Patent ID: 7708224

Claim:
An aircraft wing comprising: at least one front spar in the region of the front edge of the wing, at least one rear spar in the region of the trailing edge of the wing, a plurality of wing ribs between the front spar and the rear spar, top skin plates and bottom skin plates, a plurality of stringers between the skin plates and the wing ribs, at least one intermediate support arranged between two adjacent wing ribs, at least one fastening lug for fastening a motor, the fastening lug being supported on the intermediate support and located on the side of the lower surface of the wing, and wherein the cross section of the intermediate support comprises a vertical first side part and a vertical second side part at a distance from one another, and wherein at least at the fastening lug there is a bottom part, which is attached to the lower parts of the side parts and is transverse to the side parts, and the fastening lug is fastened to the bottom part of the intermediate support.