Design ultralight and strong metamaterials
Loading...
Date
2017
Journal Title
Journal ISSN
Volume Title
Publisher
University of New Brunswick
Abstract
A new technology emerging in today’s world is additive manufacturing with steel.
Investigating how different micro-lattices perform under different loading conditions is a
key component for implementing this new technology into every day mechanical
components. This project looks at how five different micro-lattices perform under the
four standard modes of loading and a combined loading scenario. The four standard
modes of loading are tension, compression, pure shear, and bending. The combined
loading scenario consists of combining shear and compression.
The material properties of the EOS MaragingSteel 1 material need to be
determined prior to performing computer simulations. Test specimens need to be
machined down to the appropriate specifications, known as the dog-bone. These test
specimens are designed to fracture at a specific point so that stress, strain, yield stress,
and ultimate tensile stress can be determined. The axis in which the test specimens are
printed must also be considered as some material properties may change.
The project includes a mechatronics component that involves embedding a strain
gauge sensor along the exterior bounds of the lattice. The starting point for the strain
gauge is a hard-wired unit which is then modified to communicate the data wirelessly.
This would provide useful information during the testing of a final micro-lattice structure,
and also demonstrate how this could be used in industry to monitor parts that are
currently in service.
The results of all computer simulations were reviewed and the octet-truss microlattice
was chosen, because overall it has the preferred performance characteristics under
the different loading conditions. The final micro-lattice will not at this time be printed
due to financial restrictions. The test results from the physical micro-lattice specimen
would have been compared to the results of the computer simulations, in order to verify
the simulations. The octet-truss, diamond, pyramid, block lattice truss, and cubic truss
unit cells were modeled and built into micro-lattice structures using Autodesk Inventor
and Fusion 360. For the simulations of the loading conditions, the constraints and the
loading conditions for the lattices were applied to the models using Fusion 360, and the
simulations were performed using the Autodesk Nastran software.