FIELD: transport, aviation.
SUBSTANCE: proposed device comprises strip 1 and counter strip 2. The latter has jointing points (M, N) smaller in number that the strip jointing points (PQ). First 3 and second 4 structural elements are interjointed between strip 1 and counter strip 2 at jointing points (M+N), their number being smaller than that of jointing points (P+Q) on strip 1. One of structural elements is made from composite materials. The structure comprises the strip jointing device and features first and third structural elements 3, 8 represent the parts of the abutting surfaces of box structure 9. The proposed method includes assembling box structure 9 from structural sheets 3, 8 made from composite materials and the strips jointed together with the help of remote attachment point (Q1). Wing element 4 is rigidly attached to aforesaid box structure.
EFFECT: simplified jointing box structure to aircraft wings.
6 cl, 2 dwg
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