Abstract

A rotorcraft design that incorporates a single-axis tilt swashplate assembly is disclosed. The swashplate assembly tilts about a single horizontal axis. The simplified swashplate assembly of the disclosed rotorcraft design allows for a lighter assembly with fewer moving parts. Multiple rotor drive assemblies incorporating the simplified swashplate assembly are supported by a flight body that allows for modular attachment of mission panels to allow for quick reconfiguration of the rotorcraft for various specific applications. The simplified swashplate assembly is particularly suited for aerial unmanned vehicles (UAVs) or drones.

IPC Classes  ?

• B64C 27/43 - Rotors having articulated joints with flapping hinge or universal joint, common to the blades see-saw type, i.e. two-bladed rotor

Abstract

A rotorcraft design that incorporates a single-axis tilt swashplate assembly is disclosed. The swashplate assembly tilts about a single horizontal axis. The simplified swashplate assembly of the disclosed rotorcraft design allows for a lighter assembly with fewer moving parts. Multiple rotor drive assemblies incorporating the simplified swashplate assembly are supported by a flight body that allows for modular attachment of mission panels to allow for quick reconfiguration of the rotorcraft for various specific applications. The simplified swashplate assembly is particularly suited for aerial unmanned vehicles (UAVs) or drones.

IPC Classes  ?

• B64C 27/43 - Rotors having articulated joints with flapping hinge or universal joint, common to the blades see-saw type, i.e. two-bladed rotor