CN205752456U - A kind of battery thermal box for unmanned aerial vehicle - Google Patents
A kind of battery thermal box for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205752456U CN205752456U CN201620589677.8U CN201620589677U CN205752456U CN 205752456 U CN205752456 U CN 205752456U CN 201620589677 U CN201620589677 U CN 201620589677U CN 205752456 U CN205752456 U CN 205752456U
- Authority
- CN
- China
- Prior art keywords
- heat
- battery
- aerial vehicle
- unmanned aerial
- motor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000009413 insulation Methods 0.000 claims abstract description 23
- 238000004321 preservation Methods 0.000 claims description 28
- 230000017525 heat dissipation Effects 0.000 claims description 20
- 230000005855 radiation Effects 0.000 abstract description 3
- 238000010276 construction Methods 0.000 abstract 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000005587 bubbling Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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- Hybrid Cells (AREA)
Abstract
The utility model discloses a kind of battery thermal box for unmanned aerial vehicle, this unmanned aerial vehicle is provided with motor, this motor has the radiator window being available for heat radiation, and this battery thermal box includes insulation shell and thermal conductive pipe, and this insulation shell and this thermal conductive pipe are interconnected；Wherein, the inside of this insulation shell is placed with battery, and the surface of this insulation shell offers radiator window；This thermal conductive pipe is tee T, has the first end, the second end and the 3rd end, wherein, the first end be this insulation shell with this thermal conductive pipe connect end, the second end is connected to the radiator window of motor, and the 3rd end is unsettled and atmosphere；First end and the 3rd end of this thermal conductive pipe are respectively equipped with open and close valve.This utility model simple in construction, effect are notable, by being provided with the tee T of open and close valve, just it is effectively utilized original heat being expelled directly out, has ensured the operating temperature of battery in the reasonable scope, and then ensure that the stability that electric energy provides, work with making unmanned aerial vehicle stability and high efficiency.
Description
Technical Field
The utility model relates to a battery heat preservation device especially relates to a battery heat preservation box for unmanned aerial vehicle.
Background
The existing unmanned aircraft generally uses a lithium battery as power, but because the unmanned aircraft generally works in a severe outdoor environment, the influence of air temperature is large in winter and summer, and bubbling, scrapping and even explosion are easily caused by high temperature; the low temperature easily causes the electric energy to descend, etc., which brings uncertainty to the power budget and the use of the unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
Structural not enough among the prior art, the utility model provides a battery heat preservation box for unmanned aerial vehicle ensures that the operating temperature of battery is more invariable, and then exports stable electric energy.
The utility model provides an above-mentioned technical problem's technical scheme as follows: a battery heat preservation box for an unmanned aerial vehicle is provided with a motor, the motor is provided with a heat dissipation window for heat dissipation, the battery heat preservation box comprises a heat preservation shell and a heat conduction pipeline, and the heat preservation shell is communicated with the heat conduction pipeline; the battery is placed in the heat-insulation shell, and a heat dissipation window is formed in the surface of the heat-insulation shell; the heat conducting pipeline is a three-way pipe and is provided with a first end, a second end and a third end, wherein the first end is a communicated end of the heat insulation shell and the heat conducting pipeline, the second end is connected to a heat dissipation window of the motor, and the third end is suspended and communicated with the atmosphere; and the first end and the third end of the heat conduction pipeline are respectively provided with an opening and closing valve.
On the basis of the technical scheme, the utility model discloses can also do following improvement.
Furthermore, a temperature sensing display unit is embedded on the heat preservation shell.
The utility model also provides a battery heat preservation box for the unmanned aerial vehicle, the unmanned aerial vehicle is provided with a motor, the motor is provided with a heat dissipation window for heat dissipation, the battery heat preservation box comprises a heat preservation shell and a heat conduction pipeline, and the heat preservation shell and the heat conduction pipeline are mutually communicated; the battery is placed in the heat-insulation shell, and a heat dissipation window is formed in the surface of the heat-insulation shell; the heat conducting pipeline is a three-way pipe and is provided with a first end, a second end and a third end, wherein the first end is a communicated end of the heat insulating shell and the heat conducting pipeline, the second end is connected to a heat dissipation window of the motor, the third end is connected to one end of an extension pipe, and the other end of the extension pipe is suspended and communicated with the atmosphere; and the first end and the third end of the heat conduction pipeline are respectively provided with an opening and closing valve.
On the basis of the technical scheme, the utility model discloses can also do following improvement.
Furthermore, a temperature sensing display unit is embedded on the heat preservation shell.
It should be noted that — the main difference between the above two technical solutions is the arrangement of the extension tube, because: if the heat conduction pipeline is arranged to be closer to the outer side, the third end of the heat conduction pipeline only needs to be suspended to ensure that the heat is led out to the atmosphere; if the heat conducting pipeline is arranged closer to the inner side, an extension pipe is required to be additionally arranged to ensure the effective conduction of heat.
The utility model has the advantages that: simple structure, effect are showing, have only added a three-way pipe that has the open and close valve on the basis of current structure, alright effectively utilize original direct exhaust heat, have ensured that the operating temperature of battery is in reasonable scope, and then have ensured the stability that the electric energy provided, make unmanned aerial vehicle work steadily high-efficiently.
Drawings
Fig. 1 is a schematic structural view of a battery heat preservation box for an unmanned aerial vehicle according to the present invention;
in fig. 1, the component name list represented by each reference numeral is as follows:
100 thermal insulation casing
101 cell
102 heat-insulating casing heat-radiating window
200 heat conducting pipeline
300 motor
301 motor heat radiation window
Detailed Description
The principles and features of the present invention are described below in conjunction with the following drawings, the examples given are only intended to illustrate the present invention and are not intended to limit the scope of the present invention.
Fig. 1 is a schematic structural view of a battery thermal insulation box for an unmanned aerial vehicle according to the present invention. The battery heat preservation box includes: a heat insulating case 100 and a heat conductive pipe 200, the heat insulating case 100 and the heat conductive pipe 200 being communicated with each other, wherein,
a battery 101 is placed in the heat-insulating shell 100, and a heat-insulating shell heat-radiating window 102 is formed in the surface of the heat-insulating shell 100;
The heat conducting pipeline 200 is a three-way pipe having a first end, a second end and a third end, wherein the first end is a communicating end of the heat insulating shell 100 and the heat conducting pipeline 200;
in the present invention, the unmanned aerial vehicle is provided with a motor 300, and the motor 300 has a motor heat dissipation window 301 for heat dissipation; the motor heat radiation window 301 is connected to the second end of the heat conduction pipeline 200;
the first end and the third end of the heat conducting pipeline 200 are respectively provided with an on-off valve;
the third end of the heat conducting pipeline 200 is suspended and communicated with the atmosphere.
Therefore, when the working environment temperature of the unmanned aircraft is low, the on-off valve at the first end of the heat conduction pipeline can be opened, and the on-off valve at the third end can be closed, so that the heat generated by the motor is conducted to the vicinity of the battery, the temperature near the battery is increased, and then the heat dissipation window of the self-insulation shell is exhausted to the atmosphere; when the working environment temperature of the unmanned aircraft is higher, the on-off valve at the first end of the heat conduction pipeline can be closed, and the on-off valve at the third end is opened, so that the heat generated by the motor is directly exhausted to the atmosphere through the third end of the heat conduction pipeline, and the heat generated by the battery is exhausted to the atmosphere through the heat dissipation window of the self-insulation shell.
In addition, if the three-way pipe is located inside the unmanned aircraft, an extension pipe may be connected to the third end of the heat conducting pipe 200, one end of the extension pipe is connected to the third end, and the other end of the extension pipe is suspended and communicated with the atmosphere, so as to ensure that the heat is conducted out to the atmosphere.
Preferably, a temperature sensing display unit is embedded in the heat preservation casing 100, and the temperature sensing display unit may be, for example, a thermometer, a temperature sensor and a temperature display electrically connected to each other, or a temperature sensing detector and an LED display electrically connected to each other, but not limited thereto.
The utility model discloses a battery heat preservation box for unmanned aerial vehicle simple structure, effect are showing, have only added a three-way pipe that has the open and close valve on the basis of current structure, alright effectively utilize original direct exhaust heat, have ensured the operating temperature of battery at reasonable within range, and then have ensured the stability that the electric energy provided, make unmanned aerial vehicle work steadily high-efficiently.
The above description is only for the preferred embodiment of the present invention, and is not intended to limit the present invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included within the protection scope of the present invention.
Claims (4)
1. A battery heat preservation box for an unmanned aerial vehicle, the unmanned aerial vehicle is provided with a motor, the motor is provided with a heat dissipation window for heat dissipation, and the battery heat preservation box is characterized in that,
the battery heat preservation box comprises a heat preservation shell and a heat conduction pipeline, and the heat preservation shell is communicated with the heat conduction pipeline; wherein,
a battery is placed in the heat-insulation shell, and a heat-dissipation window is formed in the surface of the heat-insulation shell;
the heat conducting pipeline is a three-way pipe and is provided with a first end, a second end and a third end, wherein the first end is a communicated end of the heat insulation shell and the heat conducting pipeline, the second end is connected to a heat dissipation window of the motor, and the third end is suspended and communicated with the atmosphere;
and the first end and the third end of the heat conduction pipeline are respectively provided with an opening and closing valve.
2. The battery thermal insulation box for the unmanned aerial vehicle as claimed in claim 1, wherein a temperature sensing display unit is embedded in the thermal insulation casing.
3. A battery heat preservation box for an unmanned aerial vehicle, the unmanned aerial vehicle is provided with a motor, the motor is provided with a heat dissipation window for heat dissipation, and the battery heat preservation box is characterized in that,
the battery heat preservation box comprises a heat preservation shell and a heat conduction pipeline, and the heat preservation shell is communicated with the heat conduction pipeline; wherein,
A battery is placed in the heat-insulation shell, and a heat-dissipation window is formed in the surface of the heat-insulation shell;
the heat conducting pipeline is a three-way pipe and is provided with a first end, a second end and a third end, wherein the first end is a communicated end of the heat insulating shell and the heat conducting pipeline, the second end is connected to a heat dissipation window of the motor, the third end is connected to one end of an extension pipe, and the other end of the extension pipe is suspended and communicated with the atmosphere;
and the first end and the third end of the heat conduction pipeline are respectively provided with an opening and closing valve.
4. The battery thermal insulation box for the unmanned aerial vehicle as claimed in claim 3, wherein a temperature sensing display unit is embedded in the thermal insulation casing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620589677.8U CN205752456U (en) | 2016-06-16 | 2016-06-16 | A kind of battery thermal box for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620589677.8U CN205752456U (en) | 2016-06-16 | 2016-06-16 | A kind of battery thermal box for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205752456U true CN205752456U (en) | 2016-11-30 |
Family
ID=57386710
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620589677.8U Expired - Fee Related CN205752456U (en) | 2016-06-16 | 2016-06-16 | A kind of battery thermal box for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205752456U (en) |
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2016
- 2016-06-16 CN CN201620589677.8U patent/CN205752456U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Wu Haoru Inventor after: Feng Tao Inventor before: Li Die Inventor before: Zhao Guangshun |
|
| COR | Change of bibliographic data | ||
| 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: 20161130 Termination date: 20210616 |