The invention relates to a flying apparatus (100) comprising a main structure of airframe or fuselage (20) and a rotative wing surface (10), the rotation of the rotative wing surface (10) allowing stabilizing the apparatus (100) during taking-off, landing and displacing through the air. The fuselage (20) hangs from the rotative wing surface (10) around a hanging point, allowing the rotative wing surface (10) and the fuselage (20) be moveable independently with respect to each other and the rotative wing surface (10) is configured as a disc with a concave surface, being orientable in order to manoeuvre the apparatus (100), and comprising one or a plurality of orientable elements (11) acting as security and secondary command and control surfaces, orienting the apparatus (100) in desired directions. The flying apparatus (100) of the invention comprises a main structure of airframe or fuselage (20) and a rotative wing surface (10): the wing surface (10) can overwrap at least partially the structure of the fuselage (20) in order to improve the aerodynamic performance.In the flying apparatus (100) according to the invention, the airframe or fuselage (20) and the rotative wing surface (10) are rotatable around any of three rotational axis (X, Y and/or Z), independently to each other.
FLYING APPARATUS
FLUGVORRICHTUNG
APPAREIL VOLANT
2019-10-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |