The invention provides a compact-type multi-rotor fuel-electric
hybrid unmanned aerial vehicle. The compact-type multi-rotor fuel-electric
hybrid unmanned aerial vehicle comprises a
fuselage and a plurality of rotors evenly arranged on the side surface of the
fuselage at intervals. An engine module, an
electric generator module and a pan-tilt
assembly are arranged at the bottom of the
fuselage, afuel tank is arranged at the top end of the fuselage, and a
control system is arranged in the fuselage. The fuselage includes a first fixed plate and a second fixed plate, the engine module, the
electric generator module and the pan-tilt
assembly are arranged at the lower end of the first fixed plate, the engine module is connected with an
electric generator, the engine module can drive the electric generator to operate, and the electric generator and the pan-tilt
assembly are separately and electrically connected to the
control system. The rotors are hinged to the side surface of the first fixed plate, and folding of the rotors is realized. The ends, close to the fuselage, of the rotors are proximal ends, and the ends, away from the fuselage, of the rotors are distal ends. Motors and propellers are arranged at the distal ends of the rotors, and the motors are electrically connected to the
control system and the propellers and can drive the propellers to rotate.