FIELD: transport.
SUBSTANCE: invention relates to connection of aircraft fuselage section with adjacent section. Fuselage element contains the first section. The section includes plating and connecting devices made with possibility of connecting the first section with adjacent second section. The section goes along fuselage longitudinal axis. Fuselage element also contains stiffening elements (stringers) passing along longitudinal axis. Herewith, end of longitudinal stiffening element goes out of free edge of the first section plating for predetermined length.
EFFECT: simplification of fuselage sections assembling, force transfer between sections, lower mass.
14 cl, 4 dwg
