Composite wing unmanned aerial vehicle

• Main Authors: WANG WEI, ZHANG HAILIN, MA JINSHAN, WANG YUE, SONG JIZHEN, LI PENGBO
• Format: Patent
• Language: Chinese; English
• Published: 08.07.2022
• Subjects: AEROPLANES; AIRCRAFT; AVIATION; COSMONAUTICS; HELICOPTERS; PERFORMING OPERATIONS; TRANSPORTING

The composite wing unmanned aerial vehicle comprises a fuselage, wings, an empennage, a level flight power unit and a multi-rotor power unit, the wings are of an integral structure extending from the left side of the unmanned aerial vehicle to the right side of the unmanned aerial vehicle, and the fuselage is rotatably installed below the wings through a first rotating part; through the first rotating part, the fuselage can rotate to a wingspan direction parallel to the wings; the multi-rotor power unit comprises a plurality of vertical power propellers, and each vertical power propeller is matched with a driving motor and a bracket; the vertical power propeller is mounted on the lower side of one end of the bracket through the driving motor, and the other end of the bracket is rotatably mounted below the wings; the bracket rotates relative to the wings, and the vertical power propellers can rotate to the positions under the wings; and the empennage comprises a vertical empennage arranged below the rear end o