To see only the CAD and FEA images, click here to go to this projects section in the CAD Portfolio
Introduction
I worked with Peter to do this. We worked on seperate ideas: Glue vs Fasteners, and both made CAD Models and did FEA. We both wrote and edited the report.
Material Properties of the Given Mateials
Young’s Modulus | Yield Strength | Poisson’s Ratio | Density | |
---|---|---|---|---|
PMMA | 3.1 GPa | 70 MPa | 0.35 | 1.19 g/cm3 |
AA110-O | 68.9 GPA | 34 MPa | 0.33 | 2.77 g/cm3 |
Epoxy | 3780 GPA | 16.7 MPa | 0.35 | 1.16 g/cm3 |
Creating the Design
3D Model with Dimension:
ANSYS Set Up and Results:
ANSYS Mesh | ANSYS Forces | ANSYS Results |
---|---|---|
Mesh of the joint. The mesh was refined around the holes seen here, and at the epoxy layer hidden from view. |
A force type load was applied at the PMMA loading hole, seen as a red vector. A fixed support was applied at the other loading hole, indicated as ‘A’. |
Maximum stress at the loading holes. Other points of interest were the thin arms about the hole, which had a larger deflection. |
Convergence of Stress
Graph | Table with Numbers |
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Physical Test Results and Future Work
We decided, due the brittle nature of the acrlic and due to the fact we were designing to ultimate failure, we should have used a flexible bonding material. For example, a foam tape. We also should have reduced the area on the acrylic that would have attached to the aluminum plate.
Fracture | Potential Changes to Shape |
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Notes:
Mainly just images - more work to come.