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Unmanned aerial vehicle structure and unmanned aerial vehicle with stealth function

A drone and fuselage technology, applied in the field of drones, can solve the problems of difficult disassembly and low stability of drones

Pending Publication Date: 2018-04-13
詹博傲
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The first purpose of the present invention is to provide a UAV structure to alleviate technical problems such as difficulty in disassembling the UAV used in the prior art, and low stability during flight.

Method used

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  • Unmanned aerial vehicle structure and unmanned aerial vehicle with stealth function
  • Unmanned aerial vehicle structure and unmanned aerial vehicle with stealth function
  • Unmanned aerial vehicle structure and unmanned aerial vehicle with stealth function

Examples

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Embodiment 1

[0040] Such as Figure 1-5 As shown, the UAV structure provided by the present embodiment includes a fuselage 10, wings 20 and a central control unit 30; the inside of the fuselage 10 is provided with a cabin 40, and the central control unit 30 is arranged in the cabin 40. 30 is used to receive instructions and issue instructions; the wings 20 are arranged along the circumference of the fuselage 10, and the wings 20 are used to provide power to drive the fuselage 10 to hang in the air, and the central control unit 30 can drive the wings 20 to generate power; the fuselage 10 Comprising an upper fuselage 101 and a lower fuselage 102, the upper fuselage 101 and the lower fuselage 102 are fastened together, and the upper fuselage 101 and the lower fuselage 102 jointly form the cabin 40; the upper fuselage 101 and the lower fuselage 102 are both in the shape of Streamlined structure.

[0041] Specifically, the UAV structure includes a fuselage 10, wings 20 and a central control un...

Embodiment 2

[0081] This embodiment also provides a UAV with a stealth function, which includes the above-mentioned UAV structure, and the outer sides of the fuselage 10 and the wings 20 are provided with a stealth coating.

[0082] Specifically, in order to improve the stealth of the UAV structure, stealth coatings are provided on the outer walls of the fuselage 10 and the wings 20, thereby forming a UAV with a stealth function.

[0083] Among them, the stealth coating is applied with stealth materials, which can reduce the detection rate and improve the survival rate of the drone itself.

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Abstract

The invention provides an unmanned aerial vehicle structure and an unmanned aerial vehicle with a stealth function and relates to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle structure comprises a vehicle body, a wing and a center control unit, a cabin is arranged in the vehicle body, and the center control unit is arranged in the cabin and used for receiving and sending out an instruction. The wing is arranged in the circumferential direction of the vehicle body and used for providing power to drive the vehicle body to fly, and the center control unit can drivethe wing to generate the power. The vehicle body comprises an upper vehicle body and a lower vehicle body which are fixedly connected in a fastened mode and form the cabin jointly. The upper vehiclebody and the lower vehicle body are each of a streamline structure, and the outer sides of the vehicle body and the wing are coated with stealth coatings correspondingly to form an unmanned aerial vehicle with the stealth function. The technical problems that in the prior art, dismounting of the unmanned aerial vehicle is difficult, the stability in the flying process is low, and the unmanned aerial vehicle is prone to being found in investigation are solved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle structure and an unmanned aerial vehicle with a stealth function. Background technique [0002] UAV is the abbreviation of unmanned aircraft, which is an unmanned aircraft mainly controlled by radio remote control or by its own program. Compared with manned aircraft, unmanned aerial vehicles have the advantages of small size, low cost, convenient use, low requirements on the combat environment, and strong battlefield survivability, and are favored by armies all over the world. The successful development and application of UAVs on the battlefield has opened a new chapter in non-contact warfare dominated by long-distance attack intelligent weapons and information weapons. [0003] Since UAVs need to fly in the air to perform various combat tasks such as reconnaissance, interference, search, and calibration, but they often encounter resis...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C1/06B64D43/00
CPCB64C1/068B64C27/08B64D43/00
Inventor 詹博傲徐啸李响詹嘉玮周浩全潘尔雅
Owner 詹博傲
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