CN108511852A - A kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle - Google Patents
A kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN108511852A CN108511852A CN201810100639.5A CN201810100639A CN108511852A CN 108511852 A CN108511852 A CN 108511852A CN 201810100639 A CN201810100639 A CN 201810100639A CN 108511852 A CN108511852 A CN 108511852A
- Authority
- CN
- China
- Prior art keywords
- upside
- fixedly connected
- unmanned plane
- battery case
- baffle
- 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.)
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/61—Types of temperature control
- H01M10/615—Heating or keeping warm
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/62—Heating or cooling; Temperature control specially adapted for specific applications
- H01M10/625—Vehicles
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/65—Means for temperature control structurally associated with the cells
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/65—Means for temperature control structurally associated with the cells
- H01M10/655—Solid structures for heat exchange or heat conduction
- H01M10/6554—Rods or plates
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/65—Means for temperature control structurally associated with the cells
- H01M10/658—Means for temperature control structurally associated with the cells by thermal insulation or shielding
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M2220/00—Batteries for particular applications
- H01M2220/20—Batteries in motive systems, e.g. vehicle, ship, plane
-
- 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
Abstract
The invention discloses a kind of battery thermostatic equipments of multi-rotor unmanned aerial vehicle,Including unmanned plane battery case,The slot bottom of the unmanned plane battery case offers circular groove,And the heating plate to match with circular groove is equipped in circular groove,And the side wall of heating plate is fixedly connected with the cell wall of circular groove,The upside of the heating plate is equipped with U-shaped heat-conducting plate,And the side wall of U-shaped heat-conducting plate is fixedly connected with the cell wall of unmanned plane battery case,The downside of the U-shaped heat-conducting plate is bonded with the upside of heating plate,The inside of the U-shaped heat-conducting plate is equipped with U-shaped thermal insulation board,And it is fixedly connected on the inside of the outside of U-shaped thermal insulation board and U-shaped heat-conducting plate,The upside of the unmanned plane battery case is equipped with horizontal baffle,And the upper end front-rear side walls of unmanned plane battery case offer horizontal sliding slot,The inside of the sliding block is fixedly connected with the both sides of baffle,On the upside of the front end of the baffle sawtooth convex block is offered with unmanned plane battery case upper wall,So that unmanned machine battery keeps constant temperature.
Description
Technical field
The present invention relates to unmanned plane field, the battery thermostatic equipment of specially a kind of multi-rotor unmanned aerial vehicle.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, nothing on machine
Cockpit, but the equipment such as automatic pilot, presetting apparatus are installed, on ground, naval vessels or machine tool remote control station personnel pass through
The equipment such as radar can be under wireless remotecontrol as conventional airplane one to it into line trace, positioning, remote control, telemetering and Digital Transmission
Sample takes off or is launched with booster rocket, can also take aerial launch to by machine tool and fly, however its battery is due to the shadow of low temperature
Ring, occur the phenomenon that power supply instability often so that there is the accident fallen in unmanned plane, thus it is proposed that a kind of more rotors without
Man-machine battery thermostatic equipment is for solving the above problems.
Invention content
The purpose of the present invention is to provide a kind of battery thermostatic equipments of multi-rotor unmanned aerial vehicle, to solve above-mentioned background technology
The problem of middle proposition.
To achieve the above object, the present invention provides the following technical solutions：A kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle,
Including unmanned plane battery case, the slot bottom of the unmanned plane battery case offers circular groove, and is equipped in circular groove and matches with circular groove
Heating plate, and the side wall of heating plate is fixedly connected with the cell wall of circular groove, and the upside of the heating plate is equipped with U-shaped heat-conducting plate, and U
The side wall of type heat-conducting plate is fixedly connected with the cell wall of unmanned plane battery case, the upside of the downside and heating plate of the U-shaped heat-conducting plate
The inside of fitting, the U-shaped heat-conducting plate is equipped with U-shaped thermal insulation board, and the outside of U-shaped thermal insulation board and the inside of U-shaped heat-conducting plate are fixed
The upside of connection, the unmanned plane battery case is equipped with horizontal baffle, and the upper end front-rear side walls of unmanned plane battery case offer
Horizontal sliding slot, and the sliding block to match with sliding slot is equipped in sliding slot, the inside of the sliding block is fixedly connected with the both sides of baffle,
On the upside of the front end of the baffle sawtooth convex block is offered with unmanned plane battery case upper wall.
Preferably, the side of the U-shaped thermal insulation board offers stomata, and stomata is uniformly covered with thermal insulation board side wall.
Preferably, vertical cylinder shape groove is offered on the upside of the left end of the U-shaped thermal insulation board, and is set in cylinder shape groove
Have the first vertical spring, and the upper end of the first spring is equipped with cylinder convex block, the both ends of first spring respectively with cylinder
It is fixedly connected on the downside of the slot bottom of groove and cylinder convex block, vertical ring groove is offered on the upside of the cylinder shape groove,
And the notch of ring groove is equipped with clamping rings, horizontal limit annulus is equipped on the downside of the clamping rings, and limit annulus
It is fixedly connected on the outside of inner wall and cylinder convex block.
