Dishing magnetic suspension ring-wing aircraft

Abstract

The invention relates to a dishing vertical takeoff and landing aircraft, namely a dishing magnetic suspension aircraft. The aircraft has an overall layout according to a dishing outline. An upper magnetic suspension ring-wing and a lower magnetic suspension ring-wing are suspended between an engine room 700 and a fixed ring 100 by a magnetic suspension driving device. The elevation angles of an upper ring-wing blade and a lower ring-wing blade are opposite to each other, and the driving forces of ring-wing power-drive magnetic rings (blocks) (2200 and 2600) are opposite to each other. The magnetic suspension ring-wing structure makes use of an electromotive power magnetic suspension driving principle to ensure that upper and lower magnetic suspension ring-wings are not only uprising and hovering rotor wings, but also an effective extension of fixed wings during forward flight. When the 2200 and the 2600 are loaded with electric power, a magnetic force drives the upper and lower ring-wings to rotate reversely to generate a lift force. The steering of the aircraft is also adjusted by the rotating speed of the upper and lower ring-wings. The forward flight is carried out by a driving device 800. The aircraft integrates the advantages of the fixed wing, a helicopter and a motor-less rotorcraft, can take off and land vertically, hover, cruise at a low altitude at a low speed, and can fly at a high speed. The dishing magnetic suspension aircraft overcomes the defects of the aircraft, is not provided with a mechanical device, is simple in control, and is high in safety.

Description

Technical field [0001] The invention relates to a dish-shaped vertical take-off and landing aircraft. Background technique [0002] In existing aircraft, vertical take-off and landing, high-speed safe flight have always been intertwined contradictions. [0003] Gyroplanes can take off and land vertically, but their manufacture and flight control are complicated and their safety is poor. And it can’t overcome the flight speed and ceiling limitations brought by the rotor itself; the fixed-wing aircraft has a high flight speed, and the ceiling is better than that of the rotorcraft, but it has high requirements for the take-off site, and it cannot ultra-low speed, low-altitude cruise, or hover. There are also some hybrid wing aircrafts trying to break through, but they have not achieved the desired effect. Contents of the invention [0004] According to the above requirements of the prior art, the present invention provides a new design method of the aircraft, which can over...

AI Technical Summary

Problems solved by technology

[0003] Gyroplanes can take off and land vertically, but their manufacture and flight control are complicated and their safety is poor

And it can’t overcome the flight speed and ceiling limit brought by the rotor itself; the flight speed of fixed-wing aircraft is high, and the ceiling is better than that of the rotorcraft, but it has high requirements for the take-off site, and it cannot be ultra-low speed, low-altitude cruise, or hovering.

There are also some hybrid wing aircraft trying to break through, but none of them have achieved the desired effect

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