CN104008293B - Suppress the method for designing of power battery module thermal runaway extension - Google Patents
Suppress the method for designing of power battery module thermal runaway extension Download PDFInfo
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Abstract
本发明提供一种抑制动力电池模块热失控扩展的设计方案,包括:对于一第一动力电池单体进行在绝热环境中的加热热失控实验;对于所述加热热失控实验结果建立一第一数学模型;对于一第二动力电池单体进行某种热失控触发实验;对于所述热失控触发实验的实验结果建立一第二数学模型;根据所述第一数学模型以及第二数学模型,建立热失控扩展的第三数学模型;进行热失控扩展实验,利用热失控扩展的实验结果验证第三数学模型;减小第三数学模型中次节扩展电池的电量,通过仿真计算,获得能够抑制热失控扩展的次节扩展电池的放电量;对于所述每个次节扩展电池的放电量进行实验验证,获得抑制所述动力电池模块热失控扩展的设计方案。
The present invention provides a design scheme for suppressing thermal runaway expansion of a power battery module, including: conducting a heating thermal runaway experiment in an adiabatic environment for a first power battery unit; establishing a first mathematical model for the heating thermal runaway experiment results Model; carry out a certain thermal runaway trigger experiment for a second power battery cell; establish a second mathematical model for the experimental results of the thermal runaway trigger experiment; according to the first mathematical model and the second mathematical model, establish a thermal runaway The third mathematical model of runaway expansion; carry out thermal runaway expansion experiments, and use the experimental results of thermal runaway expansion to verify the third mathematical model; reduce the power of the secondary extended battery in the third mathematical model, and obtain the ability to suppress thermal runaway through simulation calculations The discharge capacity of the expanded sub-section extended battery; experimental verification is performed on the discharge capacity of each sub-section extended battery, and a design scheme for suppressing thermal runaway expansion of the power battery module is obtained.
Description
技术领域technical field
本发明属于电池领域,涉及一种抑制动力电池模块热失控扩展的设计方法。The invention belongs to the field of batteries, and relates to a design method for suppressing thermal runaway expansion of a power battery module.
背景技术Background technique
在能源危机与环境污染的双重压力下,汽车动力系统电动化成为了汽车发展的重要标志之一。当前,新能源车动力电池系统多采用具有较高能量密度的动力电池,如锂离子动力电池。然而,偶发的安全事故使得锂离子动力电池系统受到质疑。Under the dual pressure of energy crisis and environmental pollution, the electrification of automobile power system has become one of the important symbols of automobile development. At present, the power battery system of new energy vehicles mostly uses power batteries with high energy density, such as lithium-ion power batteries. However, occasional safety accidents make the lithium-ion power battery system questioned.
动力电池系统事故一般是由动力电池发生热失控造成的。动力电池热失控是指由于动力电池内部材料在一定温度下,将化学能瞬间转化为热能的过程。动力电池系统通常包含多节串并联连接的单体动力电池,部分电池单体发生热失控之后,剧烈释放出的热能将会波及周围的电池,导致周围电池继续因受到高温加热而发生热失控。这种周围电池受到已有热失控影响继而发生热失控的过程,称为热失控的扩展过程。热失控的扩展是非常危险的,这意味着动力电池系统局部发生热失控后,整个系统都将因为热失控的扩展而发生热失控。防止动力电池系统内的热失控扩展的发生,将热失控限制在局部,将能够大大提高动力电池系统的安全性能,保证人民群众的生命财产安全。Power battery system accidents are generally caused by thermal runaway of the power battery. Power battery thermal runaway refers to the process of instantaneously converting chemical energy into heat energy due to the internal materials of the power battery at a certain temperature. The power battery system usually includes multiple single power batteries connected in series and parallel. After some battery cells experience thermal runaway, the heat energy released violently will spread to the surrounding batteries, causing the surrounding batteries to continue to be thermally runaway due to high temperature heating. This process in which the surrounding batteries are affected by the existing thermal runaway and then thermal runaway occurs is called the expansion process of thermal runaway. The expansion of thermal runaway is very dangerous, which means that after the local thermal runaway of the power battery system occurs, the entire system will experience thermal runaway due to the expansion of thermal runaway. Preventing the occurrence of thermal runaway expansion in the power battery system and limiting thermal runaway to local areas will greatly improve the safety performance of the power battery system and ensure the safety of people's lives and property.
然而,目前的抑制动力电池模块热失控扩展的设计方案,只是通过试错的方法,进行大量的实验以确定设计参数,该方法耗时耗力,而且精确度不高。如果可以设计出一种效率且精度均较高的抑制动力电池模块热失控扩展的方案,将有十分重要的意义。However, the current design scheme for suppressing the thermal runaway expansion of the power battery module is only through trial and error, and a large number of experiments are carried out to determine the design parameters. This method is time-consuming and labor-intensive, and the accuracy is not high. It will be of great significance if a scheme with high efficiency and high precision can be designed to suppress the thermal runaway expansion of the power battery module.
发明内容Contents of the invention
有鉴于此,确有必要提供一种效率且精度均较高的抑制动力电池模块热失控扩展的设计方法。In view of this, it is indeed necessary to provide a design method with high efficiency and high precision to suppress thermal runaway expansion of the power battery module.
本发明提供一种抑制动力电池模块热失控扩展的设计方法,其包括以下步骤:The invention provides a design method for suppressing thermal runaway expansion of a power battery module, which includes the following steps:
S1:在绝热环境下对一第一动力电池单体进行加热热失控实验,并记录所述第一动力电池单体在不同时刻的温度T(t);S1: Conduct a heating thermal runaway experiment on a first power battery cell in an adiabatic environment, and record the temperature T(t) of the first power battery cell at different times;
S2:建立所述第一动力电池单体在加热热失控实验过程中的一第一数学模型T(t)I,利用T(t)标定该第一数学模型T(t)I,所述第一数学模型T(t)I为所述第一动力电池单体在加热热失控条件下在某一时刻t的温度;S2: Establish a first mathematical model T(t) I of the first power battery cell during the heating thermal runaway experiment, use T(t) to calibrate the first mathematical model T(t) I , the first mathematical model T(t) I A mathematical model T(t) I is the temperature of the first power battery cell at a certain time t under heating thermal runaway conditions;
S3:提供一第二动力电池单体,该第二动力电池单体与所述第一动力电池单体相同,对所述第二动力电池单体进行热失控触发实验,并记录该第二动力电池单体在不同时刻的温度T′(t);S3: Provide a second power battery unit, the second power battery unit is the same as the first power battery unit, conduct a thermal runaway trigger test on the second power battery unit, and record the second power The temperature T'(t) of the battery cell at different times;
S4:建立所述第二动力电池单体在热失控触发实验过程中的一第二数学模型T(t)II,并利用T′(t)标定所述第二数学模型T(t)II,所述第二数学模型T(t)II为所述第二动力电池单体在热失控触发实验过程中在某一时刻t的温度;S4: Establish a second mathematical model T(t) II of the second power battery cell during the thermal runaway triggering experiment, and use T′(t) to calibrate the second mathematical model T(t) II , The second mathematical model T(t) II is the temperature of the second power battery cell at a certain moment t during the thermal runaway triggering experiment;
S5:对一第一动力电池模块进行加热热失控扩展实验,该第一动力电池模块包括至少两节电池单体,该电池单体与所述第一动力电池单体以及第二动力电池单体相同,且该第一动力电池模块中的热失控触发形式与所述第二动力电池单体的热失控触发形式相同,记录所述第一动力电池模块不同时刻的温度T″(t);S5: Conduct a heating thermal runaway expansion experiment on a first power battery module, the first power battery module includes at least two battery cells, the battery cells are connected to the first power battery cell and the second power battery cell The same, and the thermal runaway trigger form in the first power battery module is the same as the thermal runaway trigger form of the second power battery cell, record the temperature T"(t) of the first power battery module at different times;
S6:通过所述第一数学模型T(t)I以及所述第二数学模型T(t)II获得所述动力电池模块在加热热失控扩展实验过程中的一第三数学模型T(t)III,利用T″(t)标定该第三数学模型T(t)III,所述第三数学模型T(t)III为所述第一动力电池模块在加热热失控扩展实验过程中在某一时刻t的温度;S6: Obtain a third mathematical model T(t) of the power battery module during the heating thermal runaway expansion experiment process through the first mathematical model T(t) I and the second mathematical model T(t) II III , using T″(t) to calibrate the third mathematical model T(t) III , the third mathematical model T(t) III is the temperature of the first power battery module during a heating thermal runaway expansion experiment. temperature at time t;
S7:将所述第一动力电池模块中发生热失控触发的电池单体定义为首节触发电池,将首节触发电池之外的电池单体定义为次节扩展电池,减小第三数学模型T(t)III中每个次节扩展电池的电量,并通过第三数学模型T(t)III进行仿真计算,获得能够抑制所述第一动力电池模块热失控扩展的每个次节扩展电池的放电量;S7: Define the battery cell triggered by thermal runaway in the first power battery module as the first trigger battery, define the battery cells other than the first trigger battery as the second extended battery, and reduce the third mathematical model T (t) III , the power of each sub-section extended battery in the third mathematical model T(t) III is simulated to obtain the power of each sub-section extended battery that can suppress the thermal runaway expansion of the first power battery module Discharge capacity;
S8:选取一第二动力电池模块,该第二动力电池模块与所述第一动力模块相同,减小所述第二动力电池模块中次节扩展电池的电量后,对所述第二动力电池模块进行热失控扩展实验,该第二动力电池模块中的热失控触发形式与所述第一动力电池模块的热失控触发形式相同,利用所述第二动力电池模块热失控扩展实验的实验结果对所述每个次节扩展电池的放电量进行实验验证,确定能够抑制热失控扩展的每个次节扩展电池的放电量的设计参数,获得抑制动力电池模块热失控扩展的设计方法。S8: Select a second power battery module, the second power battery module is the same as the first power module, after reducing the power of the second extended battery in the second power battery module, power the second power battery Module conducts thermal runaway expansion experiment, the thermal runaway trigger form in the second power battery module is the same as the thermal runaway trigger form of the first power battery module, using the experimental results of the second power battery module thermal runaway expansion experiment The discharge capacity of each sub-section extended battery is verified experimentally, the design parameters of the discharge capacity of each sub-section extended battery capable of suppressing the expansion of thermal runaway are determined, and a design method for suppressing the expansion of thermal runaway of the power battery module is obtained.
