A long-distance drone 100 is disclosed having a canard body style with a main body 110, a left main wing 113, a right main wing 114, a left forewing 111, and a right forewing 112. The left forewing 111 is attached to the main body 110 forward of the left main wing 113, and the right forewing 112 is attached to the main body 110 forward of the right main wing 114. There is a left linear support 120 connecting the left forewing 111 to the left main wing 113, and a right linear support 121 connecting the right forewing 112 to the right main wing 114. A plurality of propellers 131, 132, 133, 134, 135, 136 are disposed on the left and the right linear supports 120, 121.
HYBRID VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING DRONE
HYBRIDE SENKRECHT STARTENDE UND LANDENDE (VTOL) FESTFLÜGELDROHNE
DRONE ADAV HYBRIDE À VOILURE FIXE
2022-05-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED WING AIRCRAFT
European Patent Office | 2016
|Vertical take-off and landing (VTOL) fixed wing aircraft
European Patent Office | 2018
|