Modelling a joint in a threaded rod, joint, nut and washer assembly

AI Thread Summary
The discussion focuses on modeling a joint assembly consisting of a nylon insert nut, threaded rod, washer, and a joint made of three plates, with the aim of comparing computer modeling stress results to hand calculations using the frusta cone method. The user reports unsatisfactory results from ANSYS 14.5, expressing confusion over the stress distribution expected in the model. They seek clarification on whether the assembly will generate a clamping force and inquire about the applicability of specific equations related to preload tension and required torque. The user has shared a model file for further assistance. Overall, they are looking for guidance to resolve their modeling issues and validate their calculations.
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I am trying to use computer modelling to see stress. I want to compare it to my hand calculation, which uses the frusta cone method to find the stiffness of the joint. This way, I can check my calculation in a conceptual way.

The model includes a nylon insert nut, a threaded rod, a washer and a joint (some people refer to the joint as a member).
I wanted to model these parts as solid for realism.
The member is made of three plates. Only the plate furthest from the washer is threaded.

The results that I get using ANSYS 14.5 are garbage and I cannot understand why (see the attachments for the model, boundary conditions and results). All contacts are set to 'bonded'. There should be a cone of stress, less at the top member, more to the middle, less at the bottom member. Please help.

Here is the model (630 kB):
https://www.dropbox.com/s/50od9jnfx507s8u/model.zip?dl=0
or use:
http://www.filedropper.com/model_3

Will a threaded rod / washer / nylon insert nut / threaded member actually produce a clamping force? Its hard to picture that in my mind.

Does the following equation apply to this situation:

F = 0.75 * Sp

Where F is the preload tension, resulting from the nut being tightened on the threaded rod.
Where Sp is the proof strength of the stud.

T = KDF

Where T is the Torque required to produce the force that clamps the assembly together
Where K is the nut factor
Where F is defined as before.

Thanks.
 

Attachments

  • Boundary conditions.jpg
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  • Error.jpg
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  • mesh.jpg
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  • stress.jpg
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  • flexible.jpg
    flexible.jpg
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