CN107681737A - A kind of UAV Intelligent charging system - Google Patents

A kind of UAV Intelligent charging system Download PDF

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Publication number
CN107681737A
CN107681737A CN201711045667.3A CN201711045667A CN107681737A CN 107681737 A CN107681737 A CN 107681737A CN 201711045667 A CN201711045667 A CN 201711045667A CN 107681737 A CN107681737 A CN 107681737A
Authority
CN
China
Prior art keywords
chip
resistance
connect
pins
circuit
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.)
Pending
Application number
CN201711045667.3A
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Chinese (zh)
Inventor
王飞
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Henan Flying Guard Technology Co Ltd
Original Assignee
Henan Flying Guard Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Henan Flying Guard Technology Co Ltd filed Critical Henan Flying Guard Technology Co Ltd
Priority to CN201711045667.3A priority Critical patent/CN107681737A/en
Publication of CN107681737A publication Critical patent/CN107681737A/en
Pending legal-status Critical Current

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Classifications

    • H02J7/0022
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/024Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • H02J7/0026
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00UAVs characterised by their flight controls
    • B64U2201/20Remote controls

Abstract

The invention discloses UAV Intelligent charging system of the present invention, on the one hand circuit total system is redesigned, it is multiple functional, the trend of sunshine is on the other hand followed the trail of by automatic tracking control circuit, the moment allows the solar panel face sun, realize light-use maximization, also voltage regulator circuit is optimized simultaneously, the circuit enable automatically adjusts charging voltage according to lithium battery capacity, and circuit structure of the present invention is simple, it is cheap, it is adapted to promote the use of.UAV Intelligent charging system of the present invention, on the one hand circuit total system is redesigned, it is multiple functional, the trend of sunshine is on the other hand followed the trail of by automatic tracking control circuit, the moment allows the solar panel face sun, realize light-use maximization, also voltage regulator circuit is optimized simultaneously, the circuit enable automatically adjusts charging voltage according to lithium battery capacity, and circuit structure of the present invention is simple, it is cheap, it is adapted to promote the use of.

