Dishing magnetic suspension ring-wing aircraft

A magnetic levitation and ring-wing technology, applied in aircraft, motor vehicles, transportation and packaging, etc., can solve problems such as inability to overcome flight speed and ceiling restrictions, ultra-low speed, low-altitude cruise, complex manufacturing, and flight control. The effect of safety and efficacy, small resistance and simple structure

Inactive Publication Date: 2011-06-08
范磊
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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...

Method used

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  • Dishing magnetic suspension ring-wing aircraft
  • Dishing magnetic suspension ring-wing aircraft
  • Dishing magnetic suspension ring-wing aircraft

Examples

Experimental program
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Embodiment Construction

[0050] 1. Ring wing

[0051] In the present invention, the rotation of the upper and lower ring wings is the main component to realize the take-off and landing, hovering, low-speed cruising and steering of the aircraft.

[0052] The magnetic suspension upper ring wing 200 is connected with the suspension ring 1500 connected with the magnetic suspension outer rail of the upper ring wing and the magnetic suspension inner rail connection suspension ring 2300 of the upper ring wing, and is suspended on the 1300, 1400, 1600, 1700, 1800, 2000 ring wing suspension stable magnetic ring (block ), and after the 2200 upper ring wing power drives the magnetic ring (block) to load electric energy, it uses the magnetic levitation drive principle to drive the rotation.

[0053] The magnetic suspension lower ring wing 300 is connected with the suspension ring 1900 connected with the magnetic suspension outer rail of the lower ring wing and the suspension ring 2600 connected with the magnetic ...

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PUM

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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...

Claims

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Application Information

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IPC IPC(8): B64C39/00
Inventor 范磊
Owner 范磊
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