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oltimer -> RE: Palmer 132" C-130 Build (6/9/2007 1:15 AM)
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Hi Mike; The part number for the Aerospace Composite Products 1 1/4 I.D. x 0.062 wall thickness x 70" is "TUR-13A". This is what they call a "roll wrapped carbon tube which makes it VERY strong! The normal tubing is laid up with the fibers laying lengthwise around a mandrel. For the roll wrapped tube the fibers are flat like a ribbon and rolled around a mandrel. That is why it is more expensive than the "unidirectional" tubing. My spars are a wood/carbon fiber lamination. First I spliced the spar wood so that it was a continuous spar six feet long! I then applied epoxy laminating resin to the wood and put a long strip of Saran Wrap on the work area (to catch the mess) and put the carbon fiber strip on the WIDE (1/2") side of the spar. Clamp or weight it down overnight or until the epoxy cures thoroughly. The spar should be clamped or weighted down as straight as practical. It doesn't have to be perfect, but it sure helps. I only used the carbon fiber on the front spars. The rear spars don't need it. The part numbers for the two DIFFERENT parts I used are as follows: "CLT3-62" described as 0.042-0.007" x 1/2" x 72". You will need 2 of these. They are used for the lower spar! The part number for the second strip I used is: "CLT4-62" described as 0.084-0.014" x 1/2" x 72" . You will also need two of these. When you are finished you will have four pieces of wood/carbon laminate, each 72" long. Each spar will be 144" long laid end to end. When you build the center section you will use all four spars with the thick end at the center of the assembly. Cut each spar at the end of the assembly and use it for the outer panel. Don't cut off too much excess or the spar will come out short for the outer panels. Measure, measure, measure! Be aware that you will have to deepen the rib notches for the front spars by the extra thickness. A 1/2 wide sanding stick works great! The reason that the thicknesses are different is that the carbon fiber strips don't like compression loads so the THICKER SPAR IS USED ON THE TOP OF THE WING!!! That is because it is in compression when flying. The THIN strip is used on the BOTTOM spar. Also, Mike I forgot to answer your question regarding the "TEE" shaped parts in Pic #6. I just traced it off of Sheet #1 of the plans and made a paper template then cut them out of 1/16 plywood. You obviously need two. Look between Formers #14 and 15 you will see the drafting symbol for wood-wavy lines. Move up to the wing cross section and you will see that the wood branches out just above the top of the side frame between the front and rear spars. It follows the top of the airfoil for the same distance between the spars. I used carbon paper to make my template. It should fit somewhat snug between the spars and then the lower end should fit snug between the formers 14 and 15. If you use the drawing the 5 degrees incidence comes out fairly close-between 4 and 4.5 degrees. I use a Craftsman 24" digital level that has 0.1 degree snesitivity which is pretty close for this operation. Happy Flying, Frank
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