Overview of Status of Analysis, Design, Fabrication, Tests, etc.
After meeting with our sponsor, we are thinking about not moving forward with the pin design that connects the anchor wings. Instead, we would like to uses a solid piece of flexible metal.
From a top view, the original design had a rectangular profile. We will be rounding this design to a circular profile that will fit snugly into the cylindrical drill hole.
We have a meeting scheduled with a surgeon for 1 next Wednesday
Accomplishments from Previous Week
New design feature that we feel more confident moving forward with. The pin idea involved too many moving parts, had the potential for jamming, and posed the issue of highly concentrated stress on a weak joint.
Acquired sample sutures, and should hopefully be acquiring sample anchors next week when we meet with the surgeon.
Goals for Next Week (list names after each item). Use specific and measurable objectives.
CAD (Helen) and 3d print (Delta) another iteration of the anchor
Include holes for sutures
Smaller scale
Remove hinge
Finalize Sawbones order and send to Sameer for purchasing - Darren
Finalize testing setup using Instron and Sawbones material - Bryan
Sponsor Comments from Last Meeting and Actions Taken to Address these Comments
Provide updates on individual component analysis (Friday)
Look into clear material to visualize deployment and proof of concept (PDMS)
Sameer said we should finalize our material choice soon. Darren is narrowing down selection by continuing to study materials.
Instructor Comments from Last Meeting and Actions Taken to Address these Comments
Professor had mentioned analyzing the stresses experienced by the pin. Now that we are moving away from the pin design, We need to analyze how the stress will be experienced by the flexible joint.
Target diameter is what soft anchors are right now (1.4-1.8mm)
Risks and Areas of Concern
Clearly seeing the wing deployment
Need a clear material to see what is going on
Resources or Information Required but not Available
Sample anchors
Cadavers
Porosity size of bone
Schedule
Getting to test wing deployment in clear material called PDMS
Fabricating prototype with deployment mechanism
Budget (list amount spent and amount remaining)
$0 spent
$1,100 remaining
Progress on Report and Webpage
Updated background and objective on website