Vertical lifting type disc-shaped aircraft

Abstract

The invention discloses a vertical lifting type disc-shaped aircraft, relating to the field of aircrafts. The vertical lifting type disc-shaped aircraft comprises a circular disc and a control cabinet, wherein the circular disc comprises an inner disc and an outer disc; upwards-protruding ridges are arranged on the upper surface of the circular disc; the control cabinet is internally equipped with a speed changer and an engine; the speed changer is connected with the engine; transmission shafts which are arranged in a vertical direction are arranged in the inner disc; bearings are arranged at the tops and the bottoms of the transmission shafts; a driving wheel is arranged in the middle of each transmission shaft; the side face of each driving wheel is tangent to the outer edge of the outer disc; the bearings at the tops of the transmission shafts are connected with the speed changer; the top of the inner disc is movably connected with the top of the outer disc through upper balls; and the bottom of the inner disc is movably connected with the bottom of the outer disc through lower balls. By adopting the vertical lifting type disc-shaped aircraft, the flying efficiency can be effectively improved, the stability is good, the safety is good, the structure is simple, the manufacturing is easy and the cost is low.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a vertical lift type disc-shaped aircraft. Background technique [0002] At present, there are mainly two kinds of practical aircraft: helicopter and fixed-wing aircraft. The helicopter uses the propeller to generate upward lift. During the flight, the propeller rotates at a high speed, and the aircraft needs to overcome a lot of resistance to achieve its own balance. The flight efficiency is relatively high. Low, and the aircraft is easily affected by external forces during flight. When there is a crosswind in the air, the aircraft is easy to shake, or even roll over, and the stability is poor. Restricted by its own conditions, the helicopter is generally equipped with one engine. Once the engine fails during the flight of the aircraft, the aircraft cannot fly normally. Equipment, if the helicopter breaks down during flight, the personnel in the helicopter have no escape equipment, and ...

AI Technical Summary

Problems solved by technology

[0002] At present, there are mainly two kinds of practical aircraft: helicopter and fixed-wing aircraft. The helicopter uses the propeller to generate upward lift. During the flight, the propeller rotates at a high speed, and the aircraft needs to overcome a lot of resistance to achieve its own balance. The flight efficiency is relatively high. Low, and the aircraft is easily affected by external forces during flight. When there is a crosswind in the air, the aircraft is easy to shake, or even roll over, and the stability is poor

Restricted by its own conditions, the helicopter is generally equipped with one engine. Once the engine fails during the flight of the aircraft, the aircraft cannot fly normally. Equipment, if the helicopter breaks down during the flight, the personnel in the helicopter will not have escape equipment, and the safety factor will be low. In addition, the current aircraft structure is relatively complicated, the production process is cumbersome, the strength of the material is high, and the production cost is high

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