Aerofoil comprising a high lift flap

An aerofoil wing comprising a main aerofoil and a high-lift flap, which is movably arranged on the aerofoil wing by at least two adjustment mechanisms arranged side-by-side in a spanwise direction of the aerofoil wing, each of the adjustment mechanisms having:

• a first adjustment lever, which is hinged to the main aerofoil via a first rotary linkage, forming a first axis of rotation,
• a second adjustment lever, which is hinged to the high-lift flap via a second rotary linkage, forming a second axis of rotation, and
• a central linkage, which links together the first and the second adjustment levers, forming a third axis of rotation,
• wherein the aerofoil wing has a drive device with a drive module mounted on the main aerofoil and movable with respect to the drive module a drive lever, which is coupled to the high-lift flap to exert force between the main aerofoil and the high-lift flap in a manner bypassing the adjustment mechanism,
• the aerofoil wing having a stop device to limit a maximum extended setting of the high-lift flap.