Patent attributes
Morphing aircraft wing with a mobile upper surface comprising a double skinning on the upper surface of the wing wherein one of the skinnings corresponds to the leading edge and the other corresponds to the trailing edge and they overlap in the central area of the wing with the possibility of relative displacement between the two skinnings and they extend in the direction of the chord of the wing profile, the wing comprises actuators that are positioned on the main wing spars and which exert a reaction force against said spars when they exert the force required to morph the wing displacing the skinnings in the direction of the chord of the profile to the configuration of low speed flight, take-off and landing.