CN105914812A - Unmanned aerial vehicle battery intelligent management system - Google Patents

Unmanned aerial vehicle battery intelligent management system Download PDF

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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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CN
China
Prior art keywords
module
management system
intelligent management
master control
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
CN201610255331.9A
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Chinese (zh)
Inventor
彭辉
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.)
Guangdong Rongqi Intelligent Technology Co Ltd
Original Assignee
Guangdong Rongqi Intelligent 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 Guangdong Rongqi Intelligent Technology Co Ltd filed Critical Guangdong Rongqi Intelligent Technology Co Ltd
Priority to CN201610255331.9A priority Critical patent/CN105914812A/en
Publication of CN105914812A publication Critical patent/CN105914812A/en
Pending legal-status Critical Current

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Classifications

    • 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
    • H02J7/0047Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with monitoring or indicating devices or circuits
    • 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
    • H02J7/0029Circuit 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

A kind of unmanned plane battery intelligent management system
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.
CN201610255331.9A 2016-04-22 2016-04-22 Unmanned aerial vehicle battery intelligent management system Pending CN105914812A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610255331.9A CN105914812A (en) 2016-04-22 2016-04-22 Unmanned aerial vehicle battery intelligent management system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610255331.9A CN105914812A (en) 2016-04-22 2016-04-22 Unmanned aerial vehicle battery intelligent management system

Publications (1)

Publication Number Publication Date
CN105914812A true CN105914812A (en) 2016-08-31

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Cited By (4)

* Cited by examiner, † Cited by third party
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

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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)

* Cited by examiner, † Cited by third party
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