Minimum weight and high strength framed structure

Details Minimum weight and high strength framed structure Minimum weight and high strength framed structure

B - Operations, Transporting

64

C

18/645, 244/93

B64C 1/00 (2006.01) B29C 44/12 (2006.01) B29D 12/00 (2006.01)

Patent

CA 1059487

ABSTRACT OF THE DISCLOSURE Light-weight aircraft are provided by a light-weight tubular frame- work of metal, e.g. aluminum or magnesium or boron or graphite fibers, includingcables or rods for aileron control, for spoiler aileron control, for flap control, or horizontal stabilizer control, for vertical stabilizer control, for retractorcontrol, for steering control and for landing gear assembly control in selected ones thereof and a foamed plastic adhered to the framework with a smooth hard coating over the foamed plastic. The controls are provided in a protected environment and are placed within the tubular superstructure to provide a more simplified unitary structure. The foamed plastic and the smoother hard coating may be built up in layers at certain stress points.

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