I am working on the design of the carbon fiber six inch diameter
 tube spar.

 The spar is the heaviest part of the aircraft structure so it pays
 to make it out of expensive carbon. The skins of course can be glass
 or carbon depending how much money you want to spend.


 Paul Lamar

 Paul, I am sure you are aware of the method that Paul McCready used
 to make the carbon fiber spars for the Gossemer Albatross:

 He used Aluminum irrigation tubing (~3-4" D) and laid the carbon
 fiber up on the tubing, then dissolved the Aluminum out with KOH.
 Bill Schertz

 I was called in as an aerodynamic consultant on the one that
 eventually won the Kremer prize by Jack Lambie round about 1976 or
 1977. My girl friend Rhonda and I drove up to the valley to have a
 look. I was surprise to see a propeller about 4 or 5 feet in diameter
 made from two model airplane wings and wire braced. I suggested a
 larger diameter prop not wire braced and further geared down. They
 did that and went on to win the $50,000 prize :-)

 I was not aware he built the spar that way. I was thinking of using
 a metal or plastic tube covered with several layers of garbage bag
 or other thin plastic material cut in long strips. After the epoxy
 is cured the spar can be slipped off the tube. I have done that many
 times on shorter composite tubes. Sometimes the strips can just be
 pulled out from between the surfaces. That gives enough clearance to
 remove the spar from the tube.

 How's the Kiss Cruiser doing? Do you like living up there in the US
 bush? :-)

 Paul Lamar


Paul you can also use braded carbonfibre.
You get it in a flat role with different diameters. This way the "braded fibres" are in a more or less 45 bias in the weave to the span of the spar.
Do 2 layers then dremel cut out of the male plug ( split the carbon pipe) to get off the male plug.
Then do several layers braded over the "first split mould" to the different stations according to the bending loads and specs
Vacume bag each layer as you progress and scuff between layers to get nice finnished surface between layers
Le Roux Breytenbach ZA


One needs some unidirectional fibers on top and bottom of the tube to take the high bending stresses.
These should be  layered with the thickest layers near the center of the wing.

Paul Lamar

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