CN210364367U - High-efficient radiating novel unmanned aerial vehicle - Google Patents
High-efficient radiating novel unmanned aerial vehicle Download PDFInfo
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- CN210364367U CN210364367U CN201920324377.0U CN201920324377U CN210364367U CN 210364367 U CN210364367 U CN 210364367U CN 201920324377 U CN201920324377 U CN 201920324377U CN 210364367 U CN210364367 U CN 210364367U
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Abstract
The utility model relates to a novel high-efficiency heat-dissipation unmanned aerial vehicle, which comprises a body and a horn, wherein a water tank and a heat absorption plate are arranged in the body, a heat absorption pipeline is arranged on the heat absorption plate, and a water pump is arranged on the water tank; the machine arm is of a hollow structure, the surface of the machine arm is provided with a mounting groove communicated with the hollow cavity of the machine arm, a heat dissipation plate is mounted in the mounting groove, and the lower end of the heat dissipation plate is provided with a heat dissipation pipeline; the water pump is provided with a water outlet communicated with the front end of the heat absorption pipeline and a water inlet communicated with the rear end of the heat dissipation pipeline, and the rear end of the heat absorption pipeline is communicated with the front end of the heat dissipation pipeline through a pipeline; the machine arm is rotatably provided with a paddle, and the heat dissipation plate is positioned below the paddle; the water pump takes out the coolant liquid in the water tank and inputs it into the heat absorption pipeline, absorbs the heat on the absorber plate when the coolant liquid passes through the heat absorption pipeline, then with heat-conduction to the heating panel when passing through the heat dissipation pipeline, the air current that produces through the paddle rotation at last dispels the heat to the heating panel, has improved the radiating efficiency, has avoided inside components and parts to take place the condition emergence of overheated damage.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, more specifically say, relate to a high-efficient radiating novel unmanned aerial vehicle.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. Unmanned aerial vehicle mainly divide into civilian and for military use, and at present civilian unmanned aerial vehicle's development rate is fast, especially after the national relaxation policy constraint, and market space is big.
The radiating efficiency of the radiating device of the existing unmanned aerial vehicle is low, the situation that the components and parts inside the unmanned aerial vehicle are damaged due to overheating is often caused, and therefore the market urgently needs to develop a novel efficient radiating unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model lies in, to the above-mentioned defect of prior art, provide a high-efficient radiating novel unmanned aerial vehicle.
The utility model provides a technical scheme that its technical problem adopted is:
the novel unmanned aerial vehicle with high-efficiency heat dissipation is constructed and comprises a body and a horn, wherein a water tank and a heat absorption plate are arranged in the body, a heat absorption pipeline is arranged on the heat absorption plate, and a water pump is arranged on the water tank; the machine arm is of a hollow structure, a mounting groove communicated with the hollow cavity of the machine arm is formed in the surface of the machine arm, a heat dissipation plate is mounted in the mounting groove, and a heat dissipation pipeline is arranged at the lower end of the heat dissipation plate; the water pump is provided with a water outlet communicated with the front end of the heat absorption pipeline and a water inlet communicated with the rear end of the heat dissipation pipeline, and the rear end of the heat absorption pipeline is communicated with the front end of the heat dissipation pipeline through a pipeline; the horn is last to rotate and to install the paddle, the heating panel is located the below of paddle.
High-efficient radiating novel unmanned aerial vehicle, wherein, the heat dissipation pipeline with the heat absorption pipeline all is the S type.
High-efficient radiating novel unmanned aerial vehicle, wherein, the heating panel upper end is equipped with the parallel fin of a plurality of groups.
High-efficient radiating novel unmanned aerial vehicle, wherein, the heating panel with the material of absorber plate is aluminium, copper, iron or other metals.
High-efficient radiating novel unmanned aerial vehicle, wherein, the horn is aluminum alloy material and is made by aluminum alloy extrusion technology.
The beneficial effects of the utility model reside in that:
the water pump takes out the coolant liquid in the water tank and inputs it into the heat absorption pipeline, absorbs the heat on the absorber plate when the coolant liquid passes through the heat absorption pipeline, then with heat-conduction to the heating panel when passing through the heat dissipation pipeline, the air current that produces through the paddle rotation at last dispels the heat to the heating panel, has improved the radiating efficiency, has avoided inside components and parts to take place the condition emergence of overheated damage.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the present invention will be further described with reference to the accompanying drawings and embodiments, wherein the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained without inventive efforts according to the drawings:
fig. 1 is a schematic view of the internal structure of the novel efficient heat dissipation unmanned aerial vehicle according to the preferred embodiment of the present invention;
fig. 2 is the structural schematic diagram of the novel high-efficient radiating unmanned aerial vehicle of the preferred embodiment of the utility model.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, a clear and complete description will be given below with reference to the technical solutions of the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all embodiments of the present invention. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, belong to the scope of protection of the present invention.
