FIELD: aircraft industry.
SUBSTANCE: wing of an airborne vehicle has a first panel, a second panel, ribs connected between the first and second panels, and stiffeners connected between the ribs in the direction of the wingspan and connected to the first panel. The connection between the stiffeners and the first panel prevents the stiffeners from receiving axial loads, and the stiffeners increase the first panel’s compression resistance. The connections between the stiffeners and the first panel are indirect connections formed by clamps, which are designed to prevent axial loads by the stiffeners while ensuring an increase in the resistance of the first panel to compression. The connections between the stiffeners and the first panel are indirect connections formed by clamps, which are designed to prevent receiving axial loads by the stiffeners while ensuring an increase in the resistance of the first panel to compression. The flight method is characterized by the use of the airborne vehicle’s wing.
EFFECT: group of inventions is aimed at stability improvement.
13 cl, 16 dwg
Title |
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Number |
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