A disc-shaped aircraft powered by high-pressure gas

A high-pressure gas and aircraft technology, which is applied in the field of aircraft, can solve the problems of inoperable devices, high energy consumption, and short battery life, and achieve the effects of improving safety, durability, and long battery life

Inactive Publication Date: 2021-06-22
CHONGQING UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, because the spiral blades on the rotorcraft are mostly made of metal, and the error rate is high during operation, the high-speed rotating spiral blades are likely to cause safety accidents and endanger personal safety in public places, and they cannot enter the jungle for flying. Encountering debris, branches, etc. may directly cause the propeller to be scrapped, resulting in the failure of the entire device to operate, and has problems such as high energy consumption and short battery life.

Method used

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  • A disc-shaped aircraft powered by high-pressure gas
  • A disc-shaped aircraft powered by high-pressure gas
  • A disc-shaped aircraft powered by high-pressure gas

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Embodiment

[0023] A dish-shaped aircraft powered by high-pressure gas provided in this embodiment, with reference to the accompanying drawings: figure 1 , figure 2 , image 3 As shown, it includes a cylinder block 1 and has a dish-like structure. The cylinder block 1 is provided with 24 equidistant air jet ports 1 in the circumferential direction of the cylinder and 3 air jet ports 2 with equal distances in the circumferential direction of the lower surface plane, and A jet port control valve 4 is installed at each jet port 2 for controlling the size of the air discharge; a rotating baffle 3 is installed above the interior of the cylinder block 1, and the maximum diameter edge of the rotating baffle 3 is provided A U-shaped notch is connected to the rotary motor 2 ; a piston 6 and a piston cover plate 7 are installed under the cylinder block 1 , and the piston 6 is connected to the linear motor 5 .

[0024] In this embodiment, in order to reduce the weight of the entire aircraft, the ...

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Abstract

The invention discloses a disc-shaped aircraft driven by high-pressure gas, which comprises a cylinder block, a rotating baffle is arranged above the inside of the cylinder block, a piston and a piston cover are arranged at the bottom of the inside of the cylinder block, and a There are air bags. It is characterized in that a notch is provided on the rotating baffle and is connected with a rotating motor, a number of air injection ports are provided on the cylinder body, an L-shaped support rod is provided on the piston cover, and the air bag is sleeved on the cylinder The outer surface of the middle part of the body, the piston is connected with the linear motor. The invention realizes the flight of the aircraft in different attitudes in the air by controlling the discharge of high-pressure air from the jet port per unit time, and changes the direction of the aircraft by coordinating the rotating baffle with the jet port on the cylinder block. The invention can realize rapid take-off, improves the safety of outdoor use, has the advantages of longer battery life, and is especially suitable for flying in jungles.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a dish-shaped aircraft powered by high-pressure gas. Background technique [0002] At present, the more mature aircraft rely on the static buoyancy of the air or the aerodynamic force generated by the relative motion of the air to lift off into the air, and basically the rotorcraft is used for aerial photography. However, because most of the spiral blades on the rotorcraft are made of metal, and the error rate is high during operation, the high-speed rotating spiral blades are likely to cause safety accidents and endanger personal safety in public places, and they cannot enter the jungle for flight. Encountering debris, branches, etc. may directly cause the propeller to be scrapped, causing the entire device to fail to operate, and has problems such as high energy consumption and short battery life. SUMMARY OF THE INVENTION [0003] In order to avoid and solve the above techn...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64B1/24B64B1/58
Inventor 张太绪张晋西肖雄罗双宝徐磅迤
Owner CHONGQING UNIV OF TECH
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