FIELD: aviation.
SUBSTANCE: invention relates to multilayer panels and aircraft fuselage. Corrugated composite skin panel is made of carbon-reinforced simple weave fabric. Said fabric is pre-impregnated with epoxy resin. Layers of fabric layers are selected with orientation of fibres 0/90, with axis oriented to 0° along the corrugation profile. Besides, the panel is made of alternating upper corrugated strips and lower corrugated strips.
EFFECT: higher bending stiffness, strength and reliability.
1 cl, 4 dwg
| Title | Year | Author | Number |
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