An aircraft is described and includes an airframe including first and second wings each having first and second oppositely disposed wing tips; first and second booms respectively extending longitudinally between the first and second wings and having forward and aft ends; first and second tail assemblies respectively coupled to aft ends of the first and second booms; first and second forward propulsion assemblies respectively coupled to the forward ends of the first and second booms, wherein the first and second forward propulsion assemblies are tiltable between a vertical takeoff and landing (“VTOL”) flight mode orientation and a forward flight mode orientation; first and second aft propulsion assemblies respectively coupled to upper ends of the tail assemblies, wherein the first and second aft propulsion assemblies are tiltable between a VTOL flight mode orientation and a forward flight mode orientation; and a payload module removably coupled to the airframe.
VERTICAL TAKEOFF AND LANDING DUAL-WING AERIAL VEHICLE
2020-05-07
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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