CN208849503U - A kind of Campatible unmanned plane charger - Google Patents
A kind of Campatible unmanned plane charger Download PDFInfo
- Publication number
- CN208849503U CN208849503U CN201821635440.4U CN201821635440U CN208849503U CN 208849503 U CN208849503 U CN 208849503U CN 201821635440 U CN201821635440 U CN 201821635440U CN 208849503 U CN208849503 U CN 208849503U
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- CN
- China
- Prior art keywords
- output
- interface
- unmanned plane
- power shell
- direct current
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- 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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- 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
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model provides a kind of Campatible unmanned plane charger, including power shell and is fixedly mounted on the lithium battery being electrically connected in power shell and control circuit board, and foldable solar energy charging unit is detachably electrically connected in control circuit board；DC output interface and power supply instruction component are installed on the power shell front panel, the DC output interface includes the direct current output switch being electrically connected with control circuit board, and there are four USB output interface, four direct current 12V interfaces and two automobile starting output interfaces for the direct current output output switching terminal electrical connection；The power shell rear panel is equipped with AC output interface, charging interface and exchange input interface, the AC output interface includes the exchange output switch being sequentially connected electrically, alternating-current fuse silk and two exchange output bases, the utility model has good compatibility, flexibility, portability and cruising ability, can be suitable for the outdoor charging of unmanned plane under a variety of varying environments.
Description
Technical field
The utility model relates to unmanned plane field of power supplies more particularly to a kind of Campatible unmanned plane chargers.
Background technique
UAV is to utilize radio robot and the process control provided for oneself referred to as " unmanned plane " (" UAV ")
The not manned vehicle of device manipulation.Unmanned plane is actually the general designation of unmanned vehicle, can be with from technical standpoint definition
It is divided into: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, nothing
People's parasol etc..Compared with manned aircraft, it have small in size, low cost, it is easy to use, to operational environment require low, battlefield
The advantages that survival ability is stronger.Since UAV has great significance to Future Air Combat, each main military state, the world
Family is all in the development work for stepping up progress UAV.
But the unmanned plane battery working time of current mainstream is generally at 20-30 minutes, even if one piece of reserve battery of multi-configuration,
Also it at most works 1 hour, is difficult to meet the requirement that unmanned plane inspection teams and groups open air is worked continuously, have the defects that certain.
Utility model content
In view of the above-mentioned problems, the utility model has good the utility model proposes a kind of Campatible unmanned plane charger
Compatibility, flexibility, portability and cruising ability be applicable in model suitable for the outdoor charging of unmanned plane under a variety of varying environments
It encloses extensively, the problem of background technique proposes can be efficiently solved.
In order to solve the problem above-mentioned, the utility model proposes a kind of Campatible unmanned plane chargers, including power shell
And it is fixedly mounted on the lithium battery being electrically connected in power shell and control circuit board, and be detachably electrically connected in control circuit board
There is foldable solar energy charging unit；
DC output interface and power supply instruction component, the DC output interface are installed on the power shell front panel
Including the direct current output switch being electrically connected with control circuit board, there are four USB is defeated for the direct current output output switching terminal electrical connection
Outgoing interface, four direct current 12V interfaces and two automobile starting output interfaces；
The power shell rear panel is equipped with AC output interface, charging interface and exchange input interface, the friendship
Stream output interface includes the exchange output switch being sequentially connected electrically, alternating-current fuse silk and two exchange output bases.
Further improvement lies in that: the foldable solar energy charging unit includes the installing frame of four pieces of articulated connections, described
It is fixedly installed with solar energy electroplax on installing frame, the junction of the two neighboring installing frame is equipped with magnet suction sheet, is located at
Fixing clamp is connected with by containing belt on the installing frame in portion.
Further improvement lies in that: the power supply instruction component includes exchange output indicator, AC charging indicator light, non-friendship
Current charge indicator light, remaining capacity display screen.
Further improvement lies in that: the LED light switch and LED light of electric connection are additionally provided on the power shell front panel.
Further improvement lies in that: run through on the power shell front and back panel and be equipped with fan hot hole, and between two fan hot holes
Equipped with radiator fan.
The utility model has the following beneficial effects: the utility model has abundant interface resource, can to a variety of unmanned planes into
Row charging, compatibility is good, while itself lithium battery has charging in many ways, has stronger flexibility, is suitable for a variety of
The outdoor charging of unmanned plane, applied widely under varying environment.
Detailed description of the invention
Fig. 1 is the utility model overall structure diagram.
Fig. 2 is the utility model power shell rear panel structure schematic diagram.
Fig. 3 is the utility model power shell schematic diagram of internal structure.
Fig. 4 is the utility model foldable solar energy charging unit structural schematic diagram.
Fig. 5 is the electrical block diagram of the utility model circuit control panel.
Wherein: 1- power shell；2- lithium battery；3- control circuit board；4- foldable solar energy charging unit；5- direct current is defeated
Outgoing interface；6- power supply instruction component；7- direct current output switch；8-USB output interface；9- direct current 12V interface；10- automobile starting
Output interface；11- AC output interface；12- charging interface；13- exchanges input interface；14- exchange output switch；15- exchange
Fuse；16- exchange output base；17- installing frame；18- solar energy electroplax；19- magnet suction sheet；20- fixing clamp；21- is handed over
Flow output indicator；22- AC charging indicator light；23- non-alternating charging indicator light；24- remaining capacity display screen；25-LED lamp
Switch；26-LED lamp；27- fans hot hole；28- radiator fan.
Specific embodiment
In order to deepen the understanding to the utility model, the utility model is further described below in conjunction with embodiment,
The present embodiment is only used for explaining the utility model, does not constitute the restriction to scope of protection of the utility model.
According to Fig. 1,2,3,4,5, the present embodiment proposes a kind of Campatible unmanned plane charger, including power shell
1 and it is fixedly mounted on the lithium battery 2 being electrically connected in power shell 1 and control circuit board 3, and detachable in control circuit board 3
It is electrically connected with foldable solar energy charging unit 4, wherein control circuit board 3 is used to control mutually turning for charge power supply alternating current
It changes, the size control function of voltage and current.
In the present embodiment, power technology in the prior art can be used in the control circuit in control circuit board 3, according to
The function of circuit is broadly divided into following 5 circuit modules: full bridge inverter, rectification circuit, voltage stabilization and current stabilization circuit, electricity feedback
Circuit, display decoding circuit, the DC conversion that wherein full bridge inverter is used to store lithium battery 2 are that alternating current progress is defeated
Out, rectification circuit is used to external AC conversion be direct current, and converts the straight of constant pressure and flow by voltage stabilization and current stabilization circuit
On the one hand galvanic electricity carries out the output of direct current, on the other hand carry out the charging of lithium battery 2, electricity feed circuit is for detecting lithium
Remaining capacity in battery 2, and seven segment code can be identified by showing that decoding circuit is converted into remaining capacity display screen 24, and is led to
Cross the display that remaining capacity display screen 24 carries out 2 remaining capacity of lithium battery.
DC output interface 5 and power supply instruction component 6, the direct current output are installed on 1 front panel of power shell
Interface 5 includes the direct current output switch 7 being electrically connected with control circuit board 3, and 7 output end of direct current output switch is electrically connected with four
8, four direct current 12V interfaces 9 of a USB output interface and two automobile starting output interfaces 10, direct current are connect by USB output
Mouth 8, the output of direct current 12V interface, automobile starting output interface 10 are used to that electricity will to be generated when automobile starting and directly export, and reduction is filled
Power supply inner control circuit load.
1 rear panel of power shell is equipped with AC output interface 11, charging interface 12 and exchange input interface 13,
The AC output interface 11 includes the exchange output switch 14, alternating-current fuse silk 15 and two exchange outputs being sequentially connected electrically
Base 16, wherein AC output interface 11 is for exporting the alternating current that lithium battery 2 is generated through inversion, by exchange export base into
Row exchange electricity output, during exchanging electricity output, alternating-current fuse silk 15 plays the role of current-limiting protection, charging interface 12
The charging of lithium battery 2 is carried out for accessing solar charging electrical interface or vehicle-mounted charge interface, exchange input interface 13 is for accessing
The charging of 220V alternating current progress lithium battery 2.
Compared with the prior art, the utility model has abundant interface resource, can charge to a variety of unmanned planes, simultaneous
Capacitive is good, while itself lithium battery has charging in many ways, has stronger flexibility, is suitable under a variety of varying environments
The outdoor charging of unmanned plane, it is applied widely.
The foldable solar energy charging unit 4 includes the installing frames 17 of four pieces of articulated connections, is consolidated on the installing frame 17
Dingan County is equipped with solar energy electroplax 18, and the junction of the two neighboring installing frame 17 is equipped with magnet suction sheet 19, positioned at middle part
Fixing clamp 20 is connected with by containing belt on the installing frame 17.
Installing frame in foldable solar charging unit 4 is articulated and connected by hinge, first distinguishes the installing frame 17 at both ends
It folds on adjacent installing frame 17, finally folds the installing frame 17 that two pieces fold again, finally by containing belt
On fixing clamp 20 be connected together, the folding for realizing installing frame 17 is fixed, and occupied space is smaller after folding, easy to carry,
Solar recharging, alternating current charging and vehicle-mounted charge, the diversification of lithium battery charging modes enable lithium battery more square
Just energy supply is obtained, the cruising ability of lithium battery is improved.
The power supply instruction component 6 includes exchange output indicator 21, AC charging indicator light 22, non-alternating charging instruction
Lamp 23, remaining capacity display screen 24, power supply instruction component 6 are used to indicate the working condition of charge power supply, when ac output end connects
When entering to load, exchange output indicator 21 is lit, when being charged by 220V alternating current to lithium battery 2, AC charging
Indicator light 22 is lit, when being charged by solar energy or vehicle-mounted interface to lithium battery 2,23 quilt of non-alternating charging indicator light
It lights, remaining capacity display screen 24 is used to show the electricity stored in lithium battery 2, understands the energy storage in lithium battery convenient for user
Situation.
It is additionally provided with the LED light switch 25 and LED light 26 of electric connection on 1 front panel of power shell, realizes outdoor night
Between illumination.
Run through on 1 front and back panel of power shell and be equipped with fan hot hole 27, and is equipped with radiation air between two fan hot holes 27
Fan 28 fans the setting of hot hole 27 and radiator fan 28, radiates for control circuit board 3, guarantees control circuit work normal
In temperature range.
The basic principles and main features and advantage of the utility model have been shown and described above.The technical staff of the industry
It should be appreciated that the present utility model is not limited to the above embodiments, the above embodiments and description only describe this
The principle of utility model, on the premise of not departing from the spirit and scope of the utility model, the utility model also has various change
And improvement, these various changes and improvements fall within the scope of the claimed invention.The utility model requires protection scope
It is defined by the appending claims and its equivalent thereof.
Claims (5)
1. a kind of Campatible unmanned plane charger, it is characterised in that: including power shell (1) and be fixedly mounted on power shell
(1) in be electrically connected lithium battery (2) and control circuit board (3), and be detachably electrically connected in control circuit board (3) it is foldable too
Positive energy charging unit (4)；
DC output interface (5) and power supply instruction component (6) are installed on power shell (1) front panel, the direct current is defeated
Outgoing interface (5) includes the direct current output switch (7) being electrically connected with control circuit board (3), and the direct current output switchs (7) output end
There are four USB output interface (8), four direct current 12V interfaces (9) and two automobile starting output interfaces (10) for electrical connection；
Power shell (1) rear panel is equipped with AC output interface (11), charging interface (12) and exchange input interface
(13), the AC output interface (11) include be sequentially connected electrically exchange output switch (14), alternating-current fuse silk (15) and
Two exchanges export base (16).
2. a kind of Campatible unmanned plane charger according to claim 1, it is characterised in that: the foldable solar energy fills
Electric installation (4) includes the installing frame (17) of four pieces of articulated connections, is fixedly installed with solar energy electroplax on the installing frame (17)
(18), the junction of the two neighboring installing frame (17) is equipped with magnet suction sheet (19), the installing frame positioned at middle part
(17) fixing clamp (20) are connected with by containing belt on.
3. a kind of Campatible unmanned plane charger according to claim 1, it is characterised in that: the power supply instruction component
(6) aobvious including exchange output indicator (21), AC charging indicator light (22), non-alternating charging indicator light (23), remaining capacity
Display screen (24).
4. a kind of Campatible unmanned plane charger according to claim 1, it is characterised in that: before the power shell (1)
The LED light switch (25) and LED light (26) of electric connection are additionally provided on panel.
5. a kind of Campatible unmanned plane charger according to claim 1, it is characterised in that: before the power shell (1)
Radiator fan (28) are equipped with through equipped with fan hot hole (27), and between two fan hot holes (27) on rear panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821635440.4U CN208849503U (en) | 2018-10-10 | 2018-10-10 | A kind of Campatible unmanned plane charger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821635440.4U CN208849503U (en) | 2018-10-10 | 2018-10-10 | A kind of Campatible unmanned plane charger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208849503U true CN208849503U (en) | 2019-05-10 |
Family
ID=66375060
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821635440.4U Withdrawn - After Issue CN208849503U (en) | 2018-10-10 | 2018-10-10 | A kind of Campatible unmanned plane charger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208849503U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111313498A (en) * | 2020-03-09 | 2020-06-19 | 江苏中兴派能电池有限公司 | Portable energy storage power supply device |
-
2018
- 2018-10-10 CN CN201821635440.4U patent/CN208849503U/en not_active Withdrawn - After Issue
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111313498A (en) * | 2020-03-09 | 2020-06-19 | 江苏中兴派能电池有限公司 | Portable energy storage power supply device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20190510 Effective date of abandoning: 20221223 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20190510 Effective date of abandoning: 20221223 |
|
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |