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Novel solar military unmanned aerial vehicle

A technology of solar energy and unmanned aerial vehicles, applied in the field of unmanned aerial vehicles, can solve the problems of reducing the buffering and shock absorption ability of unmanned aerial vehicles, device functional limitations, and small size of unmanned aerial vehicles. Increase functionality and flexibility, observe the effect of a wide field of view

Inactive Publication Date: 2021-01-05
安徽徽光智能科技有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The scope of application of military drones is too wide. Commonly used such as surveillance, reconnaissance or material transportation, etc., models with different functions will be selected according to the needs of use. One type of drone does not have comprehensive functions, but the drone itself The volume is small and cannot carry too many installation parts, so a large number of classifications are required during equipment production, which limits the functionality of the device and reduces the variability of the use of drones; since drones require multiple blades Rotate to fly, but each set of blades needs a separate driving force to cooperate with the rotation, so that the power consumption of the UAV is also increased, causing the UAV to be unable to fly for a long time, reducing the practical value of the device, and The blades of the drone are extremely fragile. If the blades are damaged due to impact during flight, the drone cannot maintain balance, and there may be a risk of loss of control and damage. Reduce the protective measures of the device. When the drone lands If during the transportation of materials, the inertial force generated by the contact between the body and the ground will cause the whole device to vibrate, which will not only cause wear on the parts in the body, but also have an impact on the transported materials, reducing the buffering and shock absorption of the drone landing ability

Method used

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  • Novel solar military unmanned aerial vehicle
  • Novel solar military unmanned aerial vehicle
  • Novel solar military unmanned aerial vehicle

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0031] Example 1, such as Image 6 As shown, when the device needs to transport materials, the clamping transport assembly can be connected and installed with the device, and then the materials are placed on the surface of the concave placement table 307, and the two sets of threaded rods A301 are rotated by starting the servo motor A309, and use The limit sliding of the slider 303 and the chute 304 makes the internally threaded sleeve A302 guide and move closer, and with the approaching movement of the internally threaded sleeve A302, the slider 303, the connecting arm 305 and the clamping plate 306 are moved, during which a group of connecting The arm 305 drives the inserting plate 308 to be inserted into another set of recessed placement table 307 placed on the connecting arm 305, and the material is clamped and fixed by the approach of the clamping plate 306, and then the buckle 22 is pulled to pull out the binding belt 26, And force the winding wheel 28 to rotate to drive...

Embodiment 2

[0032] Example 2, such as Figure 7 As shown, when the device lands, the universal wheel 403 is used to contact the ground first, and the hinged cooperation of the hinged block 401 is used to make the arc-shaped plate 404 open outwards to drive the spring 405 to compress and absorb shock, and then the cushion air cushion 402 is used to contact the ground Perform secondary relief to increase the cushioning and shock resistance of the device, and further improve the protection of materials.

[0033] Working principle: Firstly, the servo motor B5, the omnidirectional camera 7 and the driving motor 18 are started respectively through the controller 21, and the solar photovoltaic panel A12 and the solar photovoltaic panel B14 are installed to absorb the emitted sunlight, and the photovoltaic controller 23 Cooperate with the connection of the storage battery 2 to convert the absorbed light energy into electric energy, and start four, six or eight groups of drive motors 18 according ...

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Abstract

The invention discloses a novel solar military unmanned aerial vehicle comprising a mounting column and a controller; a servo motor B is arranged in the middle of the interior of the mounting column,a servo motor B is arranged at the top of the interior of the mounting column, a storage battery is arranged at the bottom of the interior of the mounting column, and mounting grooves connected with each other are formed in the top of the mounting column; a fixing ring is arranged at the top of the outer side of the mounting column, and four sets of all-dimensional cameras are arranged on the outer side of the fixing ring. According to the unmanned aerial vehicle, through mutual cooperation of a clamping and transporting assembly, the unmanned aerial vehicle can clamp and fix goods and materials and conduct flying transportation, meanwhile, an unmanned aerial vehicle body is provided with the fixing ring and the all-dimensional cameras, the observation view to the unmanned aerial vehicle body is wider, and the unmanned aerial vehicle body is more convenient to control; and the clamping and transporting assembly can be detached from and separated from the unmanned aerial vehicle body, so that the clamping and transporting assembly can be changed according to actual use requirements, and the functionality and flexibility of the device are improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a new solar-powered military unmanned aerial vehicle. Background technique [0002] UAV is the abbreviation of unmanned aircraft. It is an unmanned aircraft that uses radio remote control equipment and its own program control device. From a certain point of view, UAVs can complete complex aerial tasks under unmanned conditions. Flight missions and various load tasks are classified according to their uses. UAVs can be divided into military UAVs and civilian UAVs. At present, more than 70% of UAVs are used for military purposes. The second is from the technical point of view. Man-machines are divided into six camps, namely unmanned helicopters, unmanned fixed-wing aircraft, unmanned multi-rotor aircraft, unmanned airships, unmanned umbrella-wing aircraft, and flapping-wing micro-drones; [0003] The scope of application of military drones is too wide. Commonly use...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64D9/00B64D47/08B64D27/24H02J7/35B64C25/62
CPCB64C39/02B64D9/00B64D47/08B64D27/24H02J7/35B64C25/62B64U50/19B64U2101/60Y02T50/60
Inventor 裴忠军严伍琼刘志高付明珠
Owner 安徽徽光智能科技有限责任公司