Analysis: Linear Static
Basics: Two members (L bracket and Plate) connected with bolt connecter with 4 holes, 9 mm clearance holes.
Bolt connector: Picked edges of holes to create, Preload applied about 4500 lb.
Constraints: One of a member has big surface, split a surface and added fixed constrain. (not near the load path)
Contact: Separation between two members.
External Force: 1 lb., just for sake of running model. (Adding external force increase stress more)
Meshing: Generalized mesh and local control on bolt bearing surface area 0.08-inch mesh.
Results: Max stress near the bolt surface area below bolt head, in the range of 300 KSI.
Observed similar FEA on web running without any issues.
https://www.youtube.com/watch?v=KpVdgtdCF68
https://www.youtube.com/watch?v=UAk9mUe9Ya4
Thanks for reviewing and your help.
@John_Holtz Hi John, noticed you have great knowledge in Nastran. Tagging you to refer to my query if you could help. Really appreciate it.
Hi @apatel4FM8K . Welcome to Inventor Nastran.
The answer is to ignore the high stress. It is not possible to get accurate results underneath a bolt head using a bolt connector. The bolt connector only gives accurate loads transferred so that other areas of the model are accurate.
Also see Why do stresses keep going up when the mesh is refined in Nastran. The issue with the bolt connector is similar.
John
@John_Holtz Thank you for your quick response, John.
The only thing I can't understand is why it's behaving normal for others as I attached in those videos?
We use Inventor Professional 2022.5.3, and Nastran version is 2022.3.0166. (Attached Screenshot)
Hi @apatel4FM8K
I so not have any experience with SolidWorks simulation, so I cannot comment on how they avoid high stresses where their bolt connector attached to the model in the Solidworks video.
For the Inventor Nastran video, I think it was created by frequent contributor @lucmartzz . To me, it looks like the legend scale was changed to cap the maximum value to 100.0 and 150.0 instead of showing the maximum stress of xxx.x. (From the ribbon, "Results > Options > Contour Options > Set Min/Max".) Also, the Min and Max markers are hidden to not show that the maximum result is xxx.x.
John
@John_Holtz Sounds good John. I'll neglect the stress below bolt heads in that case. Thank you for being responsive and providing information quickly, it does help a lot and saves my time.
@apatel4FM8K if you check closely my video you can see that I'm including a preload on the bolts setup, as mention by @John_Holtz you can ignore those areas of stress.
Thanks for confirming @lucmartzz. Appreciate you all actively providing information here. 😊
I have a follow up question that I think ties in with this. I understand that the preload stresses can generally be ignored, but if I'm trying to do a non linear analysis with plastic deformation, I feel like this might be causing me issues. Stresses that high are going to cause significant plastic deformation around the bolt head, which I think might be one of the reasons my analyses are failing to complete. Is there a better way to model a bolted joint with preload in a non-linear analysis with materials that yield?
Have you given try to any of these options. Just a suggestion, I haven't used them.
How to apply a bolt preload to a solid modeled bolt in Inventor Nastran
Sort of. I have tried using the "split bolt" (the third option on that link), but I ended up with so many contact surfaces and constraints that I had a different issue when trying to run the model. I'm a bit worried that either of the other two options would have a similar problem.
Any my apologies, I meant to reply to the thread as a whole, not specifically to you, but I appreciate the response either way!
For my tutorial I also ran nonlinear analysis to find out if the results was going to be different. (https://www.youtube.com/watch?v=UAk9mUe9Ya4) but I had no problems of convergence.
I have never tried to reduce (or eliminate) the stress at the bolt connector. These may help or not help enough.
John
John can explain more, but my two cents, you want the bolt connectors with applied preload. Applied preload changes the stiffness of your Joint connection & assembly, allowing the load to transfer to your members and not fully pass the load on the bolts.
You can find the max preload to be applied by considering proof load of member/bolt and factor it for temp or permeant connection. That gives you max stiffness in the assembly without yielding anything, allowing the stress to distribute amongst members.
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