Unmanned aircraft with a manipulator

Abstract

The application relates to an unmanned aerial vehicle with a manipulator, the aircraft comprising a support structure, characterized in that the manipulator comprises a turntable (201) provided with a first drive for rotating it relative to the support structure, a first boom (202) provided with a second drive for rotating it relative to the turntable (201); a second boom (203); a pusher (204); a lever (205) provided with a third drive for rotating it relative to the first boom (202); an operating tip mounted at the end of the second boom (203); and a counterweight (206) arranged on the lever (205);wherein the pusher (204) is pivotally connected at its first end to the second boom (203) for rotating it relative to the first boom (202), and is pivotally connected at its second end to the lever (205), and the first boom (202) is pivotally connected at its first end to the second boom (203) and is pivotally connected at its second end to the lever (205); wherein the first boom (202), the pusher (204), the second boom (203) and the lever (205) are arranged in pairs in a kinematic arrangement similar to an articulated parallelogram mechanism.;

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