FIELD: aircraft.
SUBSTANCE: invention relates to highly loaded structures of polymer composite materials of aircraft. Joint assembly of the air frame elements of the aircraft from the polymeric composite materials includes panels of the wing box or stabilizer arms, containing longitudinal stringers and a transverse power belt made of criss-crossed bundles of unidirectional carbon filaments impregnated with a synthetic binder disposed in layers, with an overlap in the area of the cross-hairs. Power belt is provided with a connecting element made in the form of a metal bracket, which surrounds the inner base with a cross-sectional power belt of the wing box or stabilizer console and remote elements fastened to the power elements of the fuselage center wing by a fastening element.
EFFECT: invention is aimed at obtaining a high-tech design of a node for connecting elements with increased reliability and strength.
1 cl, 4 dwg
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