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Folks,
I created some constraints and I am struggling to get the correct results, or should I say what I think should be the correct result.
As you can see above, I created a rigid link between the Pin, Bushes and the Arm. I really wanted to create a pin but for some reason I could not get the results correct either.
What I was expecting to see was some load going thru the pin, but I don't see any?
Any ideas or help ? much appreciated.
Cheers
Chris
Solved! Go to Solution.
Is there a particular reason for analysing the parts as an assembly? As a first pass, just apply appropriate loads to each part individually.
If you are looking for the effect of, for example, pin deflection changing the load distribution on the arm holes, then I think ultimately a contact analysis is probably the way to go. The WL approach could work but will require careful modelling, for example to split the surfaces to avoid applying 'tensile' loads, and to iterate the spring stiffness to give the right results.
Given that you will need the bushes for contact, this looks moderately complex and will require a methodical approach to setting up. One thing to watch out for is under-constrained components - you may well still need to use some WLs and springs to prevent free rotation of the bushes and of the pin, for example.
Give it a go, and post back here if you get stuck!
How many rigid links have you created, and what geometry is each one attached to?
Rigid links are exactly that - rigid - so they will transfer all the load between surfaces they connect, and if they 'bridge' a component then that component will not deflect at all - hence will see no load.
You could use contacts, or you could use a pair of Weighted Links plus a spring for each pair of surfaces. The key question is which parts of the assembly are you looking to analyse? Are you interested in bush surface pressure, or component stresses away from the holes? If the latter, I wouldn't even include the bushes in the model...
I did think about deleting the bushes.
I was looking to analyse the arm, pin and the holes.
When I put in the contacts I got an error but I probably could have persevered a bit more.
Is there a particular reason for analysing the parts as an assembly? As a first pass, just apply appropriate loads to each part individually.
If you are looking for the effect of, for example, pin deflection changing the load distribution on the arm holes, then I think ultimately a contact analysis is probably the way to go. The WL approach could work but will require careful modelling, for example to split the surfaces to avoid applying 'tensile' loads, and to iterate the spring stiffness to give the right results.
Given that you will need the bushes for contact, this looks moderately complex and will require a methodical approach to setting up. One thing to watch out for is under-constrained components - you may well still need to use some WLs and springs to prevent free rotation of the bushes and of the pin, for example.
Give it a go, and post back here if you get stuck!
Thank You for your help much appreciated.
I just felt really I should be able to do it as an assembly. I was looking for the stress in the arm and the pin, I felt I could do this together with the other components in the assembly.
I just can get the connections correct to show the stress in the pin. My calculations by hand show that the pin, arm and housing are close to failure so I felt I could show this in the model.
I have got the contacts set between the parts, but your correct it still thinks its moving. To be honest I am just clicking now!
I have never used the weighted links and springs really before in mechanica. I have only ever used Cosmos all my days and just switch to Mechanica last week so the interface is a bit alien to me.
Yes, what Jonathan says. In other words: rigid links add infinite stiffness to the surfaces you select for the links. Infinite stiffness means: no deformation. No deformation means: no stress. So if you select the entire outer surface of the pin in a rigid link, the pin's outer surface will have infinite stiffness and zero stress.