Preferably, horizontal square groove is offered in the middle part of the front side of the baffle, and second spring is equipped in square groove, described the
The both ends of two springs are fixedly connected with the upper lower wall of square groove respectively.
Preferably, square groove lower wall front end is triangular structure.
Preferably, the upside of the limit annulus is less than the thickness of square groove lower wall away from the distance of the upside of cylinder convex block.
Compared with prior art, the beneficial effects of the invention are as follows：
1. heater plate, by U-shaped heat-conducting plate heat conduction so that heat is kept here by U-shaped thermal insulation board, reduces heat loss,
When it is cold so that battery can be with the temperature remains within the normal range, and the setting of stomata can reduce the amplitude of difference variation
2. the setting of the first spring and second spring allows cylinder convex block to resist baffle front end and makes on the upside of baffle
The sawtooth convex block of sawtooth convex block and unmanned plane battery case upper wall engages, and second spring makes the upper wall of square groove more be bonded nobody
The upper wall of machine battery slot, and when dismounting baffle, only need to pin baffle front end so that sawtooth convex block is separated from each other, you can dismounting.
Description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is side sectional view of the present invention；
Fig. 3 is enlarged drawing at the A of Fig. 1.
In figure：1 unmanned plane battery case, 2U types thermal insulation board, 3 stomatas, 4U types heat-conducting plate, 5 baffles, 6 cylinder shape grooves, 7
One spring, 8 cylinder convex blocks, 9 limit annulus, 10 clamping rings, 11 ring grooves, 12 heating plates, 13 sawtooth convex blocks, 14 second bullets
Spring.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
- 3 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle, packet
Unmanned plane battery case 1 is included, the slot bottom of unmanned plane battery case 1 offers circular groove, and is equipped in circular groove and adds with what circular groove matched
Hot plate 12, and the side wall of heating plate 12 is fixedly connected with the cell wall of circular groove, the upside of heating plate 12 is equipped with U-shaped heat-conducting plate 4, and U
The side wall of type heat-conducting plate 4 is fixedly connected with the cell wall of unmanned plane battery case 1, the upside of the downside and heating plate 12 of U-shaped heat-conducting plate 4
The inside of fitting, U-shaped heat-conducting plate 4 is equipped with U-shaped thermal insulation board 2, and the outside of U-shaped thermal insulation board 2 and the inside of U-shaped heat-conducting plate 4 are fixed
The upside of connection, unmanned plane battery case 1 is equipped with horizontal baffle 5, and the upper end front-rear side walls of unmanned plane battery case 1 offer water
Flat sliding slot, and the sliding block to match with sliding slot is equipped in sliding slot, the inside of sliding block is fixedly connected with the both sides of baffle 5, baffle 5
Front end on the upside of with 1 upper wall of unmanned plane battery case offer sawtooth convex block 13.
Further, the side of U-shaped thermal insulation board 2 offers stomata 3, and stomata 3 is uniformly covered with thermal insulation board side wall so that electricity
The difference variation amplitude of pond slot is small.
Further, vertical cylinder shape groove 6 is offered on the upside of the left end of U-shaped thermal insulation board 2, and in cylinder shape groove 6
Equipped with the first vertical spring 7, and the upper end of the first spring 7 is equipped with cylinder convex block 8, the both ends of the first spring 7 respectively with cylinder
The slot bottom of connected in star 6 is fixedly connected with the downside of cylinder convex block 8, and the upside of cylinder shape groove 6 offers vertical ring groove
11, and the notch of ring groove 11 is equipped with clamping rings 10,10 downside of clamping rings is equipped with horizontal limit annulus 9, and limits
The inner wall of annulus 9 is fixedly connected with 8 outside of cylinder convex block so that baffle 5 engages even closer.
Further, horizontal square groove is offered in the middle part of the front side of baffle 5, and second spring 14 is equipped in square groove, second
The both ends of spring 14 are fixedly connected with the upper lower wall of square groove respectively so that are intermeshed between sawtooth convex block 13.
Further, square groove lower wall front end is triangular structure, and 5 front end of baffle is facilitated to be inserted into.
Further, the upside of limit annulus 9 is less than the thickness of square groove lower wall away from the distance of the upside of cylinder convex block 8, prevents
The excessive height that only cylinder convex block 8 extends makes 5 front end of baffle be not easy to be inserted into.
