WO2020239034A1 - 一种电池管理方法、电池管理装置及飞行器 - Google Patents

一种电池管理方法、电池管理装置及飞行器 Download PDF

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Publication number
WO2020239034A1
WO2020239034A1 PCT/CN2020/092959 CN2020092959W WO2020239034A1 WO 2020239034 A1 WO2020239034 A1 WO 2020239034A1 CN 2020092959 W CN2020092959 W CN 2020092959W WO 2020239034 A1 WO2020239034 A1 WO 2020239034A1
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WIPO (PCT)
Prior art keywords
battery
state parameter
battery management
voltage
management device
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PCT/CN2020/092959
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English (en)
French (fr)
Inventor
秦威
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深圳市道通智能航空技术有限公司
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Publication of WO2020239034A1 publication Critical patent/WO2020239034A1/zh

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L58/00Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles
    • B60L58/10Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L58/00Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles
    • B60L58/10Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries
    • B60L58/12Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries responding to state of charge [SoC]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L58/00Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles
    • B60L58/10Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries
    • B60L58/18Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries of two or more battery modules
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/24Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/42Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
    • H01M10/4207Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells for several batteries or cells simultaneously or sequentially
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00Type of vehicles
    • B60L2200/10Air crafts
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/42Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
    • H01M10/425Structural combination with electronic components, e.g. electronic circuits integrated to the outside of the casing
    • H01M2010/4271Battery management systems including electronic circuits, e.g. control of current or voltage to keep battery in healthy state, cell balancing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries

Definitions

  • This application relates to the technical field of communication equipment, and in particular to a battery management method, a battery management device and an aircraft.
  • the main purpose of the present invention is to provide a battery management method, a battery management device and an aircraft, aiming to improve the power supply safety of a multi-battery system.
  • the present invention provides a battery management method applied to a battery management device, the battery management device is provided with a trigger, the first battery and the second battery are electrically connected to the battery management device, and the battery management Methods include:
  • the method further includes: if the second battery does not meet the voltage output condition, sending a sleep instruction to the second battery and/or the first battery, so that the second battery and/or The first battery enters a sleep mode.
  • the method further includes: generating a first presence signal if the first battery is connected to the battery management device;
  • the first presence signal is sent to the first battery to control the first battery to enter a sleep mode.
  • the method further includes: generating a second presence signal if the second battery is connected to the battery management device;
  • the second presence signal is sent to the second battery to control the second battery to enter a sleep mode.
  • the first state parameter includes a first voltage value
  • the second state parameter includes a second voltage value. Then, the second state parameter is determined according to the first state parameter and the second state parameter. Whether the battery meets the voltage output conditions, including:
  • the first state parameter includes a first power value
  • the second state parameter includes a second voltage value.
  • the second state parameter is determined according to the first state parameter and the second state parameter. Whether the battery meets the voltage output conditions, including:
  • the first state parameter includes a first number of cycles
  • the second state parameter includes a second number of cycles. Then, the second state parameter is determined according to the first state parameter and the second state parameter. Whether the battery meets the voltage output conditions, including:
  • the first state parameter includes a first voltage value, a first power value, and a first number of cycles
  • the second state parameter includes a second voltage value, a second power value, and a second number of cycles
  • the present invention also provides a battery management device.
  • the battery management device includes: a trigger, a memory and a processor;
  • the trigger is electrically connected to the processor
  • the memory is used to store a computer-executable battery management method program
  • the processor is used to retrieve an executable battery management method program stored in the memory to execute the aforementioned method.
  • the present invention also provides an aircraft including a fuselage
  • An arm connected to the fuselage
  • the power device is arranged on the arm and used to provide power for the aircraft to fly;
  • At least two batteries are provided on the fuselage and used to provide power to the aircraft;
  • the battery management device is provided in the body and electrically connected to the at least two batteries.
  • the present invention provides a battery management method, a battery management device, and an aircraft, wherein the battery management method detects whether the duration of the trigger being triggered exceeds a time threshold; if so, a trigger signal is generated And according to the trigger signal, the first battery is controlled to enter an output mode for voltage output, so that the battery management device sends a wake-up instruction to the second battery, so that the second battery enters the wake-up mode.
  • the second battery When the second battery is in the wake-up mode, obtain the first state parameter of the first battery, where the first state parameter is used to characterize the current operating state of the first battery; obtain the second state parameter of the second battery , The second state parameter is used to characterize the current operating state of the second battery; judging whether the second battery satisfies the voltage output condition according to the first state parameter and the second state parameter; if the first state parameter If the second battery satisfies the voltage output condition, an output instruction is issued to the second battery to make the second battery output voltage.
  • FIG. 1 is a flowchart of steps of a battery management method provided by the first embodiment of the present invention.
  • Fig. 2A is a structural block diagram of the battery management device cooperating with the first battery and the second battery.
  • Fig. 2B is a structural block diagram of the first battery.
  • FIG. 3 is a flowchart of the steps of a battery management method provided by the second embodiment of the present invention.
  • FIG. 4 is a structural block diagram of a battery management device provided by a third embodiment of the present invention.
  • FIG. 5 is a schematic diagram of a three-dimensional structure of an aircraft according to a fourth embodiment of the present invention.
  • the present invention provides a battery management method, a battery management device, and an aircraft, wherein the battery management method detects whether the duration of the trigger being triggered exceeds a time threshold; if so, a trigger signal is generated and controlled according to the trigger signal
  • the first battery enters an output mode for voltage output, so that the battery management device sends a wake-up instruction to the second battery, so that the second battery enters the wake-up mode.