本发明提供的抑制动力电池模块热失控扩展的设计方法,通过建立动力电池模块热失控扩展过程的数学模型,并利用该数学模型进行仿真计算获得所述每个次节扩展电池的放电量的参数,并对所述放电量的参数进行实验验证,通过在首节触发电池单体发生热失控触发之后,按照所述放电量的参数对所述次节扩展电池单体进行快速放电,达到抑制热失控的扩展的目的。该设计方案能够大大地缩短实验时间,提高效率,并有效节约研发成本。另外,该设计方法通过实验验证精确度较高。The design method for suppressing the thermal runaway expansion of the power battery module provided by the present invention is to establish a mathematical model of the thermal runaway expansion process of the power battery module, and use the mathematical model to perform simulation calculations to obtain the parameters of the discharge capacity of each sub-section extended battery , and carry out experimental verification on the parameters of the discharge capacity. After the thermal runaway trigger of the battery cells triggered in the first section is triggered, the extended battery cells in the second section are quickly discharged according to the parameters of the discharge capacity, so as to suppress heat. The purpose of uncontrolled expansion. This design scheme can greatly shorten the experimental time, improve efficiency, and effectively save research and development costs. In addition, the design method is verified by experiments with high accuracy.
附图说明Description of drawings
图1为本发明实施例中第一数学模型的计算结果与实验结果对比图。Fig. 1 is a comparison chart of the calculation results and the experimental results of the first mathematical model in the embodiment of the present invention.
图2为本发明实施例中第二数学模型的计算结果与实验结果对比图。Fig. 2 is a comparison chart of the calculation results and the experimental results of the second mathematical model in the embodiment of the present invention.
图3为本发明实施例中提供的动力电池模块的结构示意图。Fig. 3 is a schematic structural diagram of a power battery module provided in an embodiment of the present invention.
图4为本发明实施例中通过第三数学模型得到的电池单体的计算结果与实验结果对比图。FIG. 4 is a comparison chart of calculation results and experimental results of a battery cell obtained through a third mathematical model in an embodiment of the present invention.
图5为本发明实施例中通过第三数学模型得到的电池极柱的计算结果与实验结果对比图。Fig. 5 is a comparison chart of the calculation results and the experimental results of the battery pole obtained through the third mathematical model in the embodiment of the present invention.
图6为本发明实施例中减小次节扩展电池的电量后热失控扩展的仿真计算结果。FIG. 6 is a simulation calculation result of expansion of thermal runaway after reducing the power of the secondary extended battery in the embodiment of the present invention.
图7为本发明实施例中第2至第6节电池单体的荷电状态为75%时的实验结果。FIG. 7 is an experimental result when the state of charge of the second to sixth battery cells is 75% in the embodiment of the present invention.
图8为本发明实施例中第2至第6节电池单体的荷电状态为50%时的实验结果。FIG. 8 is an experimental result when the state of charge of the second to sixth battery cells is 50% in the embodiment of the present invention.
图9为本发明实施例提供的通过放电抑制热失控扩展的电池模块设计方法的结构框图。FIG. 9 is a structural block diagram of a battery module design method for suppressing expansion of thermal runaway through discharge according to an embodiment of the present invention.
主要元件符号说明Description of main component symbols
三元锂离子动力电池 100Ternary lithium ion power battery 100
电池单体 10battery cell 10
正极柱 11Positive pole 11
负极柱 12Negative pole 12
金属连接片 20Metal connection piece 20
金属夹具 30metal clamp 30
隔热层 40Insulation 40
刺针 50Lancet 50
如下具体实施方式将结合上述附图进一步说明本发明。The following specific embodiments will further illustrate the present invention in conjunction with the above-mentioned drawings.
具体实施方式detailed description
以下将结合附图对本发明作进一步详细的说明。The present invention will be described in further detail below in conjunction with the accompanying drawings.
本发明实施例提供一种定量分析动力电池模块热失控扩展过程中传热量的方法,其包括以下步骤:An embodiment of the present invention provides a method for quantitatively analyzing heat transfer during thermal runaway expansion of a power battery module, which includes the following steps:
S1:在绝热环境下对一第一动力电池单体进行加热热失控实验,并记录所述第一动力电池单体在不同时刻的温度T(t);S1: Conduct a heating thermal runaway experiment on a first power battery cell in an adiabatic environment, and record the temperature T(t) of the first power battery cell at different times;
S2:建立所述第一动力电池单体在加热热失控实验过程中的一第一数学模型T(t)I,利用T(t)标定该第一数学模型T(t)I,所述第一数学模型T(t)I为所述第一动力电池单体在加热热失控条件下在某一时刻t的温度;S2: Establish a first mathematical model T(t) I of the first power battery cell during the heating thermal runaway experiment, use T(t) to calibrate the first mathematical model T(t) I , the first mathematical model T(t) I A mathematical model T(t) I is the temperature of the first power battery cell at a certain time t under heating thermal runaway conditions;
S3:提供一第二动力电池单体,该第二动力电池单体与所述第一动力电池单体相同,对所述第二动力电池单体进行热失控触发实验,并记录该第二动力电池单体在不同时刻的温度T′(t);S3: Provide a second power battery unit, the second power battery unit is the same as the first power battery unit, conduct a thermal runaway trigger test on the second power battery unit, and record the second power The temperature T'(t) of the battery cell at different times;
S4:建立所述第二动力电池单体在热失控触发实验过程中的一第二数学模型T(t)II,并利用T′(t)标定所述第二数学模型T(t)II,所述第二数学模型T(t)II为所述第二动力电池单体在热失控触发实验过程中在某一时刻t的温度;S4: Establish a second mathematical model T(t) II of the second power battery cell during the thermal runaway triggering experiment, and use T′(t) to calibrate the second mathematical model T(t) II , The second mathematical model T(t) II is the temperature of the second power battery cell at a certain moment t during the thermal runaway triggering experiment;
S5:对一第一动力电池模块进行加热热失控扩展实验,该第一动力电池模块包括至少两节电池单体,该电池单体与所述第一动力电池单体以及第二动力电池单体相同,且该第一动力电池模块中的热失控触发形式与所述第二动力电池单体的热失控触发形式相同,记录所述第一动力电池模块不同时刻的温度T″(t);S5: Conduct a heating thermal runaway expansion experiment on a first power battery module, the first power battery module includes at least two battery cells, the battery cells are connected to the first power battery cell and the second power battery cell The same, and the thermal runaway trigger form in the first power battery module is the same as the thermal runaway trigger form of the second power battery cell, record the temperature T"(t) of the first power battery module at different times;
S6:通过所述第一数学模型T(t)I以及所述第二数学模型T(t)II获得所述动力电池模块在加热热失控扩展实验过程中的一第三数学模型T(t)III,利用T″(t)标定该第三数学模型T(t)III,所述第三数学模型T(t)III为所述第一动力电池模块在加热热失控扩展实验过程中在某一时刻t的温度;S6: Obtain a third mathematical model T(t) of the power battery module during the heating thermal runaway expansion experiment process through the first mathematical model T(t) I and the second mathematical model T(t) II III , using T″(t) to calibrate the third mathematical model T(t) III , the third mathematical model T(t) III is the temperature of the first power battery module during a heating thermal runaway expansion experiment. temperature at time t;
S7:将所述第一动力电池模块中发生热失控触发的电池单体定义为首节触发电池,将首节触发电池之外的电池单体定义为次节扩展电池,减小第三数学模型T(t)III中每个次节扩展电池的电量,并通过第三数学模型T(t)III进行仿真计算,获得能够抑制所述第一动力电池模块热失控扩展的每个次节扩展电池的放电量;S7: Define the battery cell triggered by thermal runaway in the first power battery module as the first trigger battery, define the battery cells other than the first trigger battery as the second extended battery, and reduce the third mathematical model T (t) III , the power of each sub-section extended battery in the third mathematical model T(t) III is simulated to obtain the power of each sub-section extended battery that can suppress the thermal runaway expansion of the first power battery module Discharge capacity;
S8:选取一第二动力电池模块,该第二动力电池模块与所述第一动力模块相同,减小所述第二动力电池模块中次节扩展电池的电量后,对所述第二动力电池模块进行热失控扩展实验,该第二动力电池模块中的热失控触发形式与所述第一动力电池模块的热失控触发形式相同,利用所述第二动力电池模块热失控扩展实验的实验结果对所述每个次节扩展电池的放电量进行实验验证,确定能够抑制热失控扩展的每个次节扩展电池的放电量的设计参数,获得抑制动力电池模块热失控扩展的设计方法。S8: Select a second power battery module, the second power battery module is the same as the first power module, after reducing the power of the second extended battery in the second power battery module, power the second power battery Module conducts thermal runaway expansion experiment, the thermal runaway trigger form in the second power battery module is the same as the thermal runaway trigger form of the first power battery module, using the experimental results of the second power battery module thermal runaway expansion experiment The discharge capacity of each sub-section extended battery is verified experimentally, the design parameters of the discharge capacity of each sub-section extended battery capable of suppressing the expansion of thermal runaway are determined, and a design method for suppressing the expansion of thermal runaway of the power battery module is obtained.
步骤S1中,所述第一动力电池单体可以为一锂离子动力电池单体。在绝热环境下对所述第一动力电池单体进行热失控测试,有利于准确获得第一动力电池单体在热失控过程中释放和吸收的热量。本实施例中采用绝热加速量热仪对所述第一动力电池单体进行热失控测试,所述第一动力电池单体为一三元锂离子动力电池。In step S1, the first power battery unit may be a lithium-ion power battery unit. Performing a thermal runaway test on the first power battery unit in an adiabatic environment is conducive to accurately obtaining the heat released and absorbed by the first power battery unit during the thermal runaway process. In this embodiment, an adiabatic acceleration calorimeter is used to conduct a thermal runaway test on the first power battery unit, and the first power battery unit is a ternary lithium-ion power battery.
所述第一动力电池单体在加热热失控实验过程中的第一数学模型T(t)I可以利用化学反应动力学方程以及欧姆定律获得。The first mathematical model T(t) I of the first power battery unit during the heating thermal runaway experiment can be obtained by using the chemical reaction kinetic equation and Ohm's law.
对于所述第一动力电池单体,所述第一数学模型T(t)I的建立可以步骤包括以下步骤:For the first power battery unit, the establishment of the first mathematical model T(t) I may include the following steps:
S21:获得所述第一动力电池单体内部化学反应产生的生热功率的总和QI(t)的计算式;S21: Obtain the calculation formula of the sum Q I (t) of the heat generation power generated by the internal chemical reaction of the first power battery cell;
S22:根据QI(t)建立所述第一动力电池单体的的计算式;S22: Establish the first power battery cell according to Q I (t) calculation formula;
S23:根据建立所述第一动力电池单体的T(t)I的计算式。S23: According to A calculation formula for T(t) I of the first power battery unit is established.
步骤S21中,所述QI(t)的表达式为:In step S21, the expression of described Q I (t) is:
QI(t)=Qr(t)+Qe(t) (1)。Q1( t )=Qr(t)+ Qe ( t) (1).
其中,Qr(t)代表所述第一动力电池单体内部材料化学反应生热功率,Qe(t)代表第一动力电池单体内短路释放的电功率。Wherein, Q r (t) represents the heat generation power of the chemical reaction of the material inside the first power battery cell, and Q e (t) represents the electric power released by the short circuit in the first power battery cell.
所述Qr(t)的表达式为:The expression of said Q r (t) is:
Qr(t)=QSEI+Qanode+Qseparator+Qcathode+Qelectrolyte+QPVDF (2)。Q r (t) = Q SEI + Q anode + Q separator + Q cathode + Q electrolyte + Q PVDF (2).
其中,QSEI代表SEI膜分解反应的产热功率;Qanode代表负极与电解液反应的产热功率;Qseparator代表隔膜分解的吸热功率;Qcathode正极分解的产热功率;Qelectrolyte电解液分解的产热功率;QPVDF代表粘接剂分解反应的产热功率。所述QSEI、Qanode、Qseparator、Qcathode、Qelectrolyte以及QPVDF都可以用Arrhenius公式的形式来进行描述。例如QSEI的计算公式为:Among them, Q SEI represents the heat generation power of the SEI film decomposition reaction; Q anode represents the heat generation power of the reaction between the negative electrode and the electrolyte ; Q separator represents the heat absorption power of the diaphragm decomposition; Decomposition heat generation power; Q PVDF represents the heat generation power of the adhesive decomposition reaction. The Q SEI , Q anode , Q separator , Q cathode , Q electrolyte and Q PVDF can all be described in the form of Arrhenius formula. For example, the calculation formula of Q SEI is:
其中,HSEI代表SEI膜分解反应所能释放的总能量,单位是J,可以根据现有文献选取;cSEI(t)代表SEI膜的归一化的浓度,即反应开始时cSEI(0)=1,反应终止时,cSEI(∞)=0,cSEI(t)是在仿真过程中随着时间变化而变化的一个变量;ASEI代表SEI膜反应的频率因子,单位是s-1;Ea,SEI是化学反应的活化能,单位是J/mol,可以根据现有文献选取;R是理想气体常量,R=8.314J/(mol·K);Ti(t)是电池单体在时间为t的温度。可以理解,Qanode,Qseparator,Qcathode,Qelectrolyte及QPVDF的表达式通过将所述QSEI表达式的下标进行相应的修改得到。Among them, H SEI represents the total energy that can be released by the decomposition reaction of the SEI film, and the unit is J, which can be selected according to the existing literature; c SEI (t) represents the normalized concentration of the SEI film, that is, c SEI (0 )=1, when the reaction terminates, c SEI (∞)=0, c SEI (t) is a variable that changes with time during the simulation process; A SEI represents the frequency factor of the SEI membrane reaction, and the unit is s - 1 ; E a, SEI is the activation energy of chemical reaction, the unit is J/mol, can choose according to existing literature; R is ideal gas constant, R=8.314J/(mol K); T i (t) is battery The temperature of the monomer at time t. It can be understood that the expressions of Q anode , Q separator , Q cathode , Q electrolyte and Q PVDF are obtained by modifying the subscript of the Q SEI expression accordingly.
根据化学反应动力学方程以及能量守恒定律,所述第一动力电池单体Qe(t)的计算式为:According to the chemical reaction kinetic equation and the law of energy conservation, the calculation formula of the first power battery unit Q e (t) is:
对于所述第一动力电池单体,在t时刻电池内部温度Ti(t)小于等于第一动力电池单体内部隔膜的熔化温度Tonset时,该第一动力电池单体内部仅发生微短路,对应的反应产热功率为Qshort(t)。在Qshort(t)的表达式中,Ashort为微弱短路的速率因子,b为短路的指数项。在t时刻电池内部温度Ti(t)大于所述第一动力电池单体内部隔膜的熔化温度Tonset时,第一动力电池单体内部会发生大规模内短路,对应的产热功率为其中ΔH代表短路释放的总能量,Δt代表平均反应时间,其决定了反应的速度,代表已经发生的微弱短路的能量。For the first power battery cell, when the internal temperature T i (t) of the battery at time t is less than or equal to the melting temperature T onset of the internal diaphragm of the first power battery cell, only a micro-short circuit occurs inside the first power battery cell , and the corresponding reaction heat generation power is Q short (t). In the expression of Q short (t), A short is the rate factor of the weak short circuit, and b is the exponent term of the short circuit. When the internal temperature T i (t) of the battery at time t is greater than the melting temperature T onset of the internal diaphragm of the first power battery cell, a large-scale internal short circuit will occur inside the first power battery cell, and the corresponding heat generation power is Where ΔH represents the total energy released by the short circuit, Δt represents the average reaction time, which determines the speed of the reaction, Represents the energy of a weak short circuit that has occurred.
