FIELD: aviation.
SUBSTANCE: present invention generally relates to aircrafts and, in particular, to aircraft wings and corresponding elements operating on shear and stretching. An aircraft wing contains the first panel connected to the second panel to form a wing caisson, a stringer located along the wing span inside the wing caisson directly next to at least one of the first panel or the second panel, a rib located along a chord inside the wing caisson, wherein the rib contains an element operating on shear and stretching, including a wall, a bar connected to the wall, and the first and the second supports passing in opposite directions from the central part of the bar and protruding outward from the central part of the bar in the direction along the chord so that far ends of the first and the second supports are placed at a distance from the wall. In this case, the first and the second supports are connected to the stringer and/or the first panel or the second panel. The group of inventions also relates to an alternative embodiment of the aircraft wing, as well as to a method for assembling the aircraft wing.
EFFECT: group of inventions is aimed at creating aircrafts that include wings having elements operating on shear and stretching, which reduce the number of gaskets used in the assembly of the aircraft wing, and/or eliminate the need for their use.
14 cl, 20 dwg
