Uniblade air rotor and flight and covercraft vehicles with its

The invention is related to air flight vehicles, such as vertical take-off and landing (VTOL) airplanes. helicopters and covercraft. The goal of this invention is to create an air rotor designed so that while after vertical take off or cover regime, one can be stopped, fixed in a specific position and hidden into the fuselage (gondola) thus eliminating of air resistance when the rotor is not in working state. On landing this rotor can be extended out. brought into rotation and used for creation of lift force and vertical landing. The indicated goal is achieved by means of the rotor made as single blade (uniblade). The author solved the problem of force and moment balance of single blade. The center of gravity of the counterweight is located below the horizontal plane, and the blade has the horizontal sway axle, that crosses the vertical rotor rotation axis. The author offer this rotor on single axis, on co-axis, and on different exiles. This uniblade rotor is designed to subsonic and supersonic VTOL airplanes. for helicopter cars, fight motorcycles, hoppycopters, and covercraft. The uniblades be used also as a veritable sweep wing (for subsonic and supersonic aircraft).