Vertical take-off, landing and horizontal straight flight of an aircraft includes activation a plurality of front and rear lifting propellers, each of which is connected to a respective independently operating electric motor. In addition, horizontal straight flight of the aircraft includes activation of additional left and right pushing propellers, each of which is connected to an independently operating electric motor. The front and rear lifting propellers are respectively positioned generally horizontally and symmetrically opposite to one another and equidistantly relative to a longitudinal axis of the aircraft. The right pushing propeller and the left pushing propeller are positioned generally vertically and symmetrically opposite to one another and equidistantly relative to the longitudinal axis of the aircraft.
METHODS OF VERTICAL TAKE-OFF/LANDING AND HORIZONTAL STRAIGHT FLIGHT OF AIRCRAFT AND AIRCRAFT FOR IMPLEMENTATION
VERFAHREN FÜR VERTIKALEN START/LAND-FLUG UND HORIZONTALEN GERADEN FLUG EINES FLUGZEUGS UND FLUGZEUG ZUR IMPLEMENTIERUNG
PROCÉDÉS DE DÉCOLLAGE/ATTERRISSAGE VERTICAUX ET DE VOL EN LIGNE DROITE HORIZONTALE D'AÉRONEF ET AÉRONEF POUR LEUR MISE EN OEUVRE
2024-04-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2023
|European Patent Office | 2022
|European Patent Office | 2022
|European Patent Office | 2023
|European Patent Office | 2022
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