Making of the carbon fiber landing gear for the Kadet
Senior
Dimensions:
Carbon fiber layer composition:
Construction:
All the above layers were laminated at the same time into a flat sandwich
using West Systems epoxy to fully saturate. Excess epoxy is squeezed out
using paper towels then the whole mess is placed between two sheets of
polyethylene and again squeezed with a wiping action. It is important to
eliminate air pockets. The bundle is then placed on edge into the form
which consists of nails standing vertically in a piece of wood. The outer
layers of continuous .007 CF laminate holds everthing together while the
separated inner sections of .014 allow it to bend at the joints to form
the corners of the gear. Additional nails are added afterward to adjust
the shape as needed. Alignment of the axle mounting surfaces and any desired
toe-in should be carefully checked and adjusted at this time.
Let it cure overnight. Then you can pull it from the form and begin shaping the edges and cleaning up the flash. After the gear shape has been cleaned up there are a few more laminations to be made. First, CF tow is added to the inside corner bends of the gear to build the thickness up to about 3/16" at the axles and to 1/4" at the fuselage corners. The tow is cut to lengths of about 1 to 2 inches to help make a fillet in the inside corners. The tow must be oriented lengthwise to the gear. When this is cured it is shaped to form a smooth fillet. Then sand the whole works. Finally a single lamination of 2oz fiberglass cloth was added to each side of the gear to provide protection to the surface. After sanding the completed gear give it a final thin coat of just epoxy resin to fill the exposed pores of the glass and give it a finished look.