FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering and may be used for production of aircraft fuselage element section. Shell segment comprises skin panel with lengthwise stiffness elements, crosswise stiffness element extending across lengthwise stiffness elements and connection angle with crimp arranged on said skin panel. Said skin panel and lengthwise stiffness elements are made of plastic reinforced by carbon fiber.
EFFECT: decreased weight, lower probability of ring frame turnover and flexure.
12 cl, 4 dwg
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