FIELD: process engineering.
SUBSTANCE: invention relates to production of structural element of composite, aircraft wing and fuselage and pre-impregnated flat-sheet laminate. Proposed method comprises forming the laminate including pre-impregnated laminate sheets in the mould. Laminate includes first layer wherein fibers are directed in one direction. First layer first surface crossing aforesaid one direction and second surface crossing said one direction are opposed.
EFFECT: ease of forming, smaller chances of wrinkling.
7 cl, 23 dwg
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