An aerial vehicle has a fuselage, at least one wing, propulsion means for forward flight and at least two pairs of arms. Each arm supports at least one rotor powered for vertical take-off and landing (VTOL) and each arm is in a deployed position for vertical take-off or hovering and transitions to a retracted position for forward flight using the at least one wing, and the arms re-transition to a deployed position for vertical landing or hovering.
AERIAL VEHICLES
2023-11-09
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |