Symmetric eight-axle aircraft

Abstract

The invention relates to a symmetric eight-axle aircraft, which belongs to the technical field of aircrafts. The symmetric eight-axle aircraft comprises an aircraft body, a left composite wing, a right composite wing, a bracket, a tail rod, a tail wing axle, a left transverse tail wing, a right transverse tail wing, a vertical tail wing, a landing gear, a front left rotor wing, a front right rotor wing, a rear left rotor wing and a rear right rotor wing. The front left rotor wing, the front right rotor wing, the rear left rotor wing and the rear right rotor wing have same structures and are mounted on the left and right sides in front of the aircraft and on the left and right sides behind the aircraft. The left transverse tail wing and the right transverse tail wing are symmetrically mounted on the left section and the right section of the tail wing axle, respectively; and the left transverse tail wing and the right transverse tail wing can deflect up and down around the tail wing axle. The left composite wing and the right composite wing have same structures and are symmetrically mounted on the left side and the right side of the aircraft body; and two rotor wings are mounted in both the left composite wing and the right composite wing. Wing sheets of the left composite wing comprise a fixed front wing sheet and a rear wing sheet which is capable of deflecting around a wing axle. The symmetric eight-axle aircraft 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.

Description

technical field [0001] A symmetrical octocopter belongs to the technical field of aircraft, in particular to an octocopter. Background technique [0002] The traditional octocopter consumes a lot of energy when cruising, and its stability and safety are poor. When it loses part or all of its power, it is basically unable to save itself; the traditional fixed-wing aircraft cannot vertically lift and hover; Low, security and stability are not high. Contents of the invention [0003] The purpose of the invention is to overcome the above-mentioned shortcomings of traditional hexacopters, fixed-wing aircraft and helicopters, and to invent a highly efficient and safe symmetrical octacopter that can take off and land vertically. [0004] A symmetrical octocopter, comprising a fuselage, a left compound wing, a right compound wing, a bracket, a tail boom, a tail shaft, a left transverse tail, a right transverse tail, a vertical tail, a landing gear, a front left rotor, a front rig...

AI Technical Summary

Problems solved by technology

[0002] The traditional octocopter consumes a lot of energy when cruising, and its stability and safety are poor. When it loses part or all of its power, it is basically unable to save itself; the traditional fixed-wing aircraft cannot vertically lift and hover; Low, low security and stability

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