FIELD: transport.
SUBSTANCE: invention relates to aircraft prefabricated wing skin panel and to method of its production. Proposed panel comprises skin panel with aerodynamic profile surface on one side and, on the other side, it has attachment surface to accommodate fasteners for wing structural elements. Said attachment surface is provided with two opposed ledges to make mounting channel. Wing structural element has first and second flanges to be clamped in said mounting channels by aforesaid opposed ledges. Said wing structural element is mounted in aforesaid channel by cold interference fit.
EFFECT: lower weight at sufficient wing strength.
18 cl, 5 dwg
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