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  • All materials in now for first initial trial of 3 ribs

  • Waiting for new rib spacer CAD for manufacturing

  • 8 ribs with a negative 0.175mm tolerance (for laser cutting)

    • Easiest way seems to overshoot the negative tolerance and sand down until we get the desired fit

  • DWG of ribs found in:

    • WARG_CAD\Fixed Wing\Fixed Wing Design\Wings\DWG

    • FW_WINGS_P006_RIB_UPDATED.dwg is the original file

    • FW_WINGS_P006_RIB_UPDATED_4INx36IN_SHEET_0.175MM_TOLERANCE.dwg is the file I created with 8 ribs and the tolerance applied → This is the file I’ll give to the RPC

Author: Nathaniel Li Date:

Initial Wing Manufacturing Trial

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  • 1/16” ribs are too thin → 1/8” or even 1/4” should be tried

    • Fragile and break easily when sanding and assembling

    • Ribs warp and deform from shrinkage of ultracote

    • Very little surface area for bonding to ultracote

  • -0.175mm tolerance for laser cutting can be reduced to -0.1mm and 0mm in future tests to get a more precise fit

    • Sanding is almost always inevitable

  • LE and TE covers work

    • Doesn’t melt even at high temp of 350F (used CF PETG but ABS should be fine)

    • TE cover is pretty small → make larger (further back on chord)

      • Easier manufacturing

      • Prevent top and bottom layer of ultracote from sticking together

  • Need to use rib spacers on spar for even spacing

  • Iron works well but shrinking technique can be improved

    • At lower temp of 242F, adhesive starts melting and is pretty easy to deal with

      • Risk of burning and over melting is rare; just keep the iron moving

      • Best to slightly tension each section as you iron it

    • At higher temp of 350F (shrinking temp), it can be harder to work with and requires special attention

      • Staying in one spot for even slightly too long will overshrink

      • Gets rid of almost all wrinkles

      • Best to slightly tension each section as you iron it

      • A little concaving as shrinking starts

        • Causes: Thin ribs, not enough tensioning

        • Can possibly be mitigated by tensioning more during shrinking

  • Need sharper knives or xacto knife to make cleaner edges/seams

  • Overall feedback about process:

    • Long and tedious process to make

    • May not be suitable for small control surfaces (like ailerons and stabilizers)

    • Any mistakes accumulate and require a full redo to correct

Design Changes

  • Thicker ribs definitely needed

  • Super simple and lightweight internal spacers (for manufacturing)

  • Jig for manufacturing wing?

    • Holding the larger full size wing can be tiring and difficult

  • Larger overall wing (changing height/thickness of rib)

    • Prevent sticking of top and bottom layer of ultracote

    • Fit servos and other components

Author: Nathaniel Li Date:

Overall Size Increase

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  • Increased the size of ribs (and appropriate LE and TE spacers) to have a 50% larger footprint

  • This should help accommodate components like servos

  • Still retains the NACA 4412 profile