  • the second battery When the second battery is in the wake-up mode, obtain the first state parameter of the first battery, where the first state parameter is used to characterize the current operating state of the first battery; obtain the second state parameter of the second battery , The second state parameter is used to characterize the current operating state of the second battery; judging whether the second battery satisfies the voltage output condition according to the first state parameter and the second state parameter; if the first state parameter If the second battery satisfies the voltage output condition, an output instruction is issued to the second battery to make the second battery output voltage.
  • FIG. 1 is a battery management method provided by the present invention, and the battery management method is applied to the battery management device 20.
  • the battery management device 20 is provided with a trigger and one or more plug-in ports.
  • the first battery 10 and the second battery 30 are plugged into the battery management device 20 through the plug-in ports to realize electrical connection with the battery management device 20.
  • the battery management device 20 can manage the first battery 10 and the second battery 30, where the first battery 10 can be one or more, and the second battery 30 can also be one or more, which is not limited here.
  • a trigger signal can be generated to wake up the first battery 10.
  • the first battery 10 includes a battery main body 101, a power switch 102, a control component 103, a communication interface 104 and an output interface 105.
  • the output interface 105 is used as a plug-in interface for plugging in with external electrical equipment.
  • the communication interface 104 is used to communicate with other batteries to obtain state parameters of other batteries.
  • the other batteries may be other first battery 10 or second battery 30.
  • the battery state parameters are used to characterize the current operating state of the battery, that is, the battery.
  • the SOH and/or SOC, the state parameter can be one or more of the battery voltage, power, cycle number, temperature, etc.
  • the power switch 102 is connected to the battery main body 101 and the output interface 105 for controlling the output of the battery main body 101.
  • the control component 103 is electrically connected to the battery main body 101, the power switch 102, and the communication interface 104, and is used to control the battery main body 101, the power switch 102, and the communication interface 104 to work together.
  • the power switch 102 includes a charging MOS switch and a discharging MOS switch.
  • the charging MOS switch When the charging MOS switch is turned off, the external power source cannot charge the battery body 101.
  • the discharge MOS switch is turned on, the battery main body 101 can charge an external electric device, which refers to a device or other battery that can consume electric energy.
  • the second battery 30 and the first battery 10 have the same structure, that is, the second battery 30 also includes a battery body, a power switch, a control component, a communication interface and an output interface. Because of the different locations where the battery management device 20 is connected, different names are used to distinguish them.
  • the battery management method includes:
  • Step S201 Detect whether the duration of the trigger being triggered exceeds a time threshold.
  • step S202 is executed.
  • the time threshold can be set as required, and can be 1s, 2s or 3s, and the trigger can be a button switch or a wave switch.
  • Step S202 If yes, generate a trigger signal and control the output voltage of the first battery according to the trigger signal.
  • the first battery 10 can output voltage so as to supply power to the battery management device 20.
  • Step S203 Send a wake-up instruction to the second battery, so that the second battery enters the wake-up mode.
  • the battery management device 20 After the first battery 10 supplies power to the battery management device 20, the battery management device 20 sends a wake-up command to the second battery 30 communicatively connected with the battery management device 20, so that the control component 103 of the second battery 30 is awakened.
  • Step S204 Obtain a first state parameter of the first battery, where the first state parameter is used to characterize the current operating state of the first battery.
  • acquiring the first state parameter of the first battery 10 may be that the first battery 10 periodically sends its first state parameter to the battery management device 20 at an interval T, so that the battery management device 20 can learn the The state parameter corresponding to the first battery 10, where the first state parameter is used to characterize the current operating state of the first battery 10, that is, the SOH and/or SOC parameters of the first battery 10.
  • the first state parameter may be the first battery Any one or a combination of 10 voltage, power, or cycle times, the interval time T can be set to 0.5s, 1s as needed.
  • acquiring the first state parameter of the first battery 10 may be that the battery management device 20 sends a parameter request to the first battery 10 so that when the first battery 10 receives the parameter request, it will respond to the parameter request.
  • the state parameters of the first battery 10 are sent to the battery management device 20.
  • Step S205 Obtain a second state parameter of the second battery, where the second state parameter is used to characterize the current operating state of the second battery.
  • the second state parameter is used to characterize the current operating state of the second battery 30, that is, the SOH parameter of the second battery 30.
  • the second state parameter may be one of the voltage, power, or number of cycles of the second battery 30. Any one or a combination of more.
  • Obtaining the second state parameter of the second battery 30 may be that the second battery 30 periodically sends its second state parameter to the battery management device 20 at an interval T, so that the battery management device 20 knows that the second battery 30 corresponds to Among them, the interval time T can be set to 0.5s or 1s as required.
  • obtaining the first state parameter of the second battery 30 may be that the battery management device 20 sends a parameter request to the second battery 30, so that when the second battery 30 receives the parameter request, it will respond to the parameter request.
  • the state parameters of the second battery 30 are sent to the battery management device 20.
  • Step S206 Determine whether the second battery meets a voltage output condition according to the first state parameter and the second state parameter.
  • the first state parameter includes a first voltage value
  • the second state parameter includes a second voltage value
  • the first state parameter is determined according to the first state parameter and the second state parameter. 2. Whether the battery meets the voltage output conditions, including:
  • S2061a Determine whether the difference between the first voltage value and the second voltage value is less than a voltage threshold.
