A multirotor aircraft 10 that is adapted for vertical take-off and landing, comprising a fuselage 20, a thrust producing units assembly 30 that is provided for producing thrust in operation, and a forward-swept wing 40 that comprises a portside half wing 43 and a starboard side half wing 44. Each one of the portside and starboard side half wings 43, 44 comprises an inboard section 45 that is connected to the fuselage 20 and an outboard section 46 that forms a wing tip 71. The inboard sections 45 of the portside and starboard side half wings 43, 44 form a central wing region 80. The portside and starboard side half wings 43, 44 are respectively connected in the region of their wing tips 71 to an associated outboard wing pod 70 that supports at least two non-tiltably mounted thrust producing units 31, 32 of the thrust producing units assembly 30.
A MULTIROTOR AIRCRAFT THAT IS ADAPTED FOR VERTICAL TAKE-OFF AND LANDING (VTOL)
FÜR SENKRECHTSTART UND -LANDUNG (VTOL) GEEIGNETES MEHRROTORFLUGZEUG
AÉRONEF MULTIROTOR ADAPTÉ POUR DÉCOLLAGE ET ATTERRISSAGE VERTICAUX (ADAV)
2021-01-27
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
MULTIROTOR AIRCRAFT THAT IS ADAPTED FOR VERTICAL TAKE-OFF AND LANDING
European Patent Office | 2020
|Multirotor aircraft that is adapted for vertical take-off and landing
European Patent Office | 2023
|Engineering Index Backfile | 1968
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