将所述Qr(t)和Qe(t)的计算式带入QI(t)=Qr(t)+Qe(t)即可得到QI(t)的计算式。The calculation formula of Q I (t) can be obtained by substituting the calculation formulas of Q r (t) and Q e (t) into Q I (t)=Q r (t)+Q e (t).
步骤S22中,根据能量守恒定律,所述第一动力电池单体在热失控过程中满足公式:In step S22, according to the law of energy conservation, the first power battery unit satisfies the formula during the thermal runaway process:
其中,M是第一动力电池单体的质量,单位是kg;Cp是第一动力电池单体的比热容,单位是J/(kg·K)。将QI(t)的计算式带入公式(5)即可得到的计算式。Wherein, M is the mass of the first power battery unit in kg; C p is the specific heat capacity of the first power battery unit in J/(kg·K). Bring the calculation formula of Q I (t) into the formula (5) to get calculation formula.
步骤S23中,所述第一动力电池单体在加热热失控条件下在某一时刻t的温度,即第一数学模型T(t)I满足公式:In step S23, the temperature of the first power battery cell at a certain moment t under the heating thermal runaway condition, that is, the first mathematical model T(t) I satisfies the formula:
T(0)I为一已知量。根据的计算式以及公式(6)即可得到第一数学模型T(t)I的计算式。T(0) I is a known quantity. according to The calculation formula and the formula (6) can get the calculation formula of the first mathematical model T(t) I .
所述利用T(t)标定所述第一数学模型T(t)I的步骤包括:对于Qr(t),根据现有文献选定一组ASEI和Ea,SEI,Aanode和Ea,anode,Aseparator和Ea,separator,Acathode和Ea,cathode,Aelectrolyte和Ea,electrolyte,以及Aa,PVDF和Ea,PVDF的值;对于Qe(t),根据实际经验选定一组Ashort,b,Δt和ΔH的值。利用所述第一数学模型T(t)I进行仿真计算得到所述第一动力电池单体在不同时刻的温度,如果通过所述仿真计算得到的温度与步骤S1中的实验结果T(t)相差较大,则在一定范围内调整ASEI和Ea,SEI,Aanode和Ea,anode,Aseparator和Ea,separator,Acathode和Ea,cathode,Aelectrolyte和Ea,electrolyte,Aa,PVDF和Ea,PVDF以及Ashort,b,Δt和ΔH的值,每调整一次采用所述第一数学模型T(t)I进行一次仿真计算,直到仿真计算结果与实验结果相近为止。The step of using T(t) to calibrate the first mathematical model T(t) I includes: for Qr( t ), selecting a set of A SEI and E a, SEI , A anode and E a according to existing literature a, anode , A separator and E a, separator , A cathode and E a, cathode , A electrolyte and E a, electrolyte , and the value of A a, PVDF and E a, PVDF ; for Q e (t), according to the actual A set of values for A short , b, Δt, and ΔH was selected empirically. Utilize described first mathematical model T (t) 1 to carry out simulation calculation and obtain the temperature of described first power battery cell at different moments, if the temperature obtained through described simulation calculation and the experimental result T (t) in step S1 If the difference is large, adjust A SEI and E a, SEI , A anode and E a, anode , A separator and E a, separator , A cathode and E a, cathode , A electrolyte and E a, electrolyte within a certain range, The values of A a, PVDF and E a, PVDF and A short , b, Δt and ΔH, each adjustment adopts the first mathematical model T(t) I to carry out a simulation calculation until the simulation calculation result is close to the experimental result .
本实施例中,标定后的ASEI和Ea,SEI,Aanode和Ea,anode,Aseparator和Ea,separator,Acathode和Ea,cathode,Aelectrolyte和Ea,electrolyte,Aa,PVDF和Ea,PVDF以及Ashort,b,Δt和ΔH的值请参见表1。由于本实施例中采用三元锂离子动力电池,三元材料的正极具有两个不同的化学反应,所以表1对应的优选数值中Acathode,,Ea,cathode,以及Hcathode的值有两组,分别为Acathode,1,Ea,cathode,1,Hcathode,1,Acathode,2,Ea,cathode,2,Hcathode,2。In this embodiment, the calibrated A SEI and E a, SEI , A anode and E a, anode , A separator and E a, separator , A cathode and E a, cathode , A electrolyte and E a, electrolyte , A a , PVDF and E a, see Table 1 for the values of PVDF and A short , b, Δt and ΔH. Since the ternary lithium ion power battery is used in this embodiment, the positive electrode of the ternary material has two different chemical reactions, so the values of A cathode , E a , cathode , and H cathode in Table 1 have two values. The groups are A cathode, 1 , E a, cathode, 1 , H cathode, 1 , A cathode, 2 , E a, cathode, 2 , H cathode, 2 .
表1Table 1
可以理解,对于所述第一动力电池单体,可以进一步包括对所述第一数学模型T(t)I进行合理简化。在进行第一数学模型T(t)I简化的过程中,应保证第一数学模型T(t)I仿真计算结果与实验结果相近,即保证第一数学模型T(t)I仿真计算的精度。由于在所述第一动力电池单体中,在t时刻电池内部温度Ti(t)小于等于第一动力电池单体内部隔膜的熔化温度Tonset时,该第一动力电池单体内部仅发生微短路,该微短路产生的能量较小,可以忽略不计。所以在加热热失控的第一数学模型T(t)I中,步骤S21可进一步包括将Qe(t)简化为:It can be understood that for the first power battery unit, reasonable simplification of the first mathematical model T(t) I may be further included. In the process of simplifying the first mathematical model T(t) I , it should be ensured that the simulation calculation results of the first mathematical model T(t) I are similar to the experimental results, that is, the accuracy of the simulation calculation of the first mathematical model T(t) I should be guaranteed . Since in the first power battery cell, when the battery internal temperature T i (t) at time t is less than or equal to the melting temperature T onset of the internal diaphragm of the first power battery cell, only the internal temperature of the first power battery cell Micro-short circuit, the energy generated by this micro-short circuit is small and can be ignored. So in the first mathematical model T(t) I of heating thermal runaway, step S21 may further include simplifying Qe (t) as:
请参阅图1,本实施例中,利用第一数学模型T(t)I,对所述第一动力电池单体进行仿真计算的结果与实验结果T(t)对比,具有较好的精度。Please refer to FIG. 1 , in this embodiment, using the first mathematical model T(t) I , the simulation calculation result of the first power battery unit is compared with the experimental result T(t), which has better accuracy.
步骤S3中,对于所述第二动力电池单体进行热失控触发实验,所述触发的形式不限,只要可以保证该热失控触发能够使所述第二动力电池单体释放出足够多的热量,从而使得相邻电池单体有足够的温度升高并发生热失控即可。优选的,所述热失控触发形式为针刺触发、过充触发或加热触发。当所述热失控触发形式采用针刺时,所述刺针直径优选为5~8mm,穿刺速度优选为10~30mm/s。本实施例中,通过针刺对所述第二动力电池单体进行热失控触发实验,刺针50的直径为8mm,穿刺速度为10mm/s。In step S3, a thermal runaway triggering experiment is performed on the second power battery unit, the form of the trigger is not limited, as long as it can be guaranteed that the thermal runaway trigger can cause the second power battery unit to release enough heat , so that the adjacent battery cells have enough temperature rise and thermal runaway occurs. Preferably, the triggering form of thermal runaway is acupuncture triggering, overcharging triggering or heating triggering. When acupuncture is used as the thermal runaway trigger, the diameter of the puncture needle is preferably 5-8 mm, and the puncture speed is preferably 10-30 mm/s. In this embodiment, a thermal runaway triggering experiment is performed on the second power battery unit by acupuncture, the diameter of the needle 50 is 8 mm, and the puncture speed is 10 mm/s.
步骤S4中,所述第二数学模型T(t)II的建立进一步包括以下步骤:In step S4, the establishment of the second mathematical model T (t) II further includes the following steps:
S41:建立所述第二动力电池单体在热失控触发过程中产热功率QII(t)的计算式;S41: Establish a calculation formula for the heat generation power Q II (t) of the second power battery unit during the thermal runaway triggering process;
S42:根据QII(t)得出的计算式;S42: According to Q II (t), it is obtained that calculation formula;
S43:根据得出T(t)II的计算式。S43: According to Get the calculation formula of T(t) II .
步骤S41中,所述QII(t)的计算公式为:In step S41, the calculation formula of said Q II (t) is:
QII(t)=Qr(t)+Qe_in(t)-Qh(t) (8)。Q II (t) = Q r (t) + Q e_in (t) - Q h (t) (8).
