A long-distance drone is disclosed having a canard wing configuration with a cabin (270) attached to a left main wing (213) and a right main wing (214). There is a left forewing (211) and a right forewing (212) connected together to form a single-piece forewing. There is a left linear support (220) connecting the left forewing (211) to the left main wing (213), and a right linear support (221) connecting the right forewing (212) to the right main wing (214). A plurality of propellers is disposed on the left and the right linear supports (220, 221).
HYBRID VTOL FIXED-WING AERIAL VEHICLE
HYBRIDES VTOL-LUFTFAHRZEUG MIT STARREN FLÜGELN
VÉHICULE AÉRIEN À AILES FIXES VTOL HYBRIDE
2023-03-22
Patent
Electronic Resource
English