  • step S2062a if the difference between the first voltage value and the second voltage value is less than the voltage threshold, step S2062a is executed, and if the difference between the first voltage value and the second voltage value is greater than or equal to the voltage threshold, then Step S2063a is executed.
  • S2062a Determine that the second battery meets a voltage output condition.
  • S2063a Determine that the second battery does not meet a voltage output condition.
  • the first state parameter includes a first electric quantity value
  • the second state parameter includes a second voltage value. Then, the judgment is performed according to the first state parameter and the second state parameter. Whether the second battery meets the voltage output conditions, including:
  • S2061b Determine whether the difference between the first power value and the second power value is less than a power threshold.
  • the power threshold is preset. If the difference between the first power value and the second power value is less than the power threshold, step S2062b is executed, and if the difference between the first power value and the second power value is greater than or equal to the power threshold, then Step S2063b is executed.
  • S2062b Determine that the second battery meets a voltage output condition.
  • S2063b Determine that the second battery does not meet the voltage output condition.
  • the first state parameter includes a first number of cycles
  • the second state parameter includes a second number of cycles
  • the first state parameter is determined based on the first state parameter and the second state parameter. 2. Whether the battery meets the voltage output conditions, including:
  • S2061c Determine whether the difference between the first cycle number and the second cycle number is less than a cycle number threshold.
  • step S2062c is executed, if the difference between the first cycle number and the second cycle number is greater than or equal to the cycle number For the threshold, step S2063c is executed.
  • S2062c Determine that the second battery meets a voltage output condition.
  • S2063c Determine that the second battery does not meet the voltage output condition.
  • the first state parameter includes a first voltage value, a first power value, and a first number of cycles
  • the second state parameter includes a second voltage value, a second power value, and a second number of cycles
  • S2061d Determine the difference between the first voltage value and the second voltage value, the difference between the first power value and the second power value, and the number of first cycles and the number of second cycles Whether the difference between is smaller than the corresponding threshold.
  • the preset voltage threshold the preset power threshold, and the preset number of cycles.
  • step S2062d If the difference between the first voltage value and the second voltage value, the difference between the first power value and the second power value, and the difference between the first cycle number and the second cycle number If the values are all smaller than the corresponding threshold value, step S2062d is executed, otherwise, step S2063d is executed.
  • S2062d Determine that the second battery meets a voltage output condition.
  • S2063d Determine that the second battery does not meet the voltage output condition.
  • Step S207 If the second battery satisfies the voltage output condition, an output instruction is issued to the second battery to make the second battery output voltage.
  • the battery management method further includes:
  • Step S208 If the second battery does not meet the voltage output condition, issue a sleep instruction to the second battery and/or the first battery, so that the second battery and/or the first battery enter Sleep mode.
  • the discharge MOS switch of the battery is turned off, so that the battery cannot output power. If the second battery 30 does not meet the condition of voltage output, a sleep instruction is sent to the first battery 10 and/or the second battery 30, so that the first battery 10 and/or the second battery 30 enters the sleep mode to avoid inter-battery factors. Differences in parameters lead to safety accidents.
  • the battery management method further includes:
  • Step S301 If the first battery is connected to the battery management device, a first presence signal is generated.
  • the battery management device 20 is provided with a first presence signal trigger. If it is detected that the first battery 10 is connected to the battery management device 20, the first presence signal trigger is triggered to generate and merge the first presence signal.
  • the first on-position signal trigger of the battery management device 20 is triggered to generate a high or low level signal, that is, a low level signal Or high level signal.
  • Step S302 Send the first presence signal to the first battery to control the first battery to enter a sleep mode.
  • the discharge MOS switch of the first battery 10 is turned off, so that the first battery 10 enters the sleep mode.
  • Step S303 Detect whether the duration of the trigger being triggered exceeds a time threshold.
  • Step S303 is the same as step S201 in FIG. 1, and will not be described in detail here.
  • Step S304 If yes, generate a trigger signal and control the output voltage of the first battery according to the trigger signal.
  • Step S304 is the same as step S202 in FIG. 1, and will not be repeated here.
  • Step S305 Send a wake-up instruction to the second battery, so that the second battery enters the wake-up mode.
  • Step S305 is the same as step S203 in FIG. 1, and will not be repeated here.
  • Step S306 Acquire a first state parameter of the first battery, where the first state parameter is used to characterize the current operating state of the first battery.
  • Step S306 is the same as step S204 in FIG. 1, and will not be repeated here.
  • Step S307 Obtain a second state parameter of the second battery, where the second state parameter is used to characterize the current operating state of the second battery;
  • Step S307 is the same as step S205 in FIG. 1 and will not be repeated here.
  • Step S308 Determine whether the second battery satisfies a voltage output condition according to the first state parameter and the second state parameter.
  • Step S308 is the same as step S206 in FIG. 1, and will not be repeated here.
  • Step S309 If the second battery satisfies the voltage output condition, an output instruction is issued to the second battery to make the second battery output voltage.
  • Step S309 is the same as step S207 in FIG. 1 and will not be repeated here.
  • Step S310 If the second battery does not meet the voltage output condition, issue a sleep instruction to the second battery and/or the first battery, so that the second battery and/or the first battery enter Sleep mode.
  • Step S310 is the same as step S208 in FIG. 1, and will not be repeated here.
  • the battery management method further includes:
  • the second presence signal is sent to the second battery to control the second battery to enter a sleep mode.
  • the battery management device 20 is provided with a second presence signal trigger. If a second battery 30 is connected to the battery management device 20, the second presence signal trigger is triggered to generate a second presence signal. When the second battery 30 receives the second presence signal, the discharge MOS switch is turned off, so that the second battery 30 enters the sleep mode.
  • the second in-position signal trigger of the battery management device 20 is triggered to generate a high or low level signal, that is, a low level signal Or high level signal.
  • the discharge MOS switch is closed, so that the second battery 30 enters the sleep mode.
  • the battery management device 20 includes a memory 201, a processor 202, a bus 203, and a trigger 204.
  • the memory 201 and the trigger 204 are electrically connected to the processor 202 through the bus 203.
  • the memory 201 includes at least one type of readable storage medium, and the readable storage medium includes flash memory, hard disk, multimedia card, card-type memory (for example, SD or DX memory, etc.), magnetic memory, magnetic disk, optical disk, etc.
  • the memory 201 may be an internal storage unit of the battery management device 20 in some embodiments, such as a hard disk of the battery management device 20. In other embodiments, the memory 201 may also be an external storage device of the battery management device 20, such as a plug-in hard disk equipped on the battery management device 20, a smart memory card (Smart Media Card, SMC), and a secure digital (Secure Digital, SD card, Flash Card, etc.
  • the memory 201 can be used not only to store application software and various data installed in the battery management device 20, such as a computer-readable battery management method program code, etc., but also to temporarily store data that has been output or will be output.
  • the processor 202 may be a central processing unit (CPU), a controller, a microcontroller, a microprocessor, or other data processing chip, and the processor 202 may call program codes stored in the memory 201 or Process the data to execute the aforementioned battery management method.
  • CPU central processing unit
  • controller controller
  • microcontroller microcontroller
  • microprocessor or other data processing chip
  • the present invention also provides an aircraft 100, which includes:
  • the power device 40, the power device 40 may be one or more, which is provided on the arm 30, and is used to provide power for the aircraft 100 to fly;
  • At least two batteries are provided in the fuselage 50 and used to provide power to the aircraft 100;
  • the aforementioned battery management device 20 is provided in the body 50 and electrically connected to at least two batteries.
  • the power device 40 includes a motor and a wing.
  • the motor is fixed to the arm 30 and connected with the wing to drive the wing to rotate and provide flight power for the aircraft 100.

Abstract

一种电池管理方法、电池管理装置(20)及飞行器(100),电池管理方法包括:检测触发器被触发的持续时间是否超过时间阈值;若是,则生成触发信号并根据触发信号控制第一电池(10)输出电压;向第二电池(30)发送唤醒指令,以使第二电池(30)进入唤醒模式;获取第一电池(10)的第一状态参数,第一状态参数用于表征第一电池(10)的当前运行状态;获取第二电池(30)的第二状态参数,第二状态参数用于表征第二电池(30)的当前运行状态;根据第一状态参数和第二状态参数判断第二电池(30)是否满足电压输出条件;若第二电池(30)满足电压输出条件,则向第二电池(30)发出输出指令,以使第二电池(30)输出电压。

Description

一种电池管理方法、电池管理装置及飞行器
本申请要求于2019年5月28日提交中国专利局、申请号为201910452984.X、申请名称为“一种电池管理方法、电池管理装置及飞行器”的中国专利申请的优先权,其全部内容通过引用结合在本申请中。
技术领域
本申请涉及通信设备技术领域,尤其涉及一种电池管理方法、电池管理装置及飞行器。
背景技术
目前,受限于锂电池技术的滞后发展,无人机等领域的续航时间普遍偏短,为了在现有电池技术的基础上提高续航时间,人们普遍的做法是增大电池在产品中的比重,产品实现的过程中由于结构等方面的限制,人们往往会采用多块电池供电的方式提高续航能力。然而,多块电池必然会增加管理的复杂和困难,必须要有一套,逻辑严密、控制合理的方法。不当的控制,很有可能带来电池的安全风险,严重时甚者导致系统崩溃,造成人员、财产的损失。
如何保障多电池系统供电的安全,是本领域技术人员亟待解决的技术问题。
发明内容
本发明的主要目的在于提供一种电池管理方法、电池管理装置及飞行器,旨在提高多电池系统的供电安全。
为实现上述目的,本发明提供一种电池管理方法,应用于电池管理装置,所述电池管理装置设置有触发器,第一电池和第二电池与所述电池管理装置电连接,所述电池管理方法包括:
检测所述触发器被触发的持续时间是否超过时间阈值;
若是,则生成触发信号并根据所述触发信号控制所述第一电池输出电压;
向所述第二电池发送唤醒指令,以使所述第二电池进入唤醒模式;
获取所述第一电池的第一状态参数,其中,所述第一状态参数用于表征所述第一电池的当前运行状态;
获取所述第二电池的第二状态参数,其中,所述第二状态参数用于表征所述第二电池的当前运行状态;
根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件;
若所述第二电池满足电压输出条件,则向所述第二电池发出输出指令,以使所述第二电池输出电压。
优选地,所述方法还包括:若所述第二电池不满足电压输出条件,则向所述第二电池和/或所述第一电池发出休眠指令,以使所述第二电池和/或所述第一电池进入休眠模式。
优选地,所述方法还包括:若所述第一电池接入所述电池管理装置时,生成第一在位信号;
将所述第一在位信号发送给所述第一电池,以控制所述第一电池进入休眠模式。
优选地,所述方法还包括:若所述第二电池接入所述电池管理装置时,生成第二在位信号;
将所述第二在位信号发送给所述第二电池,以控制所述第二电池进入休眠模式。
优选地,所述第一状态参数包括第一电压值,所述第二状态参数包括第二电压值,则,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
判断所述第一电压值和所述第二电压值之间的差值是否小于电压阈值;
若是,则判断所述第二电池满足电压输出条件。
优选地,所述第一状态参数包括第一电量值,所述第二状态参数包括第二电压值,则,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
判断所述第一电量值和所述第二电量值之间的差值是否小于电量阈值;
若是,则判断所述第二电池满足电压输出条件。
优选地,所述第一状态参数包括第一循环次数,所述第二状态参数包括第二循环次数,则,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
判断所述第一循环次数和所述第二循环次数之间的差值是否小于循环次数阈值;
若是,则判断所述第二电池满足电压输出条件。
优选地,所述第一状态参数包括第一电压值、第一电量值以及第一循环次数,所述第二状态参数包括第二电压值、第二电量值以及第二循环次数,则,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
判断所述第一电压值与所述第二电压值的差值、所述第一电量值与所述第二电量值的差值以及所述第一循环次数与所述第二循环次数之间的差值是否均小于对应的阈值;
若是,则判断所述第二电池满足电压输出条件。
本发明还提供一种电池管理装置所述电池管理装置包括:触发器、存储器以及处理器;
所述触发器与所述处理器电连接;
所述存储器用于存储计算机可执行的电池管理方法程序;
所述处理器用于调取存储在所述存储器中的可执行的电池管理方法程序,以执行前述的方法。
本发明还提供一种飞行器,所述飞行器包括机身;
机臂,与所述机身相连;
动力装置,设于所述机臂,用于给所述飞行器提供飞行的动力;
至少两个电池,所述至少两个电池设于所述机身,用于给所述飞行器提供电力;以及
前述的电池管理装置,所述电池管理装置设于所述机身并与所述至少两个电池电连接。
与现有设计相比,本发明提供了一种电池管理方法、电池管理装置及飞行器,其中该电池管理方法通过检测所述触发器被触发的持续时间是否超过时间阈值;若是,则生成触发信号并根据所述触发信号控制所述第一电池进入输出模式以进行电压输出,以使电池管理装置向所述第二电池发送唤醒指令,以使所述第二电池进入唤醒模式。第二电池处于唤醒模式时,获取所述第一电池的第一状态参数,所述第一状态参数用于表征所述第一电池的当前运行状态;获取所述第二电池的第二状态参数,所述第二状态参数用于表征所述第二电池的当前运行状态;根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件;若所述第二电池满足电压输出条件,则向所述第二电池发出输出指令,以使所述第二电池输出电压。
