FIELD: transport.
SUBSTANCE: invention relates to the aircraft engineering. Claimed structural assembly has the area element with inner and outer plies. Note here that the first surface features a convexed curvature in definite parts with respect to the central zone extending through the area element inner ply while the second surface, opposite the first one, extends parallel with said central zone. Note here that the area element is composed by the aircraft fuselage skin outer structural element, fuselage skin segment or torsion box structure. The area element first or second surface makes the aircraft fuselage skin inner surface, fuselage skin segment or torsion box facing the aircraft fuselage skin inner space, fuselage skin segment or torsion structure, as the as-mounted aircraft integral structural part (10').
EFFECT: decreased weight, simple mounting, sufficient mechanical strength and stiffness.
10 cl, 14 dwg
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