CN105914812A - Unmanned aerial vehicle battery intelligent management system - Google Patents
Unmanned aerial vehicle battery intelligent management system Download PDFInfo
- Publication number
- CN105914812A CN105914812A CN201610255331.9A CN201610255331A CN105914812A CN 105914812 A CN105914812 A CN 105914812A CN 201610255331 A CN201610255331 A CN 201610255331A CN 105914812 A CN105914812 A CN 105914812A
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- China
- Prior art keywords
- module
- management system
- intelligent management
- master control
- circuit
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Classifications
-
- 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
-
- 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
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- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses an unmanned aerial vehicle battery intelligent management system, and relates to the field of unmanned aerial vehicle equipment. The unmanned aerial vehicle battery intelligent management system comprises an MCU master control module, a power supply circuit, a protection module, a bluetooth module, a communication module, a communication interface, a display screen, a master control peripheral module, a flight control board, an upper computer and a battery measurement circuit. One end of the power supply circuit is electrically connected with the protection module, and the other end is electrically connected with the MCU master control module. The input end of the communication module is electrically connected with the MCU master control module, and the output end is electrically connected with the communication interface. The output end of the MCU master control module is electrically connected with the bluetooth module. The display screen, the master control peripheral module and the battery measurement circuit are electrically connected with the communication module. The communication interface module is electrically connected with the input end of the flight control board. The unmanned aerial vehicle battery intelligent management system capable of monitoring battery voltage, temperature and the number of times of use is provided.
Description
Technical field
The present invention relates to unmanned plane apparatus field, be specifically related to a kind of unmanned plane battery intelligent management
System.
Background technology:
In prior art, middle-size and small-size unmanned plane is because being limited by the ability of aircraft payload, no
The mode that may use large-scale unmanned plane or the generating of true airplane generator drives airborne electricity consumption
Equipment, its airborne electronic equipment system generally uses the lithium battery group of discharge and recharge capable of circulation, NI-G/nickel
Hydrogen battery group is driven, and its dynamical system of electronic unmanned plane the most generally uses Large Copacity, puts greatly
The power battery pack (lithium polymer battery, lithium Fe battery) of electricity multiplying power is driven.
Being currently used for civilian unmanned plane is mostly lithium battery, and lithium battery flattening bench is high, battery energy
Metric density is big, possesses high power endurance, and self-discharge rate is low, environmental protection, but its safety
Difference, has the danger that blast occurs, needs circuit protection, and lacks one and can detect battery electricity
Pressure, temperature, the access times of electrolytic cell and the battery management system in service life.
Summary of the invention
It is an object of the invention to provide a kind of unmanned plane battery intelligent management system, existing to solve
There is the above-mentioned multinomial defect caused in technology.
A kind of unmanned plane battery intelligent management system, including MCU main control module, power circuit,
Protection module, bluetooth module, communication module, communication interface, display screen, master control peripheral module,
Flying to control plate, host computer and cell measurement circuit, described power circuit one end is electrically connected with protection module
Connect, the other end electrically connects with MCU main control module, communication module input and MCU main control module
Electrical connection, outfan electrically connects with communication interface, MCU main control module outfan and bluetooth module
Electrical connection, display screen, master control peripheral module, cell measurement circuit are electrically connected with communication module respectively
Connecing, communication interface module electrically connects with flying control plate input.
Preferably, described MCU main control module is connected with host computer by bluetooth module.
Preferably, fly to control plate described in be connected with host computer by Digital Image Transmission module.
Preferably, described protection module includes short-circuit protection circuit, overcharge protection circuit and excessively puts
Protection circuit.
Preferably, described display screen uses OLED display screen.
Preferably, described master control peripheral module includes buzzer, LED module and key-press module.
It is an advantage of the current invention that: 1, record the access times of lithium battery, reach certain number of times,
Prohibit the use of, it is necessary to maintenance of taking away;
2, can be by voltage, electric current, temperature and the access times of liquid crystal display screen Real Time Observation battery
And the life-span;
3, wireless telecommunications, by host computer, Real Time Observation battery during aircraft flight
Electricity;
4, low-power consumption mode can be changed by button, no device is closed, save electricity consumption;
5, all use low energy-consumption electronic device, reduce the power consumption of system.
Accompanying drawing explanation
Fig. 1 is the structured flowchart of embodiment 1.
Fig. 2 is the structured flowchart of embodiment 2.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be prone to bright with effect
White understanding, below in conjunction with detailed description of the invention, is expanded on further the present invention.
Embodiment 1:
As it is shown in figure 1, a kind of unmanned plane battery intelligent management system, including MCU main control module,
Power circuit, protection module, bluetooth module, communication module, communication interface, display screen, master
Control peripheral module, fly to control plate, host computer and cell measurement circuit, described power circuit one end with
Protection module electrical connection, the other end electrically connect with MCU main control module, communication module input and
MCU main control module electrically connects, and outfan electrically connects with communication interface, and MCU main control module exports
End electrically connect with bluetooth module, display screen, master control peripheral module, cell measurement circuit respectively with
Communication module electrically connects, and communication interface module electrically connects with flying control plate input.
It should be noted that described MCU main control module is connected with host computer by bluetooth module
Connecing, MCU main control module can send data to host computer by bluetooth module to be carried out the most in real time
Display, described protection module includes short-circuit protection circuit, overcharge protection circuit and Cross prevention electricity
Road.
At the present embodiment, described display screen uses OLED display screen, described master control peripheral module
Including buzzer, LED module and key-press module.
Embodiment 2:
As in figure 2 it is shown, a kind of unmanned plane battery intelligent management system, including MCU main control module,
Power circuit, protection module, bluetooth module, communication module, communication interface, display screen, master
Control peripheral module, fly to control plate, host computer and cell measurement circuit, described power circuit one end with
Protection module electrical connection, the other end electrically connect with MCU main control module, communication module input and
MCU main control module electrically connects, and outfan electrically connects with communication interface, and MCU main control module exports
End electrically connect with bluetooth module, display screen, master control peripheral module, cell measurement circuit respectively with
Communication module electrically connects, and communication interface module electrically connects with flying control plate input.
Fly to control plate described in it should be noted that to be connected with host computer by Digital Image Transmission module
Connect, fly to control plate and real time data is sent to host computer by image transmission module shows, institute
State protection module and include short-circuit protection circuit, overcharge protection circuit and over-discharge protection circuit.
At the present embodiment, described display screen uses OLED display screen, described master control peripheral module
Including buzzer, LED module and key-press module.
Wherein, short-circuit protection circuit, it is used for occurring disconnecting circuit during short circuit, overcharges, cross and put guarantor
Protection circuit is respectively used to over-charging of battery and stops charging, crosses and stops electric discharge, cell measurement circuit when putting
For measuring the voltage of battery, electric current, temperature, OLED display screen is for showing the electricity of battery
Pressure, electric current, temperature, access times, life-span, battery abnormality, key-press module is used for setting
Putting the conversion of minimum alarm voltage and low-power consumption, LED module is made up of, no four LED
The state that same Assembled lamp bright display battery is different, buzzer is for sending out when the abnormality of the battery occurs
Go out auditory tone cues.
Based on above-mentioned, unmanned plane battery intelligent management system of the present invention, it is possible to record lithium
The access times of battery, reach certain number of times, prohibit the use of, it is necessary to maintenance of taking away, can
By voltage, electric current, temperature and access times and life-span, the energy of liquid crystal display screen Real Time Observation battery
Enough communicate wirelessly, by host computer, Real Time Observation battery electricity during aircraft flight
Amount, can change low-power consumption mode by button, be closed by no device, saves electricity consumption, entirely
Portion uses low energy-consumption electronic device, reduces the power consumption of system, and battery structure is succinct, and battery is also equipped with leading to
Communication interface.
As known by the technical knowledge, the present invention can by other essence without departing from its spirit or must
The embodiment wanting feature realizes.Therefore, embodiment disclosed above, with regard to each side
Speech, is all merely illustrative, is not only.All within the scope of the present invention or equivalent
Change in the scope of the present invention is all included in the invention.