Description

A kind of UAV Intelligent charging system
Technical field
The present invention relates to a kind of solar recharging system, specifically a kind of UAV Intelligent charging system.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself Not manned aircraft.
Unmanned plane is limited to battery technology at present, can not accomplish for a long time continue a journey, make unmanned plane application exist it is very big Limitation.And solar energy has huge open applications potentiality as a kind of green regenerative energy sources that can forever use. But the change of the output characteristics and outside environmental elements due to solar cell has much relations, the light of scale of mass production at present It is still not high and expensive to lie prostrate cell photoelectric conversion efficiency.
If can apply to solar energy in unmanned plane, the application for unmanned plane is a very big help.
The content of the invention
It is an object of the invention to provide a kind of safe and reliable and high light energy conversion efficiency UAV Intelligent charging system, To solve the problems mentioned in the above background technology.
To achieve the above object, the present invention provides following technical scheme:
A kind of UAV Intelligent charging system, including solar components, overvoltage crowbar, automatic tracking control circuit, voltage Regulation circuit, charge management module and over electrical equipment, the voltage regulator circuit connect charge management module, filled respectively Electricity condition indicating circuit and lithium battery, lithium battery are also respectively connected with over-discharge protection circuit and automatic tracking control circuit, cross and put Electric protection circuit is also respectively connected with charging inlet and warning circuit, and the solar components connect overvoltage crowbar and oneself respectively Motion tracking control circuit, overvoltage crowbar are also respectively connected with warning circuit, outside urgent charging inlet and charge management module; The voltage regulator circuit includes chip U1, chip U2, resistance R1, electric capacity C1 and triode VT1, the chip U1 pins 1 and connected Connecting resistance R2, chip U1 pin 6 connects resistance R3, and chip U1 pins 3 connect resistance R4, and chip U1 pins 5 connect electric capacity C1, core Piece U1 pins 4 connect resistance R1, the electric capacity C1 other ends, light emitting diode D3 negative poles, resistance R7, electric capacity C2, diode D2 respectively Positive pole, inductance L4, three-phase commutation bridge Q pin 5 and cathode of lithium battery, chip U1 pins 7 connect potentiometer RP1, potentiometer respectively RP1 slide plates and the resistance R1 other ends, chip U1 pins 8 connect the potentiometer RP1 other ends, resistance R5, triode VT1 transmittings respectively Pole and diode D1 negative poles, triode VT1 base stages connect the resistance R5 other ends and the resistance R3 other ends respectively, and the resistance R2 is another One end connects the resistance R4 other ends and light emitting diode D3 positive poles respectively, and the triode VT1 colelctor electrodes connect resistance R6, resistance The R6 other ends connect the resistance R7 other ends and chip U2 pins 5 respectively, and chip U2 pins 1 connect diode D1 positive poles and melted respectively Disconnected device FU, fuse FU other end connecting valve S, switch S other end connection lithium battery anodes, the chip U2 pins 4 connect The electric capacity C2 other ends, chip U2 pins 2 connect diode D2 negative poles and the inductance L4 other ends respectively.
As the further scheme of the present invention:The chip U1 models M5232L.
As the further scheme of the present invention:The chip U2 models TWH8778.
As the further scheme of the present invention:The light emitting diode D3 is green diode.
As further scheme of the invention:The triode VT1 is PNP triode.
Compared with prior art, the beneficial effects of the invention are as follows:UAV Intelligent charging system of the present invention, on the one hand to electricity Road total system is redesigned, multiple functional, and the trend of sunshine, moment are on the other hand followed the trail of by automatic tracking control circuit Allow the solar panel face sun, realize light-use maximization, while also voltage regulator circuit is optimized, make Circuit can automatically adjust charging voltage according to lithium battery capacity, and circuit structure of the present invention is simple, cheap, and suitable popularization makes With.
Brief description of the drawings
Fig. 1 is a kind of structured flowchart of UAV Intelligent charging system;
Fig. 2 is a kind of structural representation of automatic tracking control circuit in UAV Intelligent charging system.
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 describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.It is based on Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made Embodiment, belong to the scope of protection of the invention.
Refer to Fig. 1~2, in the embodiment of the present invention, a kind of UAV Intelligent charging system, including solar components, mistake Voltage protection circuit, automatic tracking control circuit, voltage regulator circuit, charge management module and over electrical equipment, the electricity Voltage regulator circuit connects charge management module, charged state indicating circuit and lithium battery respectively, and lithium battery, which was also respectively connected with, to be put Electric protection circuit and automatic tracking control circuit, over-discharge protection circuit is also respectively connected with charging inlet and warning circuit, described Solar components connect overvoltage crowbar and automatic tracking control circuit respectively, and overvoltage crowbar is also respectively connected with alarm electricity Road, outside urgent charging inlet and charge management module;The voltage regulator circuit includes chip U1, chip U2, resistance R1, electricity Hold C1 and triode VT1, the chip U1 pins 1 connect resistance R2, and chip U1 pins 6 connect resistance R3, and chip U1 pins 3 connect Connecting resistance R4, chip U1 pin 5 connects electric capacity C1, and chip U1 pins 4 connect resistance R1, the electric capacity C1 other ends, luminous two respectively Pole pipe D3 negative poles, resistance R7, electric capacity C2, diode D2 positive poles, inductance L4, three-phase commutation bridge Q pin 5 and cathode of lithium battery, core Piece U1 pins 7 connect potentiometer RP1, potentiometer RP1 slide plates and the resistance R1 other ends respectively, and chip U1 pins 8 connect electricity respectively The position device RP1 other ends, resistance R5, triode VT1 emitter stages and diode D1 negative poles, triode VT1 base stages connect resistance respectively The R5 other ends and the resistance R3 other ends, the resistance R2 other ends are connecting the resistance R4 other ends and light emitting diode D3 just respectively Pole, the triode VT1 colelctor electrodes connect resistance R6, and the resistance R6 other ends connect the resistance R7 other ends and chip U2 pins respectively 5, chip U2 pin 1 connects diode D1 positive poles and fuse FU respectively, and fuse FU other end connecting valve S, switch S are another End connection lithium battery anode, the chip U2 pins 4 connect the electric capacity C2 other ends, and chip U2 pins 2 connect diode D2 respectively Negative pole and the inductance L4 other ends.The chip U1 models M5232L.The chip U2 models TWH8778.Described luminous two Pole pipe D3 is green diode.The triode VT1 is PNP triode.
The present invention operation principle be:Existing photovoltaic cell, the output voltage of monomer are all very low(In below 1V), this In invention, multiple photovoltaic cells are in series, form solar components.Protected by the supply network that can automatically adjust dutycycle For card when intensity of illumination changes and loads change, output voltage is basicly stable, and it is defeated to provide stable voltage for charging management chip Enter.By being monitored to the secondary voltage of supply network, charging management chip is protected not damaged because of overtension.By to electricity The voltage monitoring at pond both ends, ensure that lithium battery will not damage because of overdischarge.Due to wireless indicator and its relay network node Power reguirements be 313V, using low noise, the CMOS-type voltage regulator of high speed.Under automatic tracking controller effect, Remain the round-the-clock tracking sun.In order to prevent the solar powered deficiency caused by continuous rainy days, design is emergent to fill Circuit, during charging, wireless indicator and its node normal operation.
Fig. 2 is voltage regulator circuit, and whole system is powered by batteries to circuit, and the voltage of chip U1 pins 7 is less than interior Portion's reference voltage, chip U1 pins 3 export the pulse signal of certain frequency, and light emitting diode D3 flickers are lighted, while chip U1 Pin 6 exports low level, makes chip U2 open-minded by triode VT1, and inductance L4 obtains exciting curent, exports stable voltage, Batteries E is in charged state, is carried out as batteries E charges, the rise of batteries E both end voltages, chip U1 pins 7 Voltage be higher than internal reference voltage, chip U1 pins 3 export low level, and light emitting diode D3 extinguishes, and chip U1 pins 6 are in height Level, chip U2 shut-offs, no current flow through inductance L4, are gradually reduced voltage, provide trickle charge to batteries E, work as core When the voltage of piece U1 pins 7 is less than internal reference voltage, chip U2 is open-minded, is powered again to inductance L4, so repeatedly.
It is obvious to a person skilled in the art that the invention is not restricted to the details of above-mentioned one exemplary embodiment, Er Qie In the case of without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter From the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, the scope of the present invention is by appended power Profit requires rather than described above limits, it is intended that all in the implication and scope of the equivalency of claim by falling Change is included in the present invention.Any reference in claim should not be considered as to the involved claim of limitation.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art It is appreciated that other embodiment.

