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Fracture limit prediction for a double safety structure in cylindrical-type lithium secondary batteries

机译:圆柱型锂二次电池双安全结构的断裂极限预测

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摘要

In this study, a double safety structure used for cylindrical-type lithium secondary batteries is newly introduced. The structure is necessary to prevent users and the cylindrical-type secondary batteries from unpredictable explosions due to a temporary increase in the inner pressure of the batteries. The double safety structure consists of a primary safety component as micro half-blanked component, and a secondary safety device as V-notched part. For the double safety device, both the mentioned components are considered by the micro half-blanking and the V-notch forming processes with numerical and experimental predictions for the fracture limit. The mechanical properties are investigated with both a raw and an annealed thin sheet material of 1050-H16 aluminum alloy. The main process parameters are considered to be the clearance and punch-die corner radius for the micro half-blanking process, and the remaining thickness, tip radius, and shape angle of the V-notch. In this study, finite element simulations are carried out to verify the manufacturing process with the mentioned process parameters. The ductile fracture criterion is also adopted to predict the fracture limit for each component. Furthermore, experimental investigations are included to verify the fracture limit predicted from the numerical approach. From the systematic approaches, it is confirmed that the fracture limit for the double safety structure is well predicted, and satisfies the required fracture limit.
机译:在这项研究中,新引入了一种用于圆柱型锂二次电池的双重安全结构。该结构对于防止使用者和圆柱形二次电池由于电池内部压力的暂时增加而引起的不可预测的爆炸是必要的。双重安全结构由一个主要的安全组件(作为微型半空白组件)和一个次要的安全设备(作为V型缺口部分)组成。对于双重安全装置,上述两个部件均通过微型半冲裁和V形缺口成型工艺进行了考虑,并具有针对断裂极限的数值和实验预测。用1050-H16铝合金的原始和退火薄板材料研究了机械性能。主要工艺参数被认为是微型半冲裁工艺的间隙和冲模角半径,以及V形缺口的剩余厚度,尖端半径和形状角。在这项研究中,进行了有限元模拟以验证具有上述工艺参数的制造工艺。还采用韧性断裂准则来预测每个部件的断裂极限。此外,还包括实验研究以验证通过数值方法预测的断裂极限。通过系统的方法,可以确定双重安全结构的断裂极限可以很好地预测,并满足所需的断裂极限。

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  • 来源
    《Materials & design》 |2010年第10期|P.4897-4912|共16页
  • 作者单位

    Department of Aerospace Engineering, Pusan National University, Geumjeong-gu, Busan 609-735, South Korea;

    rnIndustrial Liaison Innovation Center, Pusan National University, Geumjeong-gu, Busan 609-735, South Korea;

    rnDepartment of