The articulated Mechatronic System for propulsion, aerodynamics and the vertical takeoff Aircraft

摘要

System for Mechatronic articulated propulsion, aerodynamics and vertical take-off Aircraft which comprises an articulated System for propulsion, located inside the aircraft, which complements the Sustaining effect generated by the rotor rotation of gyroplanes during FAS And take-offOr complements the Sustaining effect generated by the mass of hot air or gas contained in the envelope of the Airship, which is a Creator of a constant pressure system of air from the vertical to the horizontal Plane for take-off for Cruise Flight,Independent of the rotor and enough Strength to generate Forward shifting of the airmobile and air pressure, directed from an Airborne into the soil to increase its mass and weight in the Air During the take-off Phase or shorten the distance of an airplane Bearing pair At Takeoff.The system facilitates the rapid Transition of the Plan of vertical flight to horizontal airmobile, without loss of altitude, due to the rapid rotation of the mechanisms of this propulsion system is characterized by a through understanding of the Turbine with a First Section that is u In air Inlet.A second section in which there is a Mobile channel for directing the flow of air to the Ground,A third section in which there is an air Outlet as well as Air Side entrances and fins arranged vertically and equipped with a mechanism that allows you to Modify your guidance to direct air pressure to maintain Stable Aberrations and a Stabilization of the airmobile; The fourth section, in which a motor and a Transmission means.