Claims (5)

1. a kind of UAV Intelligent charging system, including solar components, overvoltage crowbar, automatic tracking control circuit, electricity Voltage regulator circuit, charge management module and over electrical equipment, it is characterised in that the voltage regulator circuit connects respectively to be filled Electric management module, charged state indicating circuit and lithium battery, lithium battery are also respectively connected with over-discharge protection circuit and from motion trackings Control circuit, over-discharge protection circuit are also respectively connected with charging inlet and warning circuit, and the solar components connected respectively Voltage protection circuit and automatic tracking control circuit, overvoltage crowbar are also respectively connected with warning circuit, outside urgent charging inlet And charge management module;The voltage regulator circuit includes chip U1, chip U2, resistance R1, electric capacity C1 and triode VT1, institute State chip U1 pins 1 and connect resistance R2, chip U1 pins 6 connect resistance R3, and chip U1 pins 3 connect resistance R4, and chip U1 draws Pin 5 connect electric capacity C1, chip U1 pins 4 connect respectively resistance R1, the electric capacity C1 other ends, light emitting diode D3 negative poles, resistance R7, Electric capacity C2, diode D2 positive poles, inductance L4, three-phase commutation bridge Q pin 5 and cathode of lithium battery, chip U1 pins 7 connect electricity respectively Position device RP1, potentiometer RP1 slide plates and the resistance R1 other ends, chip U1 pins 8 connect the potentiometer RP1 other ends, resistance respectively R5, triode VT1 emitter stages and diode D1 negative poles, triode VT1 base stages connect the resistance R5 other ends respectively and resistance R3 is another One end, the resistance R2 other ends connect the resistance R4 other ends and light emitting diode D3 positive poles, the triode VT1 current collections respectively Pole connects resistance R6, and the resistance R6 other ends connect the resistance R7 other ends and chip U2 pins 5 respectively, and chip U2 pins 1 connect respectively Meet diode D1 positive poles and fuse FU, fuse FU other end connecting valve S, switch S other end connection lithium battery anodes, institute State chip U2 pins 4 and connect the electric capacity C2 other ends, chip U2 pins 2 connect diode D2 negative poles and the inductance L4 other ends respectively.
2. UAV Intelligent charging system according to claim 1, it is characterised in that the chip U1 models M5232L。
3. UAV Intelligent charging system according to claim 1, it is characterised in that the chip U2 models TWH8778。
4. UAV Intelligent charging system according to claim 1, it is characterised in that the light emitting diode D3 is green glow Diode.
5. UAV Intelligent charging system according to claim 1, it is characterised in that the triode VT1 is the poles of PNP tri- Pipe.
CN201711045667.3A 2017-10-31 2017-10-31 A kind of UAV Intelligent charging system Pending CN107681737A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711045667.3A CN107681737A (en) 2017-10-31 2017-10-31 A kind of UAV Intelligent charging system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711045667.3A CN107681737A (en) 2017-10-31 2017-10-31 A kind of UAV Intelligent charging system

Publications (1)

Publication Number Publication Date
CN107681737A true CN107681737A (en) 2018-02-09

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111775736A (en) * 2020-06-05 2020-10-16 深圳供电局有限公司 Unmanned aerial vehicle system and wireless charging device
US11565605B2 (en) 2020-10-29 2023-01-31 Wing Aviation Llc Systems and methods for battery capacity management in a fleet of UAVs

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104467088A (en) * 2014-11-28 2015-03-25 刘尚爱 Intelligent solar charging system and automatic tracking control circuit thereof
CN204361949U (en) * 2015-01-15 2015-05-27 天津市瑞通鼎科技发展有限公司 A kind of voltage regulator for automobile circuit

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104467088A (en) * 2014-11-28 2015-03-25 刘尚爱 Intelligent solar charging system and automatic tracking control circuit thereof
CN204361949U (en) * 2015-01-15 2015-05-27 天津市瑞通鼎科技发展有限公司 A kind of voltage regulator for automobile circuit

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111775736A (en) * 2020-06-05 2020-10-16 深圳供电局有限公司 Unmanned aerial vehicle system and wireless charging device
US11565605B2 (en) 2020-10-29 2023-01-31 Wing Aviation Llc Systems and methods for battery capacity management in a fleet of UAVs
US11840158B2 (en) 2020-10-29 2023-12-12 Wing Aviation Llc Systems and methods for battery capacity management in a fleet of UAVs

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Application publication date: 20180209