其中,Qr(t)为热触发实验时第二动力电池单体热化学反应释放的反应热功率;Qe_in(t)为内部短路被瞬间释放出来的热功率;Qh(t)为所述第二动力电池单体散热的功率。由于所述第二动力电池单体与所述第一动力电池单体完全相同,所以,公式(8)中Qr(t)的计算式与与所述第一动力电池单体的Qr(t)计算式相同,即公式(8)中Qr(t)可以根据步骤S21中公式(2)和(3)进行计算。本实施例中,对于所述第二动力电池单体,标定后的ASEI和Ea,SEI,Aanode和Ea,anode,Aseparator和Ea,separator,Acathode和Ea,cathode,Aelectrolyte和Ea,electrolyte,Aa,PVDF和Ea,PVDF以及Ashort,b,Δt和ΔH的值与所述第一动力电池单体中的相同,请参见表1。Among them, Q r (t) is the reaction heat power released by the thermochemical reaction of the second power battery unit during the thermal trigger experiment; Q e_in (t) is the heat power released instantaneously by the internal short circuit; Q h (t) is the Describe the heat dissipation power of the second power battery unit. Since the second power battery cell is exactly the same as the first power battery cell, the calculation formula of Q r (t) in formula (8) is the same as the Q r (t) of the first power battery cell The calculation formula of t) is the same, that is, Q r (t) in formula (8) can be calculated according to formulas (2) and (3) in step S21. In this embodiment, for the second power battery unit, A SEI and E a,SEI after calibration, A anode and E a,anode , A separator and E a,separator , A cathode and E a,cathode , The values of A electrolyte and E a, electrolyte , A a, PVDF and E a, PVDF and A short , b, Δt and ΔH are the same as those in the first power battery unit, please refer to Table 1.
根据化学反应动力学方程的变种形式得出,所述Qe_in(t)的计算公式为:Draw according to the variant form of chemical reaction kinetic equation, the calculation formula of described Q e_in (t) is:
其中,ΔH代表第二动力电池单体发生热失控触发的短路过程中,由于短路释放的电能总和,对于某一特定电池单体,ΔH为一已知量;∫Qe_in(t)dt代表在时间为t时已经释放了的电能;v代表反应速率呈指数形式。Among them, ΔH represents the sum of the electric energy released due to the short circuit during the short-circuit process triggered by the thermal runaway of the second power battery cell. For a specific battery cell, ΔH is a known quantity; ∫Q e_in (t)dt represents the The electrical energy that has been released at time t; v represents the reaction rate in exponential form.
所述Qh(t)的计算公式为:The calculation formula of said Q h (t) is:
Qh(t)=hII·AII·(T(t)II-Tamb(t)) (10)。Q h (t) = h II ·A II ·(T(t) II -T amb (t)) (10).
其中,hII代表第二动力电池单体对环境的换热系数,单位是W/(m2·K);AII代表第二动力电池单体的表面散热面积,单位是m2;T(t)II代表第二动力电池单体的仿真模型温度,单位是K;Tamb(t)代表周围环境的温度,单位是K。Among them, h II represents the heat transfer coefficient of the second power battery unit to the environment, the unit is W/(m 2 ·K); A II represents the surface heat dissipation area of the second power battery unit, the unit is m 2 ; T( t) II represents the temperature of the simulation model of the second power battery unit, the unit is K; T amb (t) represents the temperature of the surrounding environment, the unit is K.
步骤S42中,根据能量守恒定律,所述第二动力电池单体在热失控触发过程中满足公式:In step S42, according to the law of energy conservation, the second power battery unit satisfies the formula during the thermal runaway triggering process:
其中,M为所述第二动力电池单体的质量,单位是kg;Cp为所述第二动力电池单体的比热容,单位是J/(kg.K)。将QII(t)的计算式带入公式(11)即可得到的计算式。Wherein, M is the mass of the second power battery unit in kg; C p is the specific heat capacity of the second power battery unit in J/(kg.K). Bring the calculation formula of Q II (t) into the formula (11) to get calculation formula.
步骤S43中,所述第二动力电池单体在热失控触发条件下在某一时刻t的温度,即第二数学模型T(t)II满足公式:In step S43, the temperature of the second power battery cell at a certain moment t under the trigger condition of thermal runaway, that is, the second mathematical model T(t) II satisfies the formula:
T(0)II为所述第二动力电池单体热失控触发之前的温度,为一已知量。根据步骤S42中的计算式以及公式(12)即可得到第二数学模型T(t)II的计算式。T(0) II is the temperature before the thermal runaway of the second power battery unit is triggered, which is a known quantity. According to step S42 The calculation formula and the formula (12) can get the calculation formula of the second mathematical model T(t) II .
所述利用T′(t)标定所述第二数学模型T(t)II的步骤包括:根据经验值选定一组ΔH、v、hII,利用第二数学模型T(t)II进行仿真计算得到第二动力电池单体在不同时刻的温度,如果通过所述第二数学模型T(t)II仿真计算得到的温度与步骤S3中的实验结果T′(t)相差较大,则在一定范围内调整ΔH、v以及hII的值,每调整一次ΔH、v以及hII的值利用第二数学模型T(t)II进行一次仿真计算,直到仿真计算的结果与实验结果T′(t)相近为止。本实施例中,标定后的ΔH=385000J,v=0.001、hII=2W/(m2·K)。The step of using T'(t) to calibrate the second mathematical model T(t) II includes: selecting a group of ΔH, v, h II according to empirical values, and using the second mathematical model T(t) II to simulate Calculate the temperature of the second power battery cell at different times, if the temperature calculated by the simulation of the second mathematical model T(t) II differs greatly from the experimental result T'(t) in step S3, then in Adjust the values of ΔH, v, and h II within a certain range, and use the second mathematical model T(t) II to perform a simulation calculation every time the value of ΔH, v, and h II is adjusted, until the result of the simulation calculation is consistent with the experimental result T′( t) until close. In this embodiment, after calibration, ΔH=385000J, v=0.001, h II =2W/(m 2 ·K).
请参阅图2,由图中可以看出,第二动力电池单体通过第二数学模型T(t)II计算的结果与实验结果T′(t)相比,具有较好的精度。Please refer to FIG. 2 , it can be seen from the figure that the calculation result of the second power battery unit through the second mathematical model T(t) II has better accuracy than the experimental result T′(t).
可以理解,可以进一步包括对所述第二数学模型T(t)II进行合理简化。由于在所述第二数学模型T(t)II中,包括一些在热失控扩展模型计算中影响较小的次要因素。对于这些影响较小的次要因素进行近似或加以忽略,从而可以提高热失控扩展模型的仿真计算速度。在进行第二数学模型T(t)II简化的过程中,应保证第二数学模型T(t)II仿真计算结果与实验结果相近,即保证第二数学模型T(t)II仿真计算的精度。由于所述Qe_in(t)的计算式中存在指数形式,计算速度较慢,所以,在保证仿真计算精度的情况下,可以将方程:简化成线性方程:It can be understood that reasonable simplification of the second mathematical model T(t) II may be further included. Because the second mathematical model T(t) II includes some secondary factors that have less influence in the calculation of the thermal runaway expansion model. Approximating or ignoring these less influential secondary factors can improve the simulation calculation speed of the thermal runaway extended model. In the process of simplifying the second mathematical model T (t) II , it should be ensured that the simulation calculation results of the second mathematical model T (t) II are similar to the experimental results, that is, the accuracy of the simulation calculation of the second mathematical model T (t) II should be guaranteed . Since there is an exponential form in the calculation formula of said Q e_in (t), the calculation speed is relatively slow, so, under the condition of ensuring the simulation calculation accuracy, the equation can be: Simplifies to a linear equation:
步骤S6中,所述第一动力电池模块中的至少两节电池单体可以以串联的方式或并联的方式连接。请参阅图3,本实施例中,所述第一动力电池模块是一方壳的25Ah的三元锂离子动力电池100,所述三元锂离子动力电池100包括六节电池单体10、多个金属连接片20、多个金属夹具30以及多个隔热层40。每个电池单体10包括一个正极柱11以及一个负极柱12。所述金属连接片20用于将六节电池单体10串联在一起;所述金属夹具30用于夹持所述电池单体10;所述隔热层40用于隔离所述电池单体10与金属夹具30。In step S6, at least two battery cells in the first power battery module may be connected in series or in parallel. Please refer to FIG. 3 , in this embodiment, the first power battery module is a 25Ah ternary lithium-ion power battery 100 with a shell, and the ternary lithium-ion power battery 100 includes six battery cells 10, a plurality of The metal connection piece 20 , a plurality of metal clamps 30 and a plurality of heat insulation layers 40 . Each battery cell 10 includes a positive pole 11 and a negative pole 12 . The metal connecting piece 20 is used to connect six battery cells 10 in series; the metal clamp 30 is used to clamp the battery cells 10 ; the heat insulating layer 40 is used to isolate the battery cells 10 with 30 metal clamps.
