Replacing Parts with Point Mass in an Assembly

In the attached assembly model file, I am only interested in stresses on the shaft. In order to reduce the global mesh size I would like to replace the fan, the motor, and the stator with point masses and apply mass moment of inertias and other boundary conditions associated with them. I know there is a "new mass" B.C. option in the Mecway CCX solver that we could use.

Motor and shaft have steel properties and rotor and stator have nylon nylon material.

I need guidance on how to setup the point masses and apply B.C's.

Any help would be appreciated.


Comments

  • Could you attach either the STEP files or the mesh too?

    For a remote mass with CCX, you can use node-surface coupling and put a mass on the reference node.
  • Step files are attached.
    Thanks
  • edited May 2020
    I see. CCX doesn't have point rotational inertia so I think you'll need to build some structure and position the point masses so they give the required moments of inertia. I would use beam elements to hold them together, though it might be possible to use the node-surface coupling to couple all the point mass's nodes into a single rigid body.

    It might be easier to make simplified solid parts that have the required properties, or maybe just use a very coarse mesh for the existing parts.
Sign In or Register to comment.

Howdy, Stranger!

It looks like you're new here. If you want to get involved, click one of these buttons!