Patent attributes
An aeronautical apparatus is disclosed that has two pairs of wings: an aft pair and a fore pair. Each wing has a thrust-angle motor. An assembly is coupled to each thrust-angle motor. Assemblies coupled to the fore wings have a propeller motor with a propeller and a landing element which is a wheel or a landing foot. When in forward flight, the propeller rotational axis is parallel to the longitudinal axis of the fuselage and the landing element is pointing toward the aft of the aeronautical apparatus to limit the drag presented by the landing element. When in vertical flight or hovering, the propeller rotational axis is perpendicular to the longitudinal and transverse axes of the fuselage and the landing element is deployed downward to facilitate landing.