通过分别获取并分析第一电池和第二电池的电池状态参数,确保第一电池和第二电池的状态保持相对均衡条件下进行电压输出,防止第一电池和第二电池之间发生相互充电,或第二电池和第二电池之间发生相互充电而导致电池安全事故。
附图说明
图1为本发明第一实施例提供的一种电池管理方法的步骤流程图。
图2A为电池管理装置与第一电池和第二电池配合的结构框图。
图2B为第一电池的结构框图。
图3为本发明第二实施例提供的一种电池管理方法的步骤流程图。
图4为本发明第三实施例提供电池管理装置的结构框图。
图5为本发明第四实施例提供一种飞行器的立体结构示意图。
具体实施方式
为了使本发明的目的、技术方案及优点更加清楚明白,以下结合附图及实施例,对本发明进行进一步详细说明。应当理解,此处所描述的具体实施例仅用以解释本发明,并不用于限定本发明。基于本发明中的实施例,本领域普通 技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。
本发明提供了一种电池管理方法、电池管理装置及飞行器,其中该电池管理方法通过检测所述触发器被触发的持续时间是否超过时间阈值;若是,则生成触发信号并根据所述触发信号控制所述第一电池进入输出模式以进行电压输出,以使电池管理装置向所述第二电池发送唤醒指令,以使所述第二电池进入唤醒模式。第二电池处于唤醒模式时,获取所述第一电池的第一状态参数,所述第一状态参数用于表征所述第一电池的当前运行状态;获取所述第二电池的第二状态参数,所述第二状态参数用于表征所述第二电池的当前运行状态;根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件;若所述第二电池满足电压输出条件,则向所述第二电池发出输出指令,以使所述第二电池输出电压。
通过分别获取并分析第一电池和第二电池的电池状态参数,确保第一电池和第二电池的状态保持相对均衡条件下进行电压输出,防止第一电池和第二电池之间发生相互充电,或第二电池和第二电池之间发生相互充电而导致电池安全事故。
请参阅图1,图1为本发明提供的一种电池管理方法,该电池管理方法应用于电池管理装置20。
请参阅图2,电池管理装置20设置有触发器以及一个或多个插接口,第一电池10和第二电池30通过插接口插接于该电池管理装置20,实现与电池管理装置20的电连接,以使该电池管理装置20可以管理第一电池10和第二电池30,其中,第一电池10可以是一个或多个,第二电池30也可以是一个或多个在此不做限定。触发器被触发时可以产生触发信号,以唤醒第一电池10。
请参阅图3,第一电池10包括电池主体101、电源开关102、控制组件103、通信接口104以及输出接口105。
其中,输出接口105作为插接口,用于与外部的用电设备进行插接。通信接口104用于其他电池通信连接以获取其他电池的状态参数,该其他电池可以是其他的第一电池10或第二电池30,电池的状态参数用于表征电池的当前运行状态,也即电池的SOH和/或SOC,状态参数可以是电池的电压、电量、循环次数、温度等其中一个或多个。
电源开关102与电池主体101和输出接口105连接,用于控制电池主体101的输出。
控制组件103与电池主体101、电源开关102以及通信接口104电连接,用于控制电池主体101、电源开关102以及通信接口104协同工作。
其中,电源开关102包括充电MOS开关和放电MOS开关,充电MOS开关关闭时,外部电源无法给电池主体101充电。放电MOS开关打开时,电池主体101可以给外部用电设备充电,该用电设备指的是可以消耗电能的设备或其他 电池。
第二电池30和第一电池10具有相同的结构,也即第二电池30也包括电池主体、电源开关、控制组件、通信接口以及输出接口。其由于接入电池管理装置20的位置不同,采用不同的名称进行区分。
请参阅图1,该电池管理方法包括:
步骤S201:检测所述触发器被触发的持续时间是否超过时间阈值。
用户若想开启第一电池10时,通过触发设置于电池管理装置20上的触发器。若该触发器被触发的时间超过时间阈值时,执行步骤S202。
其中,时间阈值可以根据需要设定,可以为1s,2s或3s,该触发器可以是按钮开关或波动开关。
步骤S202:若是,则生成触发信号并根据所述触发信号控制所述第一电池输出电压。
放电MOS开关打开时,第一电池10可以进行电压输出从而可以给电池管理装置20进行供电。
步骤S203:向所述第二电池发送唤醒指令,以使所述第二电池进入唤醒模式。
第一电池10为电池管理装置20供电后,电池管理装置20向与该电池管理装置20通信连接的第二电池30发送唤醒指令,以使第二电池30的控制组件103被唤醒。
步骤S204:获取所述第一电池的第一状态参数,所述第一状态参数用于表征所述第一电池的当前运行状态。
部分实施例中,获取第一电池10的第一状态参数可以是,第一电池10以间隔时间T,周期性将其第一状态参数发送给电池管理装置20,以使电池管理装置20获知该第一电池10对应的状态参数,其中,第一状态参数用于表征第一电池10的当前运行状态,也即第一电池10的SOH和/或SOC参数,该第一状态参数可以第一电池10的电压、电量或循环次数中的任意一者或多者组合,间隔时间T可以根据需要设定为0.5s、1s。
在部分实施例中,获取第一电池10的第一状态参数可以是,电池管理装置20向第一电池10发送参数请求,以使第一电池10接收到该参数请求时,响应该参数请求将该第一电池10的状态参数发送给电池管理装置20。
步骤S205:获取所述第二电池的第二状态参数,所述第二状态参数用于表征所述第二电池的当前运行状态。
部分实施例中,第二状态参数用于表征第二电池30的当前运行状态,也即第二电池30的SOH参数,该第二状态参数可以第二电池30的电压、电量或循环次数中的任意一者或多者组合。
获取第二电池30的第二状态参数可以是,第二电池30以间隔时间T,周期性将其第二状态参数发送给电池管理装置20,以使电池管理装置20获知该第二电池30对应的状态参数,其中,间隔时间T可以根据需要设定为0.5s、 1s。
在部分实施例中,获取第二电池30的第一状态参数可以是,电池管理装置20向第二电池30发送参数请求,以使第二电池30接收到该参数请求时,响应该参数请求将该第二电池30的状态参数发送给电池管理装置20。
