CN107294168A - A kind of unmanned plane photovoltaic charger - Google Patents
A kind of unmanned plane photovoltaic charger Download PDFInfo
- Publication number
- CN107294168A CN107294168A CN201710570296.4A CN201710570296A CN107294168A CN 107294168 A CN107294168 A CN 107294168A CN 201710570296 A CN201710570296 A CN 201710570296A CN 107294168 A CN107294168 A CN 107294168A
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- CN
- China
- Prior art keywords
- resistance
- diode
- chip
- pin
- connection
- 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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- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 claims description 2
- 230000003287 optical effect Effects 0.000 claims 1
- 238000006243 chemical reaction Methods 0.000 abstract description 5
- 238000004519 manufacturing process Methods 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000005693 optoelectronics Effects 0.000 description 1
Classifications
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- H02J7/0026—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
-
- 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
- H02J7/0029—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with safety or protection devices or circuits
- H02J7/0036—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with safety or protection devices or circuits using connection detecting circuits
-
- 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
-
- 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
- H02J7/0029—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with safety or protection devices or circuits
- H02J7/00302—Overcharge protection
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a kind of unmanned plane photovoltaic charger, including solar panels T, inductance L1, diode D1 and triode V1, one end connection resistance R1, the resistance R2 and the pin 7 of chip IC 1 of the inductance L1, the resistance R1 other end connects the pin 6 and solar panels T of chip IC 1, inductance L1 other end connection diode D1 anode and the pin 1 of chip IC 1, the pin 2 of chip IC 1 is grounded.Unmanned plane photovoltaic charger circuit structure of the present invention is simple, component is few; conversion to voltage is realized using triode combination timer chip; and city's electro-mechanical wave straining element is provided with circuit; increase the stability of output voltage; also there is the function of short-circuit protection simultaneously, thus it is stable with low manufacture cost, easy to use and performance.
Description
Technical field
The present invention relates to a kind of unmanned air vehicle technique, specifically a kind of charger photovoltaic charger.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated, or fully or intermittently independently operated by car-mounted computer.
Unmanned plane needs to use battery to be powered, and is powered more than prior art using civil power, is filled out of doors
Electricity is very inconvenient, therefore needs to be improved.
The content of the invention
It is an object of the invention to provide a kind of unmanned plane photovoltaic charger simple in construction, easy to use, with solution
State the problem of being proposed in background technology.
To achieve the above object, the present invention provides following technical scheme：
A kind of unmanned plane photovoltaic charger, including solar panels T, inductance L1, diode D1 and triode V1, the inductance
L1 one end connection resistance R1, resistance R2 and the pin 7 of chip IC 1, the resistance R1 other end connects the He of pin 6 of chip IC 1
Solar panels T, inductance the L1 other end connection diode D1 anode and the pin 1 of chip IC 1, the pin 2 of chip IC 1 connect
Ground, the connection of pin 3 the electric capacity C1, electric capacity C1 of chip IC 1 other end ground connection, the connection of pin 88 of chip IC 1 connects resistance R2
The other end, chip IC 1 pin 5 connection resistance R4 and resistance R5, the resistance R6 another connection resistance R7 other end, electric power storage
Pond E negative pole and the solar panels T other end, resistance R4 other end connection resistance R3, diode D1 negative electrode, diode D2
Anode and triode V1 emitter stage, the resistance R3 other end connection diode D4 anode and resistance R5, resistance R5's is another
One end connecting triode V1 base stage, triode V1 colelctor electrode connection diode D3 anode, diode D3 negative electrode connection
Resistance R7 and diode D2 negative electrode, diode D4 negative electrode connection battery E positive pole, the model of the chip IC 1
MC34063。
It is used as the preferred scheme of the present invention：The diode D2 is green light LED, and pole pipe D3 is red light-emitting two
Pole pipe.
Compared with prior art, the beneficial effects of the invention are as follows：Unmanned plane photovoltaic charger circuit structure of the present invention is simple,
Component is few, and using solar powered, the conversion to voltage is realized using triode combination timer chip, and in circuit
In be provided with city's electro-mechanical wave straining element, increase output voltage stability, while also have short-circuit protection function, therefore tool
There is environmental protection, easy to use and performance is stablized.
