The invention relates to a multi-axle aircraft with a front wing and a rear wing, which belongs to the technical field of aircrafts. The multi-axle aircraft with the front wing and the rear wing comprises an aircraft body, a front left composite wing, a front right composite wing, a rear left composite wing, a rear right composite wing, a vertical tail wing, a bracket and a landing gear. An operation system and airbore equipment are mounted in the aircraft body. The front left composite wing and the front right composite wing have same structures and are symmetrically mounted on the left side and the right side of the front section of the aircraft body. The rear left composite wing and the rear right composite wing have same structures and are symmetrically mounted on the left side and the right side of the rear section of the aircraft body. The vertical tail wing is mounted at the tail part of the aircraft body. The landing gear uses a wheel type structure or a skid and wheel combined structure. The front left composite wing comprises a front left wing sheet and a front left rotor wing group; and the rear left composite wing comprises a rear left wing sheet, a rear left wing axle and a rear left rotor wing group. Rotor wings are all positioned under the wing sheets and driven by a motor. The rear left wing sheet can rotate and swing around the rear left wing axle. The multi-axle aircraft with the front wing and the rear wing, provided by the invention, is advantaged in that a takeoff and landing site for the aircraft is not big, the aircraft can vertically take off and land, the lifting force generated by the aircraft is large and the aircraft is safe, stable and flexible.
Multi-axle aircraft with front wing and rear wing
27.01.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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