FIELD: aviation.
SUBSTANCE: invention relates to aircraft, particularly, to coupling between outer skin and aircraft stabilizer or wing panel. Proposed aircraft comprises wings and stabilizer comprising torsion-box comprising side members and outer skin jointed with said side members. Wings and stabilizer also contain panels containing outer facing sheet and inner facing sheet. In longitudinal direction outer facing sheet ends on free outer edge. In longitudinal direction inner facing sheet ends on free inner edge. Said panels also include a filler arranged to form a sandwich structure between the outer facing sheet and the inner facing sheet. Inner facing sheet comprises cantilever part. Cantilever part forms free inner edge. Cantilever part is attached to outer skin of caisson part.
EFFECT: higher strength of the structure.
37 cl, 7 dwg
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