Claims (6)
1. a unmanned plane battery intelligent management system, it is characterised in that include MCU master control
Module, power circuit, protection module, bluetooth module, communication module, communication interface, display
Screen, master control peripheral module, fly to control plate, host computer and cell measurement circuit, described power circuit
Module electrically connects, the other end electrically connects with MCU main control module with protection in one end, and communication module is defeated
Entering end to electrically connect with MCU main control module, outfan electrically connects with communication interface, MCU master control mould
Block outfan electrically connects with bluetooth module, display screen, master control peripheral module, cell measurement circuit
Electrically connecting with communication module respectively, communication interface module electrically connects with flying control plate input.
A kind of unmanned plane battery intelligent management system the most according to claim 1, it is special
Levy and be: described MCU main control module is connected with host computer by bluetooth module.
A kind of unmanned plane battery intelligent management system the most according to claim 1, it is special
Levy and be: described in fly control plate be connected with host computer by Digital Image Transmission module.
A kind of unmanned plane battery intelligent management system the most according to claim 1, it is special
Levy and be: described protection module includes short-circuit protection circuit, overcharge protection circuit and Cross prevention
Circuit.
A kind of unmanned plane battery intelligent management system the most according to claim 1, it is special
Levy and be: described display screen uses OLED display screen.
A kind of unmanned plane battery intelligent management system the most according to claim 1, it is special
Levy and be: described master control peripheral module includes buzzer, LED module and key-press module.
Priority Applications (1)
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CN201610255331.9A CN105914812A (en) | 2016-04-22 | 2016-04-22 | Unmanned aerial vehicle battery intelligent management system |
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CN201610255331.9A CN105914812A (en) | 2016-04-22 | 2016-04-22 | Unmanned aerial vehicle battery intelligent management system |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106516129A (en) * | 2016-11-10 | 2017-03-22 | 广东容祺智能科技有限公司 | Multi-rotor unmanned aerial vehicle system capable of adapting to northern ultra-low temperature environments |
CN106707192A (en) * | 2017-01-23 | 2017-05-24 | 深圳市哈威飞行科技有限公司 | Aircraft safety detection management device and safety control system |
CN107064688A (en) * | 2017-04-27 | 2017-08-18 | 广东容祺智能科技有限公司 | A kind of unmanned plane abnormal electrical power supply intelligent early-warning system |
CN108535657A (en) * | 2018-03-29 | 2018-09-14 | 深圳市道通智能航空技术有限公司 | The guard method of unmanned vehicle cell safety and its device |
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CN201699442U (en) * | 2010-05-21 | 2011-01-05 | 西安交通大学 | Battery intelligent management system |
CN103840745A (en) * | 2013-09-13 | 2014-06-04 | 武汉美格科技有限公司 | Solar energy system for unmanned plane to use |
CN105223869A (en) * | 2015-10-09 | 2016-01-06 | 浪潮集团有限公司 | Unmanned aerial vehicle battery monitoring system based on cloud calculates |
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2016
- 2016-04-22 CN CN201610255331.9A patent/CN105914812A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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CN201699442U (en) * | 2010-05-21 | 2011-01-05 | 西安交通大学 | Battery intelligent management system |
CN103840745A (en) * | 2013-09-13 | 2014-06-04 | 武汉美格科技有限公司 | Solar energy system for unmanned plane to use |
CN105223869A (en) * | 2015-10-09 | 2016-01-06 | 浪潮集团有限公司 | Unmanned aerial vehicle battery monitoring system based on cloud calculates |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106516129A (en) * | 2016-11-10 | 2017-03-22 | 广东容祺智能科技有限公司 | Multi-rotor unmanned aerial vehicle system capable of adapting to northern ultra-low temperature environments |
CN106707192A (en) * | 2017-01-23 | 2017-05-24 | 深圳市哈威飞行科技有限公司 | Aircraft safety detection management device and safety control system |
CN107064688A (en) * | 2017-04-27 | 2017-08-18 | 广东容祺智能科技有限公司 | A kind of unmanned plane abnormal electrical power supply intelligent early-warning system |
CN108535657A (en) * | 2018-03-29 | 2018-09-14 | 深圳市道通智能航空技术有限公司 | The guard method of unmanned vehicle cell safety and its device |
WO2019184386A1 (en) * | 2018-03-29 | 2019-10-03 | 深圳市道通智能航空技术有限公司 | Safety protection method for battery of unmanned aerial vehicle and device thereof |
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Application publication date: 20160831 |