步骤S206:根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件。
在部分实施例中,所述第一状态参数包括第一电压值,所述第二状态参数包括第二电压值,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
S2061a:判断所述第一电压值和所述第二电压值之间的差值是否小于电压阈值。
预设电压阈值,若第一电压值和第二电压值之间的差值小于电压阈值,则执行步骤S2062a,若第一电压值和第二电压值之间的差值大于或等于电压阈值则执行步骤S2063a。
S2062a:判断所述第二电池满足电压输出条件。
S2063a:判断所述第二电池不满足电压输出条件。
在部分实施例中,所述第一状态参数包括第一电量值,所述第二状态参数包括第二电压值,则,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
S2061b:判断所述第一电量值和所述第二电量值之间的差值是否小于电量阈值。
预设电量阈值,若第一电量值和第二电量值之间的差值小于电量阈值,则执行步骤S2062b,若第一电量值和第二电量值之间的差值大于或等于电量阈值则执行步骤S2063b。
S2062b:判断所述第二电池满足电压输出条件。
S2063b:判断所述第二电池不满足电压输出条件。
在部分实施例中,所述第一状态参数包括第一循环次数,所述第二状态参数包括第二循环次数,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
S2061c:判断所述第一循环次数和所述第二循环次数之间的差值是否小于循环次数阈值。
预设循环次数,若第一循环次数和第二循环次数之间的差值小于循环次数阈值,则执行步骤S2062c,若第一循环次数和第二循环次数之间的差值大于或等于循环次数阈值则执行步骤S2063c。
S2062c:判断所述第二电池满足电压输出条件。
S2063c:判断所述第二电池不满足电压输出条件。
在部分实施例中,所述第一状态参数包括第一电压值、第一电量值以及第一循环次数,所述第二状态参数包括第二电压值、第二电量值以及第二循环次 数,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
S2061d:判断所述第一电压值与所述第二电压值的差值、所述第一电量值与所述第二电量值的差值以及所述第一循环次数与所述第二循环次数之间的差值是否均小于对应的阈值。
即,预设电压阈值,预设电量阈值,预设循环次数。
判断第一电压值和第二电压值之间的差值是否小于电压阈值;
判断第一电量值和第二电量值之间的差值是否小于电量阈值;
判断第一循环次数和第二循环次数之间的差值是否小于循环次数阈值;
若第一电压值与所述第二电压值的差值、所述第一电量值与所述第二电量值的差值以及所述第一循环次数与所述第二循环次数之间的差值均小于对应的阈值,则执行步骤S2062d,否则执行步骤S2063d。
S2062d:判断所述第二电池满足电压输出条件。
S2063d:判断所述第二电池不满足电压输出条件。
步骤S207:若所述第二电池满足电压输出条件,则向所述第二电池发出输出指令,以使所述第二电池输出电压。
若检测到第二电池30满足电压输出条件,则向第二电池30发出输出指令,以使第二电池30开启放电MOS开关,从而使得第二电池30输出电压。
在部分实施例中,电池管理方法还包括:
步骤S208:若所述第二电池不满足电压输出条件,则向所述第二电池和/或所述第一电池发出休眠指令,以使所述第二电池和/或所述第一电池进入休眠模式。
休眠模式为电池的放电MOS开关关闭,从而使得电池无法输出电量。若第二电池30不满足电压输出的条件,则向第一电池10和/或第二电池30发送休眠指令,使得第一电池10和/或第二电池30进入休眠模式,避免电池之间因参数差异导致安全事故。
请参阅图3,在部分实施例中,所述电池管理方法还包括:
步骤S301:若所述第一电池接入所述电池管理装置时,生成第一在位信号。
电池管理装置20设置有第一在位信号触发器,若检测到有第一电池10接入电池管理装置20时,第一在位信号触发器被触发,从而生成并第一在位信号。
例如,当第一电池10接入该电池管理装置20时,电池管理装置20的第一在位信号触发器被触发,生成一个被拉高或拉低的电平信号,也即低电平信号或高电平信号。
步骤S302:将所述第一在位信号发送给所述第一电池,以控制所述第一电池进入休眠模式。
第一电池10接收到该第一在位信号时,关闭第一电池10的放电MOS开关, 使第一电池10进入休眠模式。
步骤S303:检测所述触发器被触发的持续时间是否超过时间阈值。
步骤S303与图1的步骤S201相同,在此不做赘述。
步骤S304:若是,则生成触发信号并根据所述触发信号控制所述第一电池输出电压。
步骤S304与图1的步骤S202相同,在此不做赘述。
步骤S305:向所述第二电池发送唤醒指令,以使所述第二电池进入唤醒模式。
步骤S305与图1的步骤S203相同,在此不做赘述。
步骤S306:获取所述第一电池的第一状态参数,所述第一状态参数用于表征所述第一电池的当前运行状态。
步骤S306与图1的步骤S204相同,在此不做赘述。
步骤S307:获取所述第二电池的第二状态参数,所述第二状态参数用于表征所述第二电池的当前运行状态;
步骤S307与图1的步骤S205相同,在此不做赘述。
步骤S308:根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件。
步骤S308与图1的步骤S206相同,在此不做赘述。
步骤S309:若所述第二电池满足电压输出条件,则向所述第二电池发出输出指令,以使所述第二电池输出电压。
步骤S309与图1的步骤S207相同,在此不做赘述。
步骤S310:若所述第二电池不满足电压输出条件,则向所述第二电池和/或所述第一电池发出休眠指令,以使所述第二电池和/或所述第一电池进入休眠模式。
步骤S310与图1的步骤S208相同,在此不做赘述。
在部分实施例中,所述的电池管理方法还包括:
若所述第二电池接入所述电池管理装置时,生成第二在位信号;
将所述第二在位信号发送给所述第二电池,以控制所述第二电池进入休眠模式。
具体地,电池管理装置20设置有第二在位信号触发器,若有第二电池30接入电池管理装置20时,第二在位信号触发器被触发,从而生成并第二在位信号。第二电池30接收到该第二在位信号时,关闭放电MOS开关,使第二电池30进入休眠模式。
例如,当第二电池30接入该电池管理装置20时,电池管理装置20的第二在位信号触发器被触发,生成一个被拉高或拉低的电平信号,也即低电平信号或高电平信号。第二电池30接收到电平信号时,关闭放电MOS开关,使第二电池30进入休眠模式。