Brief description of the drawings
Fig. 1 is the circuit diagram of unmanned plane photovoltaic charger.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Referring to Fig. 1, a kind of unmanned plane photovoltaic charger, including solar panels T, inductance L1, diode D1 and triode
V1, the inductance L1 one end connection resistance R1, resistance R2 and the pin 7 of chip IC 1, resistance R1 other end connection chip
IC1 pin 6 and solar panels T, the inductance L1 other end connection diode D1 anode and the pin 1 of chip IC 1, chip
IC1 pin 2 is grounded, and the connection of pin 3 the electric capacity C1, electric capacity C1 of chip IC 1 other end ground connection, the pin 8 of chip IC 1 are connected
The 8 connection resistance R2 other end, the connection resistance R4 and resistance R5 of pin 5 of chip IC 1, resistance R6 another connection resistance R7's
The other end of the other end, battery E negative pole and solar panels T, resistance R4 other end connection resistance R3, diode D1 the moon
The emitter stage of pole, diode D2 anode and triode V1, the resistance R3 other end connection diode D4 anode and resistance R5,
Resistance R5 other end connecting triode V1 base stage, triode V1 colelctor electrode connection diode D3 anode, diode D3
Negative electrode connect resistance R7 and diode D2 negative electrode, diode D4 negative electrode connection battery E positive pole, the chip IC 1
Model MC34063.
IC1 model NE555.
The present invention operation principle be：Solar panels T completes opto-electronic conversion and output voltage is powered to circuit, chip IC 1
It is conventional dc source conversion integrated circuit, it will export 12.6V voltages after 12V power boosters through R3, D4.Triode V1 is
The switching tube of charged state is detected, light emitting diode D2 and light emitting diode D3 are respectively green and red led.During charging,
Because there is charging current, pressure drop is produced on R3, triode V1 conductings, light emitting diode D3 is lighted.Full of when, protect in lithium battery
Protection cut-out electric current is overcharged on plate, light emitting diode D2 is lighted.
Unmanned plane photovoltaic charger circuit structure of the present invention is simple, component is few, using solar powered, using triode
The conversion to voltage is realized with reference to timer chip, and is provided with city's electro-mechanical wave straining element, increase output in circuit
The stability of voltage, while also there is the function of short-circuit protection, therefore it is stable with environmental protection, easy to use and performance.
Claims (2)
1. a kind of unmanned plane photovoltaic charger, including solar panels T, inductance L1, diode D1 and triode V1, its feature exist
In one end connection resistance R1, the resistance R2 and the pin 7 of chip IC 1 of the inductance L1, resistance R1 other end connection chip
IC1 pin 6 and solar panels T, the inductance L1 other end connection diode D1 anode and the pin 1 of chip IC 1, chip
IC1 pin 2 is grounded, and the connection of pin 3 the electric capacity C1, electric capacity C1 of chip IC 1 other end ground connection, the pin 8 of chip IC 1 are connected
The 8 connection resistance R2 other end, the connection resistance R4 and resistance R5 of pin 5 of chip IC 1, resistance R6 another connection resistance R7's
The other end of the other end, battery E negative pole and solar panels T, resistance R4 other end connection resistance R3, diode D1 the moon
The emitter stage of pole, diode D2 anode and triode V1, the resistance R3 other end connection diode D4 anode and resistance R5,
Resistance R5 other end connecting triode V1 base stage, triode V1 colelctor electrode connection diode D3 anode, diode D3
Negative electrode connect resistance R7 and diode D2 negative electrode, diode D4 negative electrode connection battery E positive pole, the chip IC 1
Model MC34063.
2. a kind of unmanned plane photovoltaic charger according to claim 1, it is characterised in that the diode D2 sends out for green glow
Optical diode, pole pipe D3 is red light-emitting diode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710570296.4A CN107294168A (en) | 2017-07-13 | 2017-07-13 | A kind of unmanned plane photovoltaic charger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710570296.4A CN107294168A (en) | 2017-07-13 | 2017-07-13 | A kind of unmanned plane photovoltaic charger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107294168A true CN107294168A (en) | 2017-10-24 |
Family
ID=60101788
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710570296.4A Withdrawn CN107294168A (en) | 2017-07-13 | 2017-07-13 | A kind of unmanned plane photovoltaic charger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107294168A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108497520A (en) * | 2018-05-21 | 2018-09-07 | 安徽卓特信息技术有限公司 | A kind of energy saving jujube Quick cleaning device |
| CN109089647A (en) * | 2018-07-23 | 2018-12-28 | 刘桂明 | A kind of new energy vegetable cultivation storehouse |
-
2017
- 2017-07-13 CN CN201710570296.4A patent/CN107294168A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108497520A (en) * | 2018-05-21 | 2018-09-07 | 安徽卓特信息技术有限公司 | A kind of energy saving jujube Quick cleaning device |
| CN109089647A (en) * | 2018-07-23 | 2018-12-28 | 刘桂明 | A kind of new energy vegetable cultivation storehouse |
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Legal Events
| 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: 20171024 |
|
| WW01 | Invention patent application withdrawn after publication |