Chapter 10 Canard fabrication
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Another mile stone in the project! In this chapter we build the
first flying surface and get to cut some cores with the hot-wire.
I’ll start right out by confessing that I cut my first
canard
up and put it in the trash. I wasn't careless, it just didn't
go
well. Often times on this project I’ll
get discouraged or
disappointed in how a part turned out, well maybe that
happened once or twice... Usually the next
morning the
sun comes up, the birds start chirping and
things don’t
look too
bad after all! Well that wasn’t
the case on this
one. I slept on it a few nights, talked it
over with my wife
and
…..tossed it. I have never regretted it. The second
attempt went very well, the canard is straight and
true
with no twist and no issues to haunt me.
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Here are some shots of the foam core cutting process, can you see how my wife could have gotten a hair cut doing this?
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Next the
leading edge of each cores are cut off just in front of the spar cap
trough, the aft cores are set up on trailing edge and jigged
straight using string lines and shims to get it
perfect. Aluminum hardpoints for the lift tabs are installed, then the
shear web lay-ups are installed. These lay-ups go from
spar cap
face, over the front edge and back over to the opposite spar
cap face (trough).
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Leading edge cores are microed in place after attaching the lift tabs. I made my own tabs and used 3/16” 2024 T3 al. I wanted them a little beefier than 1/8”. I know 1/8” is more than adequate but if Nat was concerned that we don’t even scratch them I figured a little more material would be in order. Also gives me a little margin should corrosion ever get started.
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Here
you see the bottom skin has been applied, peel ply is put down and wet
out using epoxy
brought up from underneath if possible.
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And I'm done with dis guy!