基于铅酸电池试验的Peukert方程(Peukert equation,PE)提供一个修正电流倍率影响的经验模型。但该模型的试验及应用中,存在混淆电荷损失及剩余电荷量的问题。采用二阶段放电试验方法来建立修正的Peukert模型,即对于每种倍率分别进行两...基于铅酸电池试验的Peukert方程(Peukert equation,PE)提供一个修正电流倍率影响的经验模型。但该模型的试验及应用中,存在混淆电荷损失及剩余电荷量的问题。采用二阶段放电试验方法来建立修正的Peukert模型,即对于每种倍率分别进行两个阶段的恒流放电:特定倍率放电到截至电压—静置—标准倍率放电到截至电压(CC-OC-CC)。依据两个阶段放电的总电荷量(最大可用电荷量)而非第一阶段的电荷量(可用电荷量)去建立修正的Peukert方程(PE3)。该方程(PE3)反映了倍率与电荷损耗(库仑效率)之间的关系,排除了剩余电荷量的影响,更适合于动态工况下的荷电状态(State of charge,SOC)估计。另外磷酸铁锂电池试验表明剩余电荷量与电流倍率的关系规律性更强,更符合Peukert形式的方程(PE2),与铅酸电池Peukert模型的扩散机理一致,故剩余电荷量也可据此估计。展开更多
以纳米Li Fe PO4锂离子电池为研究对象,在50--450 A和-18~50℃范围内,对其充放电特性、Peukert模型与温度的关系进行了讨论,利用Ragone曲线对阀控式密封铅酸动力电池、镍氢动力电池及锰酸锂离子电池的能量功率特性进行了对比分析。研究...以纳米Li Fe PO4锂离子电池为研究对象,在50--450 A和-18~50℃范围内,对其充放电特性、Peukert模型与温度的关系进行了讨论,利用Ragone曲线对阀控式密封铅酸动力电池、镍氢动力电池及锰酸锂离子电池的能量功率特性进行了对比分析。研究表明,该纳米Li Fe PO4锂离子电池的快速放电能力和能量功率特性都得到很大改善,尤其适合于高温工况;低温性能依然还是纳米Li Fe PO4锂离子电池的弱点,亟待进一步提高。展开更多
To overcome the problems encountered in predicting the endurance of electricpowered fixed-wing unmanned aerial vehicles(UAVs),which were stemmed from the dynamic changes in electric power system efficiency and battery...To overcome the problems encountered in predicting the endurance of electricpowered fixed-wing unmanned aerial vehicles(UAVs),which were stemmed from the dynamic changes in electric power system efficiency and battery discharge characteristics under different operating conditions,the required battery power model and battery discharge model were studied.The required battery power model was determined using an approximate model of electric power system efficiency based on wind tunnel testing and the self-adaptive penalty function.Furthermore,current correction and ambient temperature correction terms were proposed for the trained Kriging model representing the discharge characteristics under standard operation,and then the discharged capacity-terminal voltage model was established.Through numerical integration of this model with the required battery power model,the electric-powered fixed-wing UAV endurance prediction model was obtained.Laboratory tests indicated that the proposed endurance model could precisely calculate the battery discharge time and accurately describe the battery discharge process.The similarity of the theoretical and flight test results reflected the accuracy of the proposed endurance model as well as the importance of considering dynamic changes in power system efficiency in endurance calculations.The proposed endurance model meeting precision requirements can be used in practical engineering applications.展开更多
文摘基于铅酸电池试验的Peukert方程(Peukert equation,PE)提供一个修正电流倍率影响的经验模型。但该模型的试验及应用中,存在混淆电荷损失及剩余电荷量的问题。采用二阶段放电试验方法来建立修正的Peukert模型,即对于每种倍率分别进行两个阶段的恒流放电:特定倍率放电到截至电压—静置—标准倍率放电到截至电压(CC-OC-CC)。依据两个阶段放电的总电荷量(最大可用电荷量)而非第一阶段的电荷量(可用电荷量)去建立修正的Peukert方程(PE3)。该方程(PE3)反映了倍率与电荷损耗(库仑效率)之间的关系,排除了剩余电荷量的影响,更适合于动态工况下的荷电状态(State of charge,SOC)估计。另外磷酸铁锂电池试验表明剩余电荷量与电流倍率的关系规律性更强,更符合Peukert形式的方程(PE2),与铅酸电池Peukert模型的扩散机理一致,故剩余电荷量也可据此估计。
文摘以纳米Li Fe PO4锂离子电池为研究对象,在50--450 A和-18~50℃范围内,对其充放电特性、Peukert模型与温度的关系进行了讨论,利用Ragone曲线对阀控式密封铅酸动力电池、镍氢动力电池及锰酸锂离子电池的能量功率特性进行了对比分析。研究表明,该纳米Li Fe PO4锂离子电池的快速放电能力和能量功率特性都得到很大改善,尤其适合于高温工况;低温性能依然还是纳米Li Fe PO4锂离子电池的弱点,亟待进一步提高。
文摘To overcome the problems encountered in predicting the endurance of electricpowered fixed-wing unmanned aerial vehicles(UAVs),which were stemmed from the dynamic changes in electric power system efficiency and battery discharge characteristics under different operating conditions,the required battery power model and battery discharge model were studied.The required battery power model was determined using an approximate model of electric power system efficiency based on wind tunnel testing and the self-adaptive penalty function.Furthermore,current correction and ambient temperature correction terms were proposed for the trained Kriging model representing the discharge characteristics under standard operation,and then the discharged capacity-terminal voltage model was established.Through numerical integration of this model with the required battery power model,the electric-powered fixed-wing UAV endurance prediction model was obtained.Laboratory tests indicated that the proposed endurance model could precisely calculate the battery discharge time and accurately describe the battery discharge process.The similarity of the theoretical and flight test results reflected the accuracy of the proposed endurance model as well as the importance of considering dynamic changes in power system efficiency in endurance calculations.The proposed endurance model meeting precision requirements can be used in practical engineering applications.
