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Solar wind power aircraft

A technology of aircraft and solar energy, applied in the field of aviation traffic, can solve the problems of demanding flight conditions, short stay in the air, short-term sports entertainment, etc.

Inactive Publication Date: 2022-06-28
黎奇凡
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Nowadays, there are also many drones that are electric. Although they do not consume fuel or emit carbon dioxide, they have a short time in the air, low power, slow flight speed, and light load, which cannot meet the needs of normal air transportation.
A small number of solar-powered aircraft, including a few gliders, have very low energy consumption and can fly for a long time, but the load is very light and the flight conditions are demanding. They can only be used for drone high-altitude reconnaissance, short-term sports entertainment, and cannot meet the needs of air transport flights.

Method used

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Examples

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Embodiment Construction

[0030] as attached figure 1Shown is a specific embodiment of a solar wind powered aircraft of the present invention, a three-view, cross-sectional view and a partial enlarged schematic diagram of the overall structure of a single-group flying-wing single-pod urban family aircraft:

[0031] Including the upper flying wing 1, the lower flying wing 2, the surface of the upper and lower flying wings is a one-way ventilation airfoil 3, the airfoil surface 3 is supported by the carbon fiber flying wing bracket 4, and the upper flying wing 1 and the lower flying wing 2 are supported by suspension cables 13. The AI ​​cockpit 14 is suspended, and the AI ​​cockpit 14 has a high-performance battery 16 , and the lower wing 2 and the AI ​​cockpit 14 are provided with a landing gear 15 below the battery 16 .

[0032] as attached figure 2 As shown, it is a structural diagram of the one-way vent 5, and a schematic diagram of the working state of the one-way valve blade 6 when the flying win...

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Abstract

The invention provides a solar energy and wind power aircraft which does not consume fuel oil or external electric energy at all. At ordinary times, a large-area solar cell panel is used for generating electricity, and a high-performance storage battery is used for storing electricity In the lift-off stage, the electric energy stored in the storage battery is used for climbing; after being lifted off, the aircraft continuously climbs by mainly utilizing the wind energy of the upflow of the atmospheric troposphere and flies like a wild goose by virtue of the wind power. The vertical take-off and landing unmanned aerial vehicle is suitable for being developed into a multifunctional unmanned aerial vehicle, an express delivery logistics unmanned aerial vehicle, a vertical take-off and landing household aircraft for urban families or a vertical take-off and landing aircraft with energy in remote mountainous areas, deserts and islands with inconvenient traffic.

Description

technical field [0001] The invention relates to the field of air traffic, in particular to a solar-powered wind-powered aircraft completely powered by solar energy and atmospheric updrafts. Background technique [0002] Most of today's aircrafts consume a lot of fuel and emit a lot of carbon dioxide. Nowadays, many drones are also electric. Although they do not consume fuel and emit no carbon dioxide, they have short airborne time, low power, slow flight speed and light load, which cannot meet the needs of normal air transportation. A few solar-powered aircrafts, including a few gliders, have low energy consumption and can fly for a long time, but they have very light load and demanding flight conditions, so they can only be used for high-altitude reconnaissance by drones, short-term sports entertainment, and cannot meet the needs of air transport flights. . [0003] The purpose of the present invention is: to propose a solar wind powered aircraft, which can take off and l...

Claims

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Application Information

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IPC IPC(8): B64C3/10B64D27/02B64C29/00H02J7/35
CPCB64C3/10B64D27/02B64C29/00H02J7/35
Inventor 黎奇凡
Owner 黎奇凡
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