be sufficient.

Be more specific and I will answer in more detail

Best wishes
TERRY [pc2]
 
netjack: (1) In general, I'd say your method is correct. Joint analysis is often nontrivial, to say the least, and any suggestions from anyone to streamline the process economically for a very large, shell-element global model are appreciated. The local model is necessary where global model joint geometry does not reasonably match actual joint geometry general configuration. How do you get loads applied accurately to boundaries of your local models? Mapped 3-D, nodal, enforced displacements?

(2) No comment on this product, except it sounds like it might give completely wrong answer if global model joint geometry does not reasonably match actual joint geometry general configuration.
 
Yes ..it is correct,provided you analyse the welds with appropriate boundary conditions.The actula loads acting in the welded region can be obtained from the stic(beam)model and applied on the 3D model.

U need to model the actual welds(including any deterioration in them in service,if already put to service)and do 3D analysis.Get the maximum stresses and compare with the allowable stresses to know the adequacy or otherwise of the welds.This method gives best results,though it requires some effort.No pains no gains!

Best Wishes
 
There is another way to do this, provide say 0.1mm distance between surf.1 and surf.2 and model 3d weld with say 0.5mm in diameter at your actual location and length and perform 3d analysis.

 
I would suggest the FEMFAT software. This can anylize several different weld seams from the fatigue side. I think this is the best fatigue software!
 
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