采用集总参数法,将各节电池单体,各节电池单体的极柱均视为具有单一质量,单一热容和单一温度的节点。各个节点具有其自身的质量Mi,热容Cpi以及温度Ti。Using the lumped parameter method, each battery cell and the pole of each battery cell are regarded as nodes with a single mass, a single heat capacity and a single temperature. Each node has its own mass M i , heat capacity C pi and temperature T i .
将所述第一动力电池模块中进行热失控触发实验的电池单体定义为首节触发电池,将所述第一动力电池模块中首节触发电池之外的其它电池单体定义为次节扩展电池。所述第三数学模型Ti(t)III的获得可以进一步包括以下步骤:Define the battery cell that is subjected to the thermal runaway triggering experiment in the first power battery module as the first trigger battery, and define the battery cells other than the first trigger battery in the first power battery module as the second extended battery . The obtaining of the third mathematical model T i (t) III may further include the following steps:
S61:分别建立首节触发电池、次节扩展电池、电池极柱以及夹具在加热热失控扩展条件下的能量变化率Qi计算式;S61: respectively establish the energy change rate Q i calculation formulas of the trigger battery of the first section, the extended battery of the second section, the battery pole, and the fixture under the condition of heating thermal runaway expansion;
S62:根据Qi分别建立首节触发电池、次节扩展电池、电池极柱以及夹具在加热热失控扩展条件下的的计算式;S62: According to Q i , respectively establish the conditions of the first trigger battery, the second extended battery, the battery pole and the fixture under the condition of heating thermal runaway expansion calculation formula;
S63:根据分别建立首节触发电池、次节扩展电池、电池极柱以及夹具在加热热失控扩展条件下的Ti(t)III的计算式。S63: According to The calculation formulas of T i (t) III of the first trigger battery, the second extended battery, the battery pole and the fixture under the condition of heating thermal runaway expansion are respectively established.
步骤S61中,根据能量守恒定律,在加热热失控扩展条件下,首节触发电池、次节扩展电池、电池极柱以及夹具的能量变化率Qi的计算式均可以表示为:In step S61, according to the law of energy conservation, under the condition of heating thermal runaway expansion, the calculation formula of the energy change rate Q i of the first trigger battery, the second extension battery, the battery pole and the fixture can be expressed as:
Qi(t)=Qsheng(t)-Qsan(t) (14)。Q i (t) = Q sheng (t) - Q san (t) (14).
其中,Qsan(t)表示散热功率;Qsheng(t)代表生热功率。对于首节触发电池Qsheng(t)=QI(t)=Qr(t)+Qe_in(t),-Qsan(t)=-∑Qij(t)-Qih(t);对于次节扩展电池,Qsheng(t)=QII(t)=Qr(t)+Qe(t),-Qsan(t)=-∑Qij(t)-Qih(t);由于极柱和夹具均是纯金属材料,不会发生化学反应,所以对于极柱和夹具,Qsheng(t)=0,-Qsan(t)=-∑Qij(t)-Qih(t)。其中,Qij代表节点i向节点j进行传热的散热功率;Qih(t)代表节点i向周围环境进行散热的散热功率。Among them, Q san (t) represents heat dissipation power; Q sheng (t) represents heat generation power. For the first trigger cell Q sheng (t)=Q I (t)=Q r (t)+Q e_in (t), -Q san (t)=-∑Q ij (t)-Q ih (t); For the sub-section extended battery, Q sheng (t)=Q II (t)=Q r (t)+Q e (t), -Q san (t)=-∑Q ij (t)-Q ih (t) ; Since poles and fixtures are pure metal materials, no chemical reaction will occur, so for poles and fixtures, Q sheng (t)=0, -Q san (t)=-∑Q ij (t)-Q ih (t). Among them, Q ij represents the heat dissipation power from node i to node j; Q ih (t) represents the heat dissipation power from node i to the surrounding environment.
对于所述动力电池模块,Qi的计算式具体为:For the power battery module, the calculation formula of Q i is specifically:
采用热阻法建立各节点之间的传热模型,根据傅里叶导热公式,节点i向节点j进行传热的散热功率Qij的计算式为:The thermal resistance method is used to establish the heat transfer model between nodes. According to the Fourier heat conduction formula, the calculation formula of the heat dissipation power Q ij for heat transfer from node i to node j is:
Qij(t)=Aij·(Ti(t)III-Tj(t)III)/Rij (16)。Q ij (t)=A ij ·(T i (t) III -T j (t) III )/R ij (16).
其中,Aij(t)代表节点i与节点j之间的有效传热面积,单位是m2;Rij(t)代表节点i与节点j之间传热的热阻,单位是(m2·K)/W;Ti(t)III代表t时刻节点i的温度,Tj(t)III代表t时刻节点j的温度。Among them, A ij (t) represents the effective heat transfer area between node i and node j, the unit is m 2 ; R ij (t) represents the thermal resistance of heat transfer between node i and node j, the unit is (m 2 ·K)/W; T i (t) III represents the temperature of node i at time t, and T j (t) III represents the temperature of node j at time t.
根据傅里叶导热公式,节点i向周围环境进行散热的散热功率Qih(t)的计算式为:According to the Fourier heat conduction formula, the calculation formula of the heat dissipation power Q ih (t) for node i to dissipate heat to the surrounding environment is:
Qih(t)=Aih·(Ti(t)III-Th(t))/Rih (17)Q ih (t)=A ih ·(T i (t) III -T h (t))/R ih (17)
其中,所述Aih(t)代表节点i对环境散热的等效面积,单位是m2;Rih(t)对环境散热的等效热阻,单位是(m2·K)/W;Ti(t)IIIt时刻节点i的温度,Th(t)代表t时刻环境温度。Wherein, the A ih (t) represents the equivalent area of the node i for heat dissipation to the environment, and the unit is m 2 ; the equivalent thermal resistance of R ih (t) to the heat dissipation of the environment, the unit is (m 2 ·K)/W; T i (t) III is the temperature of node i at time t, and T h (t) represents the ambient temperature at time t.
公式(15)中,所述次节扩展电池的短路能量Qe(t)的表达式为:In the formula (15), the expression of the short-circuit energy Q e (t) of the extended battery in the second section is:
其中,是通过插值计算得出的温度,该满足公式:in, is the temperature calculated by interpolation, the Satisfies the formula:
其中,α是计算过程中的权重因子,0<α<0.5。优选地,α=0.23;Ti-1(t)为第i-1节电池单体的模型计算温度,Ti(t)为第i节电池单体的模型计算温度,i=2,3,4,5或6。Among them, α is the weight factor in the calculation process, 0<α<0.5. Preferably, α=0.23; T i-1 (t) is the model calculation temperature of the i-1th battery cell, T i (t) is the model calculation temperature of the i-th battery cell, i=2,3 , 4, 5 or 6.
步骤S62中,根据能量守恒定律:In step S62, according to the law of conservation of energy:
可以分别得到所述首节触发电池、次节扩展电池以及电池极柱和夹具在加热热失控扩展条件下的计算式。It can be obtained respectively that the triggering battery of the first section, the extended battery of the second section, and the battery pole and the fixture are heated under the condition of thermal runaway expansion. calculation formula.
步骤S63中,在加热热失控扩展条件下,所述首节触发电池、次节扩展电池以及电池极柱和夹具的Ti(t)III满足公式:In step S63, under the condition of heating thermal runaway expansion, T i (t) III of the trigger battery of the first section, the extended battery of the second section, and the battery pole and the clamp satisfy the formula:
其中,T(0)III为一已知量。将带入公式(21)即可分别得到首节触发电池、次节扩展电池以及电池极柱和夹具在加热热失控扩展条件下的第三数学模型T(t)III。Wherein, T(0) III is a known quantity. Will Introducing formula (21) to obtain the third mathematical model T(t) III of the trigger battery of the first section, the extended battery of the second section, and the battery pole and fixture under the condition of heating thermal runaway expansion.
所述利用T″(t)对所述第三数学模型T(t)III进行标定可以包括:根据现有文献选定一组Rij与Aij的值,利用所述第三数学模型T(t)III进行仿真计算得到动力电池模块各节点在不同时刻的温度,如果与步骤S5中的实验结果T″(t)相差较大,则在一定范围内调整Rij与Aij的值,每调整一次采用所述第三数学模型T(t)III进行一次仿真计算,直到仿真计算结果与实验结果相近为止。The use of T"(t) to calibrate the third mathematical model T(t) III may include: selecting a set of values of R ij and A ij according to existing literature, using the third mathematical model T( t) III performs simulation calculation to obtain the temperature of each node of the power battery module at different times, if it is quite different from the experimental result T″(t) in step S5, then adjust the values of R ij and A ij within a certain range, every Adjust once and use the third mathematical model T(t) III to perform a simulation calculation until the simulation calculation result is close to the experimental result.
