FIELD: aircraft engineering.
SUBSTANCE: proposed panel comprises skin with smooth flat geometrical shape of outer surface secured to frame structures. The latter are composed of a system of crossed ribs secured to said skin. Said system of ribs consists of unidirectional high-strength (high modulus) threads and/or fabric secured by polymer binder and oriented along geodesic lines on the skin inner surface. Thickness and height of said ribs differ.
EFFECT: decreased weight, higher rigidity and stability in operation.
5 cl, 2 dwg
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