An aerial vehicle 10 has a fuselage 26, at least one wing 20, propulsion means 18 for forward flight and at least two pairs of arms 12. Each arm supports at least one rotor 16 powered for vertical take-off and landing (VTOL) and each arm 12 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 12 re-transition to a deployed position for vertical landing or hovering.
AERIAL VEHICLES
2025-01-09
Patent
Electronic Resource
English