The novel efficient heat dissipation unmanned aerial vehicle of the preferred embodiment of the present invention is shown in fig. 1, referring to fig. 2, and comprises a vehicle body 1 and a vehicle arm 2, wherein a water tank 3 and a heat absorbing plate 4 are arranged in the vehicle body 1, a heat absorbing pipeline 5 is arranged on the heat absorbing plate 4, and a water pump 6 is arranged on the water tank 3; the machine arm 2 is of a hollow structure, a mounting groove 21 communicated with the hollow cavity of the machine arm 2 is formed in the surface of the machine arm 2, a heat dissipation plate 7 is mounted in the mounting groove 21, and a heat dissipation pipeline 8 is arranged at the lower end of the heat dissipation plate 7; the water pump 6 is provided with a water outlet 61 communicated with the front end of the heat absorption pipeline 5 and a water inlet 62 communicated with the rear end of the heat dissipation pipeline 8, and the rear end of the heat absorption pipeline 5 is communicated with the front end of the heat dissipation pipeline 8 through a pipeline; a paddle 9 is rotatably mounted on the horn 2, and the heat dissipation plate 7 is positioned below the paddle 7; the cooling liquid in the water tank 3 is pumped out by the water pump 6 and is input into the heat absorption pipeline 5, the cooling liquid absorbs heat on the heat absorption plate 4 when passing through the heat absorption pipeline 5, then the heat is conducted to the heat dissipation plate 7 when passing through the heat dissipation pipeline 8, and finally the air flow generated by rotation of the blades 9 dissipates heat of the heat dissipation plate 7, so that the heat dissipation efficiency is improved, and the occurrence of the situation of overheating damage of internal components is avoided.
As shown in fig. 2, the heat dissipation pipeline 8 and the heat absorption pipeline 5 are both in an S shape; the heat dissipation pipes 8 can fully conduct heat to the heat dissipation plate, and the heat absorption pipes 5 can fully absorb heat on the heat absorption plate.
As shown in fig. 1-2, the upper end of the heat dissipation plate 7 is provided with a plurality of parallel sets of heat dissipation fins 71; the heat radiation capability of the heat radiation plate 7 is enhanced.
As shown in fig. 1-2, the material of the heat dissipation plate 7 and the heat absorption plate 4 is aluminum, copper, iron or other metals; the materials can be selected in various ways.
As shown in fig. 1-2, the horn 2 is made of aluminum alloy material and is manufactured by aluminum alloy extrusion molding process; the metal horn facilitates heat conduction.
It will be understood that modifications and variations can be made by persons skilled in the art in light of the above teachings and all such modifications and variations are considered to be within the scope of the invention as defined by the following claims.
Claims (5)
1. A novel high-efficiency radiating unmanned aerial vehicle comprises a body and a horn; the heat absorption device is characterized in that a water tank and a heat absorption plate are arranged in the machine body, a heat absorption pipeline is arranged on the heat absorption plate, and a water pump is arranged on the water tank; the machine arm is of a hollow structure, a mounting groove communicated with the hollow cavity of the machine arm is formed in the surface of the machine arm, a heat dissipation plate is mounted in the mounting groove, and a heat dissipation pipeline is arranged at the lower end of the heat dissipation plate; the water pump is provided with a water outlet communicated with the front end of the heat absorption pipeline and a water inlet communicated with the rear end of the heat dissipation pipeline, and the rear end of the heat absorption pipeline is communicated with the front end of the heat dissipation pipeline through a pipeline; the horn is last to rotate and to install the paddle, the heating panel is located the below of paddle.
2. A novel unmanned aerial vehicle with high efficiency of heat dissipation as defined in claim 1, wherein the heat dissipation pipeline and the heat absorption pipeline are both S-shaped.
3. The novel high-efficiency radiating unmanned aerial vehicle as claimed in claim 2, wherein the upper end of the radiating plate is provided with a plurality of groups of parallel radiating fins.
4. The unmanned aerial vehicle with high heat dissipation efficiency as claimed in claim 2, wherein the material of the heat dissipation plate and the heat absorption plate is aluminum, copper or iron.
5. The novel efficient heat dissipation unmanned aerial vehicle of claim 1, wherein the horn is made of aluminum alloy material and is manufactured by an aluminum alloy extrusion molding process.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920324377.0U CN210364367U (en) | 2019-03-14 | 2019-03-14 | High-efficient radiating novel unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920324377.0U CN210364367U (en) | 2019-03-14 | 2019-03-14 | High-efficient radiating novel unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210364367U true CN210364367U (en) | 2020-04-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920324377.0U Expired - Fee Related CN210364367U (en) | 2019-03-14 | 2019-03-14 | High-efficient radiating novel unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN210364367U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111902033A (en) * | 2020-09-09 | 2020-11-06 | 南京工业职业技术大学 | Unmanned aerial vehicle with circuit board heat radiation structure |
| WO2023178688A1 (en) * | 2022-03-25 | 2023-09-28 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
-
2019
- 2019-03-14 CN CN201920324377.0U patent/CN210364367U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111902033A (en) * | 2020-09-09 | 2020-11-06 | 南京工业职业技术大学 | Unmanned aerial vehicle with circuit board heat radiation structure |
| WO2023178688A1 (en) * | 2022-03-25 | 2023-09-28 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200421 Termination date: 20210314 |