A detachable multiaxial aircraft is related. The aircraft includes a fuselage and a number of lift arm assemblies. The lift arm assembly includes a landing chassis, an electric motor mounted on the landing chassis, and a propeller fixed on the electric motor. The lift arm assembly further includes a shell located on the landing chassis and surrounding the propeller. The fuselage includes a first connector, and the shell includes a second connector. The lift arm assembly is detachably connected to the fuselage by the first connector and the second connector.
DETACHABLE MULTIAXIAL AIRCRAFT
2019-06-13
Patent
Electronic Resource
English