The invention is related to a multirotor aircraft 1 that is adapted for vertical take-off and landing. The multirotor aircraft comprises a fuselage 2, a tail boom 4 that is provided with a vertical fin 5, a thrust producing units assembly 40 that is provided for producing thrust in operation, at least one lower wing 12 which comprises a lower wing inboard section 12a that is connected to the fuselage and a lower wing outboard section 12b that forms a lower wing tip 27, and at least one upper wing 11 which is connected to the vertical fin and which forms an upper wing tip. The at least one upper wing 11 is joined to the at least one lower wing 12 in a joined-wing configuration.
A MULTIROTOR JOINED-WING AIRCRAFT WITH VTOL CAPABILITIES
BOXWING FLUGZEUG MIT MEHREREN ROTOREN MIT FÄHIGKEIT ZUM SENKRECHTEN STARTEN UND LANDEN (VTOL)
AÉRONEF MULTIROTOR À AILE JOINTE AVEC DES CAPACITÉS DE DÉCOLLAGE ET ATTERRISSAGE VERTICAUX (ADAV)
2021-01-13
Patent
Electronic Resource
English
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