Operation principle：
Heating plate 12 heats, 4 heat conduction of U-shaped heat-conducting plate so that battery is not to be in direct contact heat source, heat transfer to U-shaped guarantor
The setting of warm plate 2, the first spring 7 and cylinder convex block 8 makes cylinder convex block upper end withstand on the downside of the front end of baffle so that baffle 5
Engaging is close, and second spring 14 withstands square groove upper wall so that 1 upper wall of sawtooth convex block 13 and unmanned plane battery case of 5 upside of baffle
Sawtooth convex block 13 be intermeshed, anti-baffle plate 5 slip.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle, including unmanned plane battery case (1), it is characterised in that：It is described nobody
The slot bottom of machine battery slot (1) offers circular groove, and the heating plate (12) to match with circular groove is equipped in circular groove, and heating plate
(12) side wall is fixedly connected with the cell wall of circular groove, and the upside of the heating plate (12) is equipped with U-shaped heat-conducting plate (4), and U-shaped heat conduction
The side wall of plate (4) is fixedly connected with the cell wall of unmanned plane battery case (1), downside and the heating plate (12) of the U-shaped heat-conducting plate (4)
Upside fitting, the inside of the U-shaped heat-conducting plate (4) is equipped with U-shaped thermal insulation board (2), and the outside of U-shaped thermal insulation board (2) is led with U-shaped
Hot plate is fixedly connected on the inside of (4), and the upside of the unmanned plane battery case (1) is equipped with horizontal baffle (5), and unmanned machine battery
The upper end front-rear side walls of slot (1) offer horizontal sliding slot, and the sliding block to match with sliding slot is equipped in sliding slot, the sliding block
Inside is fixedly connected with the both sides of baffle (5), is opened up with unmanned plane battery case (1) upper wall on the upside of the front end of the baffle (5)
There is sawtooth convex block (13).
2. a kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The U-shaped guarantor
The side of warm plate (2) offers stomata (3), and stomata (3) is uniformly covered with thermal insulation board side wall.
3. a kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The U-shaped guarantor
Vertical cylinder shape groove (6) is offered on the upside of the left end of warm plate (2), and the first vertical bullet is equipped in cylinder shape groove (6)
Spring (7), and the upper end of the first spring (7) is equipped with cylinder convex block (8), the both ends of first spring (7) are recessed with cylinder respectively
It is fixedly connected on the downside of the slot bottom of slot (6) and cylinder convex block (8), vertical circle is offered on the upside of the cylinder shape groove (6)
Ring groove (11), and the notch of ring groove (11) is equipped with clamping rings (10), and level is equipped on the downside of the clamping rings (10)
Limit annulus (9), and inner wall and cylinder convex block (8) outside for limiting annulus (9) are fixedly connected.
4. a kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The baffle
(5) horizontal square groove is offered in the middle part of front side, and second spring (14), the both ends of the second spring (14) are equipped in square groove
It is fixedly connected respectively with the upper lower wall of square groove.
5. a kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：Under the square groove
Wall front end is triangular structure.
6. a kind of battery thermostatic equipment of multi-rotor unmanned aerial vehicle according to claim 1, it is characterised in that：The limit circle
The distance of upside of the upside of ring (9) away from cylinder convex block (8) is less than the thickness of square groove lower wall.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810100639.5A CN108511852B (en) | 2018-01-31 | 2018-01-31 | Many rotor unmanned aerial vehicle's battery constant temperature equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810100639.5A CN108511852B (en) | 2018-01-31 | 2018-01-31 | Many rotor unmanned aerial vehicle's battery constant temperature equipment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108511852A true CN108511852A (en) | 2018-09-07 |
| CN108511852B CN108511852B (en) | 2020-11-24 |
Family
ID=63374601
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810100639.5A Active CN108511852B (en) | 2018-01-31 | 2018-01-31 | Many rotor unmanned aerial vehicle's battery constant temperature equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108511852B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116149396A (en) * | 2023-04-18 | 2023-05-23 | 东方空间技术(山东)有限公司 | Temperature control system of arrow-borne flight control combination and preparation method of flexible heating device |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012069281A (en) * | 2010-09-21 | 2012-04-05 | Denso Corp | Heating device |
| CN107394079A (en) * | 2017-08-01 | 2017-11-24 | 合肥威斯伏新材料有限公司 | A kind of battery heat-preservation fixing device |
| CN206720540U (en) * | 2017-05-08 | 2017-12-08 | 国新电梯科技股份有限公司 | A kind of safety guard of escalator danger button |
-
2018
- 2018-01-31 CN CN201810100639.5A patent/CN108511852B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012069281A (en) * | 2010-09-21 | 2012-04-05 | Denso Corp | Heating device |
| CN206720540U (en) * | 2017-05-08 | 2017-12-08 | 国新电梯科技股份有限公司 | A kind of safety guard of escalator danger button |
| CN107394079A (en) * | 2017-08-01 | 2017-11-24 | 合肥威斯伏新材料有限公司 | A kind of battery heat-preservation fixing device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116149396A (en) * | 2023-04-18 | 2023-05-23 | 东方空间技术(山东)有限公司 | Temperature control system of arrow-borne flight control combination and preparation method of flexible heating device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108511852B (en) | 2020-11-24 |
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Effective date of registration: 20210720 Granted publication date: 20201124 |