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Disc-shaped helicopter

A helicopter and dish-shaped technology, applied in the field of aircraft, can solve the problems of hovering in the air, the inability to achieve vertical take-off and landing, and the limitation of the speed of the helicopter, so as to achieve the effect of stable flight

Inactive Publication Date: 2022-05-13
王西银 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the development of the aerospace industry, aircrafts are becoming more and more diversified, and there are aircrafts in different fields or flying places. People are familiar with fixed-wing aircraft and helicopters. Fixed-wing aircraft are fast, The voyage is far, but the takeoff and landing are limited by the site, and it cannot achieve vertical takeoff and landing and hovering in the air; the helicopter can achieve vertical takeoff and landing and hovering in the air, but as the altitude increases, the rotor of the helicopter The speed and its strength are limited, and it cannot go to a higher altitude
And there are few helicopters suitable for a variety of flying places in the existing technology, and can achieve supersonic speed and flight stability

Method used

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Embodiment Construction

[0023] The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments, so that those skilled in the art can implement it with reference to the description.

[0024] It should be understood that terms such as "having", "comprising" and "including" used herein do not exclude the presence or addition of one or more other elements or combinations thereof.

[0025] Such as Figure 1-Figure 4 As shown, the invention provides a dish-shaped helicopter, comprising: a dish-shaped fuselage 1, a cockpit 2 is provided at the center of the dish-shaped fuselage 1, and a storage area 3 is provided below the cockpit 2, and the dish-shaped Fuselage 1 is provided with three circumferential areas sequentially from the center outward along its radial direction, and 36 engines 4 are evenly distributed along the circumferential direction on the three described circumferential areas, and 36 engines 4 are arranged symmetrically, and the lo...

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Abstract

The invention discloses a disc-shaped helicopter which comprises a disc-shaped fuselage, a cockpit is arranged in the center of the disc-shaped fuselage, a storage area is arranged below the cockpit, three circumferential areas are sequentially arranged on the disc-shaped fuselage from the center to the outside in the radial direction of the disc-shaped fuselage, and 36 engines are evenly distributed on the three circumferential areas in the circumferential direction and symmetrically arranged. A first telescopic vortex mechanism is arranged on the outer side of the circumference of the lower portion of the storage area in the circumferential direction, a second telescopic vortex mechanism is arranged on the lower portion of the disc-shaped machine body in the circumferential direction, and a vortex area is formed between the first telescopic vortex mechanism and the second telescopic vortex mechanism. A controller is arranged in the cockpit, can be driven by a driver and is used for controlling the engine, the first telescopic vortex mechanism, the second telescopic vortex mechanism and the like, wing-free and tail-free hypersonic flight can be realized, and the flight is stable; the disc-shaped helicopter can also be of a spherical structure, serves as a standby unmanned aerial vehicle, is suitable for various flight places and is not afraid of severe weather.

Description

technical field [0001] The invention relates to the technical field of aircraft, and more specifically, the invention relates to a dish-shaped helicopter. Background technique [0002] With the development of the aerospace industry, aircrafts are becoming more and more diversified, and there are aircrafts in different fields or flying places. People are familiar with fixed-wing aircraft and helicopters. Fixed-wing aircraft are fast, The voyage is far, but the takeoff and landing are limited by the site, and it cannot achieve vertical takeoff and landing and hovering in the air; the helicopter can achieve vertical takeoff and landing and hovering in the air, but as the altitude increases, the rotor of the helicopter Both the speed and its strength are limited, and it cannot go to a higher altitude. And there are few helicopters suitable for various flying places in the existing technology, and can realize supersonic speed and flight stability. Therefore, it is necessary to ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/00B64C15/00B64D27/02
CPCB64C39/001B64C15/00B64D27/02
Inventor 王西银王永兴
Owner 王西银