The present invention is a simple mechanism that is a function of another prior invention, a multi-engine turbine, which it complements to be able to lift an aircraft in vertical take-off. It consists, simply, of metal parts that extend perpendicular to the plane of the wing elevations and that are put in the perspective of channeling the air that arrives from the turbines and that would tend to extend towards the sides of the elevon that has descended and that faces him directly.
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