A CURVED LAMINATED STRUCTURE

With the present invention, there is provided a curved laminated structure (D) suitable for use in aviation industry comprising at least one upper layer (D1) positioned on the inner radius surface, at least one lower layer (D2) positioned on the outer radius surface of the curved laminated structure (D), and at least one intermediate layer (D3) positioned between the said upper layer (D1) and lower layer (D2), characterized by comprising: at least one fiber bundle (1) consisting of unidirectional fibers, which is positioned at an upper side of the intermediate layer (D3) facing the outer layer (D1) and on the curved laminated structure (D) in the longitudinal direction, in order to ensure strength, by means of elongation stiffness, against deformation induced by the growth of an inner angle in the region of a bend of the said curved laminated structure (D) and resulting from a tensile force applied on the curved laminated structure (D), and at least one adhesive tape (2) lying on the bend region of the curved laminated structure (D) and on the intermediate layer (D3), along the width of the curved laminated structure (D), in order to prevent propagation of a possible delamination crack within the said curved laminated structure (D) and between the layers.