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Remote control airplane with coldproof function

A technology of remote control aircraft and functions, which is applied in the field of remote control aircraft and can solve the problem of landing gear being frozen on the ground

Active Publication Date: 2017-12-12
泸州深远世宁无人机科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If the current drones are used in cold regions, after the drone lands for too long, the landing gear will be frozen on the ground.

Method used

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  • Remote control airplane with coldproof function
  • Remote control airplane with coldproof function
  • Remote control airplane with coldproof function

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Embodiment Construction

[0017] In order to make the purpose, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the examples and accompanying drawings. As a limitation of the present invention.

[0018] like Figure 1~3 As shown, a remote control aircraft with cold protection function includes outrigger 1, drone body 2, four rotor frames 7 and four motor compartments 6, outrigger 1 is fixed below the drone body 2, and four motors The bins 6 are respectively fixed on the four corners of the UAV body 2, and the rotor frame 7 is fixed above the motor bin 6; it also includes a water tank 3, four cold water pipes 9 and four hot water pipes 8, and the water tank 3 is fixed on the UAV body 2, the lower end of the leg 1 is fixed with a base plate 4, the cold water pipe 9 and the hot water pipe 8 are arranged inside the drone body 2, the leg 1 and the base plate 4, and the lower surface of the base plate 4 i...

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Abstract

The invention discloses a remote control airplane with a coldproof function, relates to the field of an unmanned aerial vehicle, and solves the problem that in the prior art, when the unmanned aerial vehicle is used in a cold region and after the landing time of the unmanned aerial vehicle is too long, a landing gear has the potential hazard of being frozen onto the ground. The remote control airplane comprises an unmanned aerial vehicle body, a support leg, a water tank, a motor cabin, a motor, a landing gear, water spraying heads, a cold water pipeline and a hot water pipeline, wherein water in the water tank enters the motor cabin through the cold water pipeline; then, water in the motor cabin is conveyed to the water spraying head arranged at the bottom of the landing gear through the hot water pipeline. When the remote control airplane is used in the cold region, the temperature reduction on the motor and the unfreezing on the landing gear can be realized at the same time; the water cooling temperature reduction can be performed on a certain specific motor according to requirements; the hot water can be output at the same time in positions of four water spraying heads for unfreezing.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a remote-controlled aircraft with a cold-proof function. Background technique [0002] Unmanned aircraft, referred to as "unmanned aerial vehicle", or "UAV" in English, is an unmanned aircraft that is controlled by radio remote control equipment and its own program control device, or is completely or intermittently operated autonomously by an on-board computer. Drones are often better suited for missions that are too "dumb, dirty or dangerous" than manned aircraft. According to the application field, UAV can be divided into military and civilian. In terms of military use, UAVs are divided into reconnaissance aircraft and target aircraft. In terms of civilian use, drones + industry applications are the real rigid needs of drones; currently, they are used in aerial photography, agriculture, plant protection, micro selfies, express delivery, disaster relief, wildlife observ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64C25/32B64D33/08
CPCB64C25/32B64C39/024B64D33/08B64U50/19B64U2201/20B64U10/10
Inventor 秦继源
Owner 泸州深远世宁无人机科技有限公司
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