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A cooling device for a multi-rotor UAV

A technology of multi-rotor drones and cooling devices, which is applied in the field of drones, can solve the problems that the cooling devices cannot be installed on drones of different specifications, and poor versatility, so as to achieve the effect of ensuring stability and universality

Active Publication Date: 2021-11-30
江苏御风海上安全咨询服务有限公司
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

[0004] In order to solve the problems raised in the above-mentioned background technology, the object of the present invention is to provide a multi-rotor UAV cooling device, which has the advantage of high versatility, and solves the problem that the existing UAV cooling device has poor versatility and cannot easily dissipate heat. The problem of installing the device on drones of different specifications

Method used

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  • A cooling device for a multi-rotor UAV
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  • A cooling device for a multi-rotor UAV

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Embodiment Construction

[0045] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0046] Such as Figure 1 to Figure 4 As shown, a kind of multi-rotor UAV cooling device provided by the present invention comprises multi-rotor UAV body 1, and the top of multi-rotor UAV body 1 is provided with cooling fan 2, and the front and back of cooling fan 2 are all fixed The adjustment frame 3 is connected, and the inside of the adjustment frame 3 is slidingly installed with the installation rod 4. The front and back of the multi-rotor UAV body 1 can b...

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Abstract

The invention discloses a heat dissipation device for a multi-rotor UAV, which comprises a body of the multi-rotor UAV. A cooling fan is arranged on the top of the body of the multi-rotor UAV. Both the front and the back of the cooling fan are fixedly connected with adjustable frame, the inside of the adjustment frame is slidably installed with a mounting rod, the front and back of the multi-rotor UAV body are glued and fixed to limit plates, the bottom of the mounting rod is fixedly connected with a buffer mechanism, and the multi-rotor The bottom of the drone body is provided with a storage battery. The present invention solves the problem of poor versatility and inconvenientness of existing UAV cooling devices by setting the multi-rotor UAV body, cooling fan, adjustment frame, installation rod, limit plate, buffer mechanism, battery and supporting legs. The cooling device is installed on drones of different specifications, and the heat dissipation power depends on the power of the drone to affect the battery life of the drone. It has the advantages of high versatility and does not affect battery life.

Description

technical field [0001] The invention relates to the technical field of drones, in particular to a cooling device for multi-rotor drones. Background technique [0002] UAV is a general term for unmanned aerial vehicles. It is equipped with autopilot, program control device and other equipment. It can track and locate flight equipment through ground station or pilot operation. Compared with manned aircraft, it has small size, With the advantages of low cost and convenient use, there are many types of UAVs, mainly including fixed-wing UAVs, flapping-wing UAVs and multi-rotor UAVs. Vertical take-off and landing can hover in the air after taking off. Therefore, compared with fixed-wing UAVs and flapping-wing UAVs, multi-rotor UAVs have been widely used in various fields. The existing multi-rotor UAVs are due to The flight time is long, causing the body to heat up seriously, and because there is no cooling device, the temperature of the body cannot be lowered, so there is a risk ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D33/10B64C25/62
CPCB64D33/10B64C25/62B64U10/10B64U50/19B64U30/20
Inventor 许蕤
Owner 江苏御风海上安全咨询服务有限公司
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