将所述第一动力电池模块中的首节触发电池定义为第一节电池单体,与第一节电池单体相邻的电池单体为第二节电池单体,与第二节电池单体相邻的电池单体为第三节电池单体,以此类推。本实施例中,标定后的Rij与Aii的值的一组优选结果请参阅表2。The first trigger battery in the first power battery module is defined as the first battery cell, the battery cell adjacent to the first battery cell is the second battery cell, and the battery cell adjacent to the second battery cell is The adjacent battery cell is the third battery cell, and so on. In this embodiment, please refer to Table 2 for a set of preferred results of the calibrated values of R ij and A ii .
表2Table 2
请参阅图4-5,由图中可以看出,本实施例利用第三数学模型计算得到的首节触发电池及其正、负电极柱以及次节扩展电池及其正、负电极柱在热失控扩展过程中在不同时刻的温度与实验结果相比误差较小,说明所述第三数学模型T(t)III具有较好的精度。从图5中还可以看出,第一节电池单体与第二节电池单体发生热失控的时间差约为480s,第二节电池单体在发生热失控之前的内核温度达到了110℃。Please refer to Figure 4-5, it can be seen from the figure that the first trigger battery and its positive and negative electrode columns and the second extended battery and its positive and negative electrode columns calculated by the third mathematical model in this embodiment are heated Compared with the experimental results, the temperature at different times during the runaway expansion process has smaller errors, which shows that the third mathematical model T(t) III has better precision. It can also be seen from Figure 5 that the time difference between the thermal runaway of the first battery cell and the second battery cell is about 480s, and the core temperature of the second battery cell reaches 110°C before thermal runaway occurs.
步骤S7中,减小第三数学模型中的次节扩展电池的电量后,在热失控扩展过程中,次节扩展电池的瞬时电功率释放值Qe满足式:In step S7, after reducing the power of the secondary extended battery in the third mathematical model, the instantaneous electric power release value Q e of the secondary extended battery satisfies the formula:
可以理解,公式(22)可以进一步简化为:It can be understood that formula (22) can be further simplified as:
其中,Tonset代表次节扩展电池内部隔膜的熔化温度,即热失控温度;ΔH代表短路释放的总电能;代表已经发生的微弱短路的能量;Δt代表温度达到热失控温度点时,大规模内短路的持续时间;KSOC代表放电后次节扩展电池的电量总和占次节扩展电池的初始电量总和的百分比。Among them, Tonset represents the melting temperature of the internal diaphragm of the extended battery in the second section, that is, the thermal runaway temperature; ΔH represents the total electric energy released by the short circuit; Represents the energy of the weak short circuit that has occurred; Δt represents the duration of the large-scale internal short circuit when the temperature reaches the thermal runaway temperature point; K SOC represents the percentage of the total power of the secondary extended battery after discharge to the initial total power of the secondary extended battery .
整个热失控扩展过程中,所有次节扩展电池单体电能释放量的总和ΔH应满足式:During the entire thermal runaway expansion process, the sum ΔH of the electric energy release of all sub-section extended battery cells should satisfy the formula:
ΔH=∫Qedt.......(24)ΔH=∫Q e dt......(24)
在进行仿真计算过程中,对于首节触发电池,KSOC等于100%;对于每个次节扩展电池,KSOC均小于100%,且每个次节扩展电池的KSOC均相等。本实施例中,对于第二节电池单体到第六节电池单体,设置了几组不同的KSOC进行仿真计算,其中,每一组数据中第二节电池单体到第六节电池单体的KSOC均相等。具体请参见表3:In the process of simulation calculation, for the triggering battery of the first section, K SOC is equal to 100%; for each extended battery of the second section, K SOC is less than 100%, and the K SOC of each extended battery of the second section is equal. In this embodiment, for the second battery cell to the sixth battery cell, several sets of different K SOCs are set for simulation calculation, wherein, in each set of data, the second battery cell to the sixth battery cell The K SOC of the monomers are all equal. Please refer to Table 3 for details:
表3table 3
请参阅图6,从图中可以看出,在仿真计算中,当KSOC在50%~100%之间时,第二节电池单体均会发生热失控。当KSOC在80%~100%时,第三节电池单体会发生热失控的扩展,而当第二节电池单体的KSOC在75%及以下时,第三节电池单体不会发生热失控的扩展;说明所述次节扩展电池放电量的设计参数即次节扩展电池的电量的边界值KSOC-B≈75%。在仿真计算时,当第二节电池单体到第六节电池单体的电量低于边界值KSOC-B时,动力电池模块内部的热失控扩展能够得到有效的抑制。Please refer to FIG. 6 . It can be seen from the figure that in the simulation calculation, when the K SOC is between 50% and 100%, thermal runaway will occur in the second battery cell. When the K SOC is 80% to 100%, thermal runaway expansion will occur in the third battery cell, and when the K SOC of the second battery cell is 75% or below, the third battery cell will not Expansion of thermal runaway occurs; indicating that the design parameter of the discharge capacity of the secondary extended battery is the boundary value K SOC-B ≈75% of the electric quantity of the secondary extended battery. In the simulation calculation, when the power of the second battery cell to the sixth battery cell is lower than the boundary value K SOC-B , the expansion of thermal runaway inside the power battery module can be effectively suppressed.
步骤S8中,对于所述每个次节扩展电池的放电量进行实验验证。具体地,选取一第二动力电池模块,该第二动力电池模块与所述第一动力模块相同,在仿真计算中得到的次节扩展电池的电量边界值KSOC-B的附近选取多组实验参数,将所述第二动力电池模块中次节扩展电池的电量按照KSOC-B进行放电,对所述第二动力电池模块进行热失控扩展实验,该第二动力电池模块中的热失控触发形式与所述第一动力电池模块的热失控触发形式相同,利用所述第二动力电池模块热失控扩展实验的实验结果对于所述每个次节扩展电池的放电量进行实验验证,通过实验验证获得实际情况下次节扩展电池的边界值KSOC-B。In step S8, experimental verification is performed on the discharge capacity of each sub-section extended battery. Specifically, select a second power battery module, the second power battery module is the same as the first power module, and select multiple sets of experiments near the power boundary value K SOC-B of the sub-section extended battery obtained in the simulation calculation Parameters, discharge the power of the second extension battery in the second power battery module according to K SOC-B , conduct a thermal runaway expansion experiment on the second power battery module, and the thermal runaway in the second power battery module triggers The form is the same as that of the thermal runaway triggering form of the first power battery module, and the experimental results of the thermal runaway expansion experiment of the second power battery module are used to verify the discharge capacity of each sub-section extended battery, and the experimental verification is carried out Obtain the boundary value K SOC-B of the next extended battery in the actual situation.
本实施例中,分别选取KSOC为75%、50%进行了实验。具体设计情况如表4:In this embodiment, experiments were carried out by selecting K SOC as 75% and 50% respectively. The specific design situation is shown in Table 4:
表4Table 4
请参阅图7,从图中可以看出,当次节扩展电池的KSOC=75%时,第一节电池单体与第二节电池单体发生热失控的时间差约为680s,与图5中次节扩展电池未放电时第一节电池单体与第二节电池单体发生热失控的时间差约为480s相比,第二节电池单体热失控的延时增大。这种延时的增大使得实验中第二节电池单体在热失控发生之前的内核温度达到了220℃,远高于图5中的110℃。从图中还可以看出,第二节电池单体发生热失控时,最高温度达到了928℃,并导致了第三节电池单体到第六节电池单体的依次热失控。这可能是因为本实施例中的动力电池模块在荷电状态为75%附近时,热稳定性变化较为剧烈。图7的结果表明,尽管仿真计算中的KSOC-B=75%,但在实际过程中,KSOC-B应当小于75%。Please refer to Figure 7. It can be seen from the figure that when the K SOC of the extended battery in the second section is 75%, the time difference between the thermal runaway of the first battery cell and the second battery cell is about 680s, which is the same as that in Figure 5 Compared with the time difference between the thermal runaway of the first battery cell and the second battery cell when the secondary extended battery is not discharged, which is about 480s, the delay of the thermal runaway of the second battery cell is longer. This increase in time delay caused the core temperature of the second battery cell to reach 220°C before thermal runaway occurred in the experiment, much higher than the 110°C in Figure 5. It can also be seen from the figure that when the thermal runaway of the second battery cell occurs, the maximum temperature reaches 928°C, which leads to the sequential thermal runaway of the third battery cell to the sixth battery cell. This may be because the thermal stability of the power battery module in this embodiment changes drastically when the state of charge is around 75%. The result of Fig. 7 shows that although K SOC-B = 75% in the simulation calculation, in the actual process, K SOC-B should be less than 75%.