请参阅图4,在部分实施例中,电池管理装置20包括存储器201、处理器 202、总线203以及触发器204,存储器201、触发器204通过总线203与处理器202电连接。
其中,存储器201至少包括一种类型的可读存储介质,所述可读存储介质包括闪存、硬盘、多媒体卡、卡型存储器(例如,SD或DX存储器等)、磁性存储器、磁盘、光盘等。存储器201在一些实施例中可以是电池管理装置20的内部存储单元,例如该电池管理装置20的硬盘。存储器201在另一些实施例中也可以是电池管理装置20的外部存储设备,例如电池管理装置20上配备的插接式硬盘,智能存储卡(Smart Media Card,SMC),安全数字(Secure Digital,SD)卡,闪存卡(Flash Card)等。存储器201不仅可以用于存储安装于电池管理装置20的应用软件及各类数据,例如计算机可读的电池管理方法程序的代码等,还可以用于暂时地存储已经输出或者将要输出的数据。
处理器202在一些实施例中可以是中央处理器(Central Processing Unit,CPU)、控制器、微控制器、微处理器或其他数据处理芯片,处理器202可调用存储器201中存储的程序代码或处理数据,以执行前述的电池管理方法。
请参阅图5,本发明还提供一种飞行器100,该飞行器100包括:
机身50;
机臂30,该机臂30与机身50相连;
动力装置40,该动力装置40可以为一个或多个,其设于机臂30,用于给飞行器100提供飞行的动力;
至少两个电池(图未示),所述至少两个电池设于机身50,用于给飞行器100提供电力;以及
前述的电池管理装置20,该电池管理装置20设于机身50并与至少两个电池电连接。
该动力装置40包括马达和机翼,马达固定于机臂30并与机翼连接,用于驱动机翼转动,以为飞行器100提供飞行动力。
以上仅为本发明的优选实施例,并非因此限制本发明的专利范围,凡是利用本发明说明书及附图内容所作的等效结构或等效流程变换,或直接或间接运用在其他相关的技术领域,均同理包括在本发明的专利保护范围内。

Claims (10)

  1. 一种电池管理方法,应用于电池管理装置,所述电池管理装置设置有触发器,第一电池和第二电池与所述电池管理装置电连接,其特征在于,所述电池管理方法包括:
    检测所述触发器被触发的持续时间是否超过时间阈值;
    若是,则生成触发信号并根据所述触发信号控制所述第一电池输出电压;
    向所述第二电池发送唤醒指令,以使所述第二电池进入唤醒模式;
    获取所述第一电池的第一状态参数,其中,所述第一状态参数用于表征所述第一电池的当前运行状态;
    获取所述第二电池的第二状态参数,其中,所述第二状态参数用于表征所述第二电池的当前运行状态;
    根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件;
    若所述第二电池满足电压输出条件,则向所述第二电池发出输出指令,以使所述第二电池输出电压。
  2. 如权利要求1所述的电池管理方法,其特征在于,所述方法还包括:
    若所述第二电池不满足电压输出条件,则向所述第二电池和/或所述第一电池发出休眠指令,以使所述第二电池和/或所述第一电池进入休眠模式。
  3. 如权利要求1所述的电池管理方法,其特征在于,所述方法还包括:
    若所述第一电池接入所述电池管理装置时,生成第一在位信号;
    将所述第一在位信号发送给所述第一电池,以控制所述第一电池进入休眠模式。
  4. 如权利要求3所述的电池管理方法,其特征在于,所述方法还包括:
    若所述第二电池接入所述电池管理装置时,生成第二在位信号;
    将所述第二在位信号发送给所述第二电池,以控制所述第二电池进入休眠模式。
  5. 如权利要求1-4任意一项所述的电池管理方法,其特征在于,所述第一状态参数包括第一电压值,所述第二状态参数包括第二电压值,则,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
    判断所述第一电压值和所述第二电压值之间的差值是否小于电压阈值;
    若是,则判断所述第二电池满足电压输出条件。
  6. 如权利要求1-4任意一项所述的电池管理方法,其特征在于,所述第一状态参数包括第一电量值,所述第二状态参数包括第二电压值,则,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
    判断所述第一电量值和所述第二电量值之间的差值是否小于电量阈值;
    若是,则判断所述第二电池满足电压输出条件。
  7. 如权利要求1-4任意一项所述的电池管理方法,其特征在于,所述第一状态参数包括第一循环次数,所述第二状态参数包括第二循环次数,则,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
    判断所述第一循环次数和所述第二循环次数之间的差值是否小于循环次数阈值;
    若是,则判断所述第二电池满足电压输出条件。
  8. 如权利要求1-4任意一项所述的电池管理方法,其特征在于,所述第一状态参数包括第一电压值、第一电量值以及第一循环次数,所述第二状态参数包括第二电压值、第二电量值以及第二循环次数,则,所述根据所述第一状态参数和所述第二状态参数判断所述第二电池是否满足电压输出条件,包括:
    判断所述第一电压值与所述第二电压值的差值、所述第一电量值与所述第二电量值的差值以及所述第一循环次数与所述第二循环次数之间的差值是否均小于对应的阈值;
    若是,则判断所述第二电池满足电压输出条件。
  9. 一种电池管理装置,其特征在于,所述电池管理装置包括:触发器、存储器以及处理器;
    所述触发器与所述处理器电连接;
    所述存储器用于存储计算机可执行的电池管理方法程序;
    所述处理器用于调取存储在所述存储器中的可执行的电池管理方法程序,以执行如权利要求1-8任一项所述的方法。
  10. 一种飞行器,其特征在于,所述飞行器包括:
    机身;
    机臂,与所述机身相连;
    动力装置,设于所述机臂,用于给所述飞行器提供飞行的动力;
    至少两个电池,所述至少两个电池设于所述机身,用于给所述飞行器提供电力;以及
    如权利要求9所述的电池管理装置,所述电池管理装置设于所述机身并与所述至少两个电池电连接。
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