UNMANNED VERTICAL TAKE-OFF AND LANDING AERIAL VEHICLE (VERSIONS) Russian patent published in 2018 - IPC B64C17/04 

FIELD: aircraft.

SUBSTANCE: invention relates to aircraft engineering, in particular to the stabilization systems for unmanned aerial vehicles of a helicopter type. Unmanned vertical take-off and landing aerial vehicle contains a housing with a rotor, placed in the air flow created by the rotor, aerodynamic roll and pitch steering controls and target load. Load is freely suspended to the body at a point lying on its vertical axis of symmetry, and is kinematically connected with aerodynamic controls by means of articulation linkage. Each of the mechanisms includes a rocker and links that connect one arm of the rocker to the load or its suspension, and the other to the corresponding steering wheel. Traction, articulated at one end with the load or its suspension, is connected to the rocker with the possibility of transferring the movement only in one direction.

EFFECT: simplification of design, cost reduction and increased reliability are provided.

7 cl, 10 dwg