A vertical take-off and landing aircraft includes a fuselage, 2N tilting rotors, and 2N fixed rotors. Wings of a fixed-wing structure are arranged on two sides of the fuselage. An empennage is arranged at a tail of the fuselage. The 2N tilting rotors are symmetrically installed on two sides of the fuselage and located on the front and rear sides of the wings respectively. The 2N fixed rotors are symmetrically installed on the wings on both sides of the fuselage, located on the front and rear sides of the wings respectively and on the outer sides of the tilting rotors. N is a natural number greater than or equal to 2. In a vertical take-off and landing configuration, projections of all the tilting rotors and all the fixed rotors on a horizontal plane are approximately centrally symmetrical about the center of gravity of the aircraft.
VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND CONTROL METHOD FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT
SENKRECHT STARTENDES UND LANDENDES FLUGZEUG UND STEUERUNGSVERFAHREN FÜR SENKRECHT STARTENDES UND LANDENDES FLUGZEUG
AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX ET PROCÉDÉ DE COMMANDE POUR AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX
2025-01-08
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND CONTROL METHOD FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT
European Patent Office | 2024
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