Multi-copter cross-row vertical take-off and landing hybrid fixed-wing aircraft

Abstract

A kind of multi-rotor horizontal column type vertical take-off and landing composite fixed-wing aircraft, using the upper single wing fixed wing without sweep as the basis, right one rotor, right two rotors, right three rotors are sequentially connected on the spar of the leading edge of the upper single wing close to the right side of fuselage;Left one rotor, left two rotors, left three rotors are sequentially connected on the spar of the leading edge of the upper single wing close to the left side of fuselage;In the initial state, the lift of each rotor is vertically upward, the projection of the connecting line of the rotation center of each rotor on the horizontal plane is a horizontal straight line, the midpoint of the straight line, the projection of the center of gravity of the aircraft on the horizontal plane overlaps, the flight controller connects the six electronic governors of motor, the flight controller connects six tilt components, the flight controller can drive the rotor lift direction to convert between vertically upward and horizontally forward, only three groups of rotors can meet the pitch, roll and heading of the aircraft, with the advantages of compact structure and high flight efficiency, become a new architecture of general vertical take-off and landing composite fixed-wing aircraft.

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