Design of a Carbon Fiber Composite Monocoque Chassis for a Formul.pdf

Potential Process for locating points and installing Torlon inserts:

Tldr: used a cmm to divot and mark location, drilled holes, removed core, inserted torlon insert and epoxied with a gun

  1. Composite coque is complete (two halves of the female mold are joined via a lap joint)
  2. Used a CMM to probe and divot the hole location (divot helps create a seat for actual drilling later)

3.a. Drilling method 1 (CNCdrill available):

3.b. Drilling method 2 (hand drill):

  1. Drill through full sandwich panel
  2. Bore out core material around hole creating a hollow donut cavity (they used an allen key placed in a drill), leaving both carbon skins intact (purpose of this step is to provide more epoxy bond area by clearing out core around hole)
  3. Slide Torlon insert through hole so its flanged lips sandwich both skins
  4. Inject epoxy into one port until it exits the other, cavity is now fully filled and insert is locked
  5. This results in a solid reinforced load bearing hardpoint that won't crush or pull through