Composite structure and method of making

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

52249, 523091, 5230914, 138144, 156173, 244133, 428 36, B64C 100

Patent

active

042302935

ABSTRACT:
An elongate hollow structure with a plurality of reinforcements arranged in a pattern and acting as spacers between a pair of skins. The skins are of resin impregnated wound filaments with reinforcing strips of facing preimpregnated wound filaments that crisscross at the spacing reinforcements, abutting panels extend between adjacent reinforcing spacers to fill the space between the skins, and the structure is bonded with resin into a composite structure.

REFERENCES:
patent: 1307002 (1919-06-01), Fowler
patent: 3989562 (1976-11-01), Hladik et al.

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