请参阅图8,从图中可以看出,当次节扩展电池的KSOC=50%时,在第一节电池单体受到针刺触发之后,第二节电池单体的温度缓慢上升,最高温度达到263℃。第二节电池单体到第六节电池单体均没有发生热失控。可以理解,第二节电池单体没有发生热失控与本实施例中的动力电池模块在50%的荷电状态下,热失控温度点Tonset升高有一定的关系。图8的实验结果表明,在实际过程中,KSOC-B大于50%。Please refer to Fig. 8. It can be seen from the figure that when the K SOC of the extended battery in the second section is 50%, after the first battery cell is triggered by acupuncture, the temperature of the second battery cell rises slowly, and the maximum The temperature reached 263°C. No thermal runaway occurred in the second battery cell to the sixth battery cell. It can be understood that the lack of thermal runaway of the second battery cell has a certain relationship with the rise of the thermal runaway temperature point T onset of the power battery module in this embodiment when the state of charge is 50%. The experimental results in Fig. 8 show that in the actual process, K SOC-B is greater than 50%.
通过实验验证可以得出,本实施例中,次节扩展电池单体的放电量有一个边界值KSOC-B,50%<KSOC-B<75%。Through experimental verification, it can be concluded that in this embodiment, the discharge capacity of the sub-section extended battery cell has a boundary value K SOC-B , 50%<K SOC-B <75%.
根据所述实验验证结果,确定能够抑制热失控扩展的电池单体放电量的设计参数。具体地,当第一节电池单体发生热失控之后,在热失控向第二节电池单体扩展的时间限制之内,将动力电池模块中第二节到第六节电池单体尽快放电到电量小于等于KSOC-B。本实施例中,当KSOC=100%时,第一节电池单体与第二节电池单体的热失控间隔为481s,第二节电池单体与第三节电池单体的热失控间隔为161s,第三节电池单体与第四节电池单体的热失控间隔为156s,第四节电池单体与第五节电池单体的热失控间隔为157s,第五节电池单体与第六节电池单体的热失控间隔为137s。可以选取相邻电池单体之间热失控扩展的平均时间间隔为137s到161s中的任何一个值,本实施例中选取相邻电池单体之间热失控扩展的平均时间间隔为160s。为抑制热失控扩展,应在160s内,尽快将相邻电池单体的电量放到初始电量的50%或50%以下。根据公式:放电电流I=(Ce×3600×KSOC)/(nΔt),可以得到第二节电池单体到第六节电池单体不继续发生热失控扩展的最小放电电流。其中,Ce代表动力电池模块中首节触发电池的初始电量,单位为AH;Δt代表相邻电池单体之间热失控扩展的平均时间间隔,单位为s;n代表平均时间间隔个数。本实施例中,Ce=25AH;Δt=160s;对于第二节电池单体,n=1;对于第三节电池单体,n=2;对于第四节电池单体,n=3;第五节电池单体,n=4;对于第六节电池单体,n=5,KSOC小于50%,通过计算可以得出,第二节电池单体到第六节电池单体不继续发生热失控扩展的最小放电电流分别为I2=281A;I3=141A。I4=94A;I5=70A;I6=56A。According to the experimental verification results, the design parameters of the discharge capacity of the battery cells capable of suppressing the expansion of thermal runaway are determined. Specifically, after the thermal runaway of the first battery cell occurs, within the time limit for the thermal runaway to extend to the second battery cell, the second to sixth battery cells in the power battery module are discharged as soon as possible to The power is less than or equal to K SOC-B . In this embodiment, when K SOC =100%, the thermal runaway interval between the first battery cell and the second battery cell is 481s, and the thermal runaway interval between the second battery cell and the third battery cell is 481s. The thermal runaway interval between the third battery cell and the fourth battery cell is 156s, the thermal runaway interval between the fourth battery cell and the fifth battery cell is 157s, and the fifth battery cell and The thermal runaway interval of the sixth battery cell is 137s. The average time interval of thermal runaway expansion between adjacent battery cells can be selected as any value from 137s to 161s. In this embodiment, the average time interval of thermal runaway expansion between adjacent battery cells is selected as 160s. In order to suppress the expansion of thermal runaway, the power of adjacent battery cells should be reduced to 50% or less than 50% of the initial power as soon as possible within 160s. According to the formula: discharge current I=(C e ×3600×K SOC )/(nΔt), the minimum discharge current at which the second battery cell to the sixth battery cell does not continue to expand thermal runaway can be obtained. Among them, C e represents the initial power of the first trigger battery in the power battery module, in AH; Δt represents the average time interval of thermal runaway expansion between adjacent battery cells, in s; n represents the number of average time intervals. In this embodiment, C e =25AH; Δt=160s; for the second battery cell, n=1; for the third battery cell, n=2; for the fourth battery cell, n=3; The fifth battery cell, n=4; for the sixth battery cell, n=5, K SOC is less than 50%, it can be obtained through calculation that the second battery cell to the sixth battery cell do not continue The minimum discharge currents for thermal runaway expansion are I 2 =281A; I 3 =141A. I 4 =94A; I 5 =70A; I 6 =56A.
请看附图9,本实施例中,提供一种抑制热失控扩展的电池模块设计方法示意图。三元锂离子动力电池除了需要对于功率器件60进行供电之外,为了抑制可能发生的热失控扩展,三元锂离子动力电池的各节电池单体都通过电路与安全性放电器件相连。为了不让第3节相邻的电池发生热失控的扩展,则安全性放电器件应能够使得任意一节电池能够以141A的电流快速放电至50%的荷电状态。Please refer to FIG. 9 . In this embodiment, a schematic diagram of a battery module design method for suppressing expansion of thermal runaway is provided. In addition to powering the power device 60 , the ternary lithium-ion power battery needs to supply power to the power device 60 . In order to suppress possible expansion of thermal runaway, each cell of the ternary lithium-ion power battery is connected to a safety discharge device through a circuit. In order to prevent thermal runaway expansion of the third adjacent battery, the safety discharge device should enable any battery to be quickly discharged to 50% state of charge at a current of 141A.
另外,本领域技术人员还可以在本发明精神内做其他变化,这些依据本发明精神所做的变化,都应包含在本发明所要求保护的范围内。In addition, those skilled in the art can also make other changes within the spirit of the present invention, and these changes made according to the spirit of the present invention should be included in the scope of protection claimed by the present invention.
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| CN108445039B (en) * | 2018-02-07 | 2021-05-04 | 清华大学 | Power battery thermal runaway safety performance prediction method and device and computer readable storage medium |
| CN108446434B (en) * | 2018-02-07 | 2020-02-11 | 清华大学 | Prediction method and device for thermal runaway safety of power battery and computer readable storage medium |
| CN111913120B (en) * | 2020-07-16 | 2022-07-22 | 中国汽车技术研究中心有限公司 | Method and device for testing influence of parallel battery pack electric connection on thermal diffusion |
| CN112018459B (en) * | 2020-07-17 | 2021-09-14 | 清华大学 | Battery system thermal failure diffusion inhibition structure and determination method thereof, and battery system |
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| CN113671384B (en) * | 2021-08-20 | 2023-06-16 | 华北电力大学(保定) | Battery temperature prediction method and system |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7820319B2 (en) * | 2009-07-17 | 2010-10-26 | Tesla Motors, Inc. | Cell thermal runaway propagation resistant battery pack |
| CN102222940A (en) * | 2010-04-13 | 2011-10-19 | 江苏高和机电制造有限公司 | Cell management system of electric automobile |
| CN102496747A (en) * | 2011-11-18 | 2012-06-13 | 中国检验检疫科学研究院 | Thermal management device for power batteries and thermal management method for power batteries |
| US8415043B2 (en) * | 2008-12-30 | 2013-04-09 | Gateway, Inc. | System for reducing thermal transfer between cells in a battery |
-
2014
- 2014-05-29 CN CN201410232531.3A patent/CN104008293B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8415043B2 (en) * | 2008-12-30 | 2013-04-09 | Gateway, Inc. | System for reducing thermal transfer between cells in a battery |
| US7820319B2 (en) * | 2009-07-17 | 2010-10-26 | Tesla Motors, Inc. | Cell thermal runaway propagation resistant battery pack |
| CN102222940A (en) * | 2010-04-13 | 2011-10-19 | 江苏高和机电制造有限公司 | Cell management system of electric automobile |
| CN102496747A (en) * | 2011-11-18 | 2012-06-13 | 中国检验检疫科学研究院 | Thermal management device for power batteries and thermal management method for power batteries |
Non-Patent Citations (1)
| Title |
|---|
| 锂离子电池各向异性导热的实验与建模;冯旭宁 等;《汽车安全与节能学报》;20121231;第3卷(第2期);第158-164页 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12176745B2 (en) | 2019-11-13 | 2024-12-24 | Lg Energy Solution, Ltd. | Forced discharge test apparatus and forced discharge test method |
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