The invention relates to a multi-axle aircraft, which belongs to the technical field of aircrafts. The multi-axle aircraft comprises an aircraft body, a left composite wing, a right composite wing, brackets, a front rotor and a rear rotor and a landing gear. An operating system and airborne equipment are mounted in the aircraft body. The left composite wing and the right composite wing have same structures and are symmetrically mounted on the left and right sides of the aircraft body. The front rotor and the rear rotor have same structures and are respectively mounted at the front and rear ends of the aircraft body through the brackets. The landing gear adopts a wheel type structure or a skid and wheel combined structure. The left composite wing and the right composite wing have same structures and symmetrically mounted on the left and right sides of the aircraft body. Two rows of rotors are mounted in the left composite wing and the right composite wing; and all rotors are driven by a motor. A wing of the left composite wing comprises a front wing and a rear wing, which both can deflect around a wing shaft. The multi-axle aircraft provided by the invention does not need a big landing site and can vertically take off and land. The multi-axle aircraft provided by the invention has the advantages of great lift force, safety, stability and flexibility.
Multi-axle aircraft
2016-02-03
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Multi-axle steering system for multi-axle vehicle and multi-axle vehicle
Europäisches Patentamt | 2015
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