CN108173321A - A kind of unmanned plane quickly charging battery device - Google Patents
A kind of unmanned plane quickly charging battery device Download PDFInfo
- Publication number
- CN108173321A CN108173321A CN201810159357.2A CN201810159357A CN108173321A CN 108173321 A CN108173321 A CN 108173321A CN 201810159357 A CN201810159357 A CN 201810159357A CN 108173321 A CN108173321 A CN 108173321A
- Authority
- CN
- China
- Prior art keywords
- fixedly installed
- contact block
- babinet
- charging
- unmanned plane
- 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.)
- Withdrawn
Links
- 230000005611 electricity Effects 0.000 claims abstract description 25
- 230000013011 mating Effects 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 6
- 230000004888 barrier function Effects 0.000 claims 1
- 230000007613 environmental effect Effects 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
Classifications
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
- H02J7/0045—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction concerning the insertion or the connection of the batteries
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0047—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with monitoring or indicating devices or circuits
-
- H02J7/025—
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a kind of unmanned plane quickly charging battery devices,Including supporting leg,Babinet,Accumulator,Charging panel,Spring,Contact block A,Contact block B,Electricity storage module,Electric wire and control panel,Supporting leg has several,Supporting leg top is fixedly installed in babinet lower surface,Accumulator is fixedly installed in babinet,Charging panel is cylinder,Charging panel bottom is provided with groove A,Babinet top is set in groove A,Spring has several,It is connected at the top of spring top and groove A,Spring bottom end is fixedly installed in babinet upper surface,Charging panel lower surface center is connected with contact block A upper surfaces,Contact block B lower surfaces are fixedly installed in babinet upper surface center,Electricity storage module is fixedly installed in babinet,Charging panel is connected with electricity storage module one end,Electricity storage module side is connected with each other with accumulator,The inventive structure is reasonable,Charging is quick,It is convenient,Safety coefficient is higher,It is and energy saving,Environmental protection,It is pollution-free,It has a extensive future.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specially a kind of unmanned plane quickly charging battery device.
Background technology
UAV referred to as " unmanned plane " (" UAV "), is controlled using radio robot and the program provided for oneself
The not manned vehicle that device manipulates.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, low cost, it is easy to use, to operational environment require low, battlefield
The advantages that survival ability is stronger.
Traditional unmanned plane charging needs battery unloading charging or wired charging, both charging modes are all more unrestrained
It is time-consuming and not convenient enough, it would therefore be highly desirable to which a kind of improved technology solves the problems, such as this in the presence of the prior art.
Invention content
The purpose of the present invention is to provide a kind of unmanned plane quickly charging battery device, when mating unmanned plane drop to charging
When on plate, contact block A and contact block B contact with each other, and the electric current in accumulator passes sequentially through contact block B, contact block A and contact plate
Electric current is radioed to the battery in unmanned plane, the charging method is quickly, conveniently；When unmanned plane flies up, contact block A and connect
Contact block B is detached, and will not have electric current to be transmitted to charging panel, safety coefficient is higher；Charging panel is made of contact plate and solar panels,
It is main to use solar energy, it is energy-saving and environmental protection, pollution-free, it has a extensive future, to solve mentioned above in the background art ask
Topic.
To achieve the above object, the present invention provides following technical solution：A kind of unmanned plane quickly charging battery device, including
Supporting leg, babinet, accumulator, charging panel, spring, contact block A, contact block B, electricity storage module, electric wire and control panel, supporting leg
There are several, supporting leg top is fixedly installed in babinet lower surface, and accumulator is fixedly installed in babinet, and charging panel is cylinder
Body, charging panel bottom are provided with groove A, and babinet top is set in groove A, and spring has several, spring top and groove A tops
It is connected, spring bottom end is fixedly installed in babinet upper surface, and charging panel lower surface center is connected with contact block A upper surfaces, connects
Contact block B lower surfaces are fixedly installed in babinet upper surface center, and contact block A is consistent with contact block B-section area, electricity storage module
Be fixedly installed in babinet, charging panel lower surface is connected with electric wire one end, the electric wire other end be set in babinet and with storing up electricity mould
Block is connected, and electricity storage module side is connected with each other with accumulator, and babinet outer surface is installed with control panel.
Preferably, charging panel includes contact plate and solar panels, and solar panels center is provided with circular groove, contact plate
It is fixedly installed in circular groove, solar panels lower surface any position is connected with electric wire.
Preferably, contact plate includes housing, PET sheet, interval insulant, coil and magnetic piece, PET sheet lower surface and separating material
Material upper surface is connected, and interval insulant lower surface is connected with coil upper surface, and coil lower surface is connected with magnetic piece upper surface, PET
Piece, interval insulant, coil and magnetic piece are fixedly installed in housing.
Preferably, control panel includes shell, display screen, switch, button, circuit board and power pack, and shell is provided on one side
Groove B, circular hole and several groove C, display screen are fixedly installed in groove B, and switch is fixedly installed in circular hole, and button fixation is set
It is placed in groove C, circuit board is fixedly installed in shell, power pack and circuit board mutual conduction.
Preferably, charging method includes the following steps：
A, unmanned plane quickly charging battery device can be positioned over open air, when there is the sun, solar panels absorb the sun
Can, solar energy will pass sequentially through solar panels, electric wire, electricity storage module and be transmitted in accumulator, achieve the purpose that electric power storage；
B, when mating unmanned plane is drop on charging panel, since pressure acts on, contact block A and contact block B are by phase mutual connection
It touches, the electric energy in accumulator will be transmitted to contact plate, then the side for passing through wireless charging by coil by contact block A and contact block B
Electric energy is transferred to mating unmanned plane by formula；
C, when mating unmanned plane flies away from charging panel, contact block A and contact block B will be disconnected from each other, and accumulator termination will be electric
Contact plate can be transferred to；
D, the switch on control panel is opened, control panel can show the electricity in accumulator on a display screen
Come.
Compared with prior art, the beneficial effects of the invention are as follows：
(1) when mating unmanned plane is drop on charging panel, contact block A and contact block B contact with each other, the electricity in accumulator
Stream passes sequentially through contact block B, contact block A and contact plate and electric current is radioed to battery in unmanned plane, and the charging method is fast
Speed, conveniently.
(2) when unmanned plane flies up, contact block A and contact block B separation will not have electric current to be transmitted to charging panel, safety
Coefficient is higher.
(3) charging panel is made of contact plate and solar panels, mainly uses solar energy, energy-saving and environmental protection, pollution-free,
It has a extensive future.
Description of the drawings
Fig. 1 is the structural diagram of the present invention.
Fig. 2 is charging plate structure schematic diagram.
Fig. 3 is contact plate structure schematic diagram.
Fig. 4 panel construction schematic diagrames in order to control.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other without making creative work
Embodiment shall fall within the protection scope of the present invention.
Referring to Fig. 1, the present invention provides a kind of technical solution：A kind of unmanned plane quickly charging battery device, including support
Leg 1, babinet 2, accumulator 3, charging panel 4, spring 5, contact block A6, contact block B7, electricity storage module 8, electric wire 9 and control panel
10, supporting leg 1 has several, and 1 top of supporting leg is fixedly installed in 2 lower surface of babinet, and accumulator 3 is fixedly installed in babinet 2,
Charging panel 4 is cylinder, and 4 bottom of charging panel is provided with groove A, and 2 top of babinet is set in groove A, and spring 5 has several, bullet
Be connected at the top of 5 top of spring and groove A, 5 bottom end of spring is fixedly installed in 2 upper surface of babinet, 4 lower surface center of charging panel and
Contact block A6 upper surfaces are connected, and contact block B7 lower surfaces are fixedly installed in 5 upper surface center of babinet, contact block A6 and contact
Block B7 areas of section are consistent, and electricity storage module 8 is fixedly installed in babinet 2, and 4 lower surface of charging panel is connected with 9 one end of electric wire, electric wire
9 other ends are set in babinet 2 and are connected with electricity storage module 8, and 8 side of electricity storage module is connected with each other with accumulator 3, outside babinet 2
Side surface is installed with control panel 10.
As shown in Fig. 2, charging panel 4 includes contact plate 41 and solar panels 42,42 center of solar panels is provided with circle
Groove, contact plate 41 are fixedly installed in circular groove, and 42 lower surface any position of solar panels is connected with electric wire 9.
As shown in figure 3, contact plate 41 includes housing 411, PET sheet 412, interval insulant 413, coil 414 and magnetic piece
415,41 lower surface of PET sheet is connected with 413 upper surface of interval insulant, 413 lower surface of interval insulant and 414 upper surface phase of coil
Even, 414 lower surface of coil is connected with 415 upper surface of magnetic piece, PET sheet 412, interval insulant 413, coil 414 and magnetic piece 415
It is fixedly installed in housing 411.
As shown in figure 4, control panel 10 include shell 101, display screen 102, switch 103, button 104, circuit board 105 and
Power pack 106, shell 101 are provided with groove B, circular hole and several groove C, display screen 102 and are fixedly installed in groove B, open on one side
103 are closed to be fixedly installed in circular hole, button 104 is fixedly installed in groove C, and circuit board 105 is fixedly installed in shell 101,
Power pack 106 and 105 mutual conduction of circuit board.
The inventive structure is reasonable, and quickly, conveniently, safety coefficient is higher, and energy-saving and environmental protection, pollution-free, application prospect for charging
It is wide.
A kind of unmanned plane quickly charging battery device, charging method include the following steps：
A, the invention can be placed in open air, when there is the sun, solar panels 42 absorb solar energy, and solar energy will lead to successively
It crosses solar panels 42, electric wire 9, electricity storage module 8 to be transmitted in accumulator 3, achievees the purpose that electric power storage.
B, when mating unmanned plane is drop on charging panel 4, since pressure acts on, contact block A6 and contact block B7 will be mutual
It contacts, the electric energy in accumulator 3 will be transmitted to contact plate 41, then pass through nothing by coil 414 by contact block A6 and contact block B7
Electric energy is transferred to mating unmanned plane by the mode of micro USB electricity.
C, when mating unmanned plane flies away from charging panel, contact block A6 and contact block B7 will be disconnected from each other, and accumulator 3 terminates will
Electric energy is transferred to contact plate 41.
D, the switch 103 on control panel 10 is opened, control panel 10 can be by the electricity in accumulator 3 in display screen
It is shown on 102, user is allowed to understand the electricity in accumulator 3.
The beneficial effects of the invention are as follows：
The inventive structure is reasonable, and quickly, conveniently, safety coefficient is higher, and energy-saving and environmental protection, pollution-free, application prospect for charging
It is wide.
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 (5)
1. a kind of unmanned plane quickly charging battery device, it is characterised in that：Including supporting leg, babinet, accumulator, charging panel, bullet
Spring, contact block A, contact block B, electricity storage module, electric wire and control panel, the supporting leg have several, the supporting leg top
The babinet lower surface is fixedly installed in, the accumulator is fixedly installed in babinet, and the charging panel is cylinder, described to fill
Battery plate bottom is provided with groove A, and the babinet top is set in groove A, and the spring has several, the spring top with it is recessed
It is connected at the top of slot A, the spring bottom end is fixedly installed in babinet upper surface, charging panel lower surface center and contact block
A upper surfaces are connected, and the contact block B lower surfaces are fixedly installed in babinet upper surface center, the contact block A and contact block
B-section area is consistent, and the electricity storage module is fixedly installed in babinet, and the charging panel lower surface is connected with electric wire one end, institute
It states the electric wire other end to be set in babinet and with electricity storage module be connected, the electricity storage module side is connected with each other with accumulator, institute
It states babinet outer surface and is installed with control panel.
2. a kind of unmanned plane quickly charging battery device according to claim 1, it is characterised in that：The charging panel includes
Contact plate and solar panels, the solar panels center are provided with circular groove, and the contact plate is fixedly installed in round recessed
In slot, solar panels lower surface any position is connected with electric wire.
3. a kind of unmanned plane quickly charging battery device according to claim 1 or 2, it is characterised in that：The contact plate
Including housing, PET sheet, interval insulant, coil and magnetic piece, the PET sheet lower surface is connected with interval insulant upper surface, described
Interval insulant lower surface is connected with coil upper surface, and the coil lower surface is connected with magnetic piece upper surface, the PET sheet,
Barrier material, coil and magnetic piece are fixedly installed in housing.
4. a kind of unmanned plane quickly charging battery device according to claim 1, it is characterised in that：The control panel packet
Shell, display screen, switch, button, circuit board and power pack are included, the shell is provided with groove B, circular hole and several groove C on one side,
The display screen is fixedly installed in groove B, and the switch is fixedly installed in circular hole, and the button is fixedly installed on groove C
Interior, the circuit board is fixedly installed in shell, the power pack and circuit board mutual conduction.
5. a kind of unmanned plane quickly charging battery device according to claim 1, it is characterised in that：Its charging method includes
Following steps：
A, unmanned plane quickly charging battery device is positioned over open air, when there is the sun, solar panels absorb solar energy, solar energy
Solar panels, electric wire, electricity storage module will be passed sequentially through to be transmitted in accumulator, achieve the purpose that electric power storage；
B, when mating unmanned plane is drop on charging panel, since pressure acts on, contact block A and contact block B will contact with each other, and store
Electric energy in battery will be transmitted to contact plate, then will be electric by way of wireless charging by coil by contact block A and contact block B
Mating unmanned plane can be transferred to；
C, when mating unmanned plane flies away from charging panel, contact block A and contact block B will be disconnected from each other, and accumulator termination passes electric energy
It is defeated by contact plate；
D, the switch on control panel is opened, control panel shows the electricity in accumulator on a display screen.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810159357.2A CN108173321A (en) | 2018-02-26 | 2018-02-26 | A kind of unmanned plane quickly charging battery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810159357.2A CN108173321A (en) | 2018-02-26 | 2018-02-26 | A kind of unmanned plane quickly charging battery device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108173321A true CN108173321A (en) | 2018-06-15 |
Family
ID=62510754
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810159357.2A Withdrawn CN108173321A (en) | 2018-02-26 | 2018-02-26 | A kind of unmanned plane quickly charging battery device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108173321A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109774935A (en) * | 2019-03-22 | 2019-05-21 | 华能安阳能源有限责任公司 | The patrol unmanned machine of wind power plant and its control system based on wireless charging technology |
-
2018
- 2018-02-26 CN CN201810159357.2A patent/CN108173321A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109774935A (en) * | 2019-03-22 | 2019-05-21 | 华能安阳能源有限责任公司 | The patrol unmanned machine of wind power plant and its control system based on wireless charging technology |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180615 |
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| WW01 | Invention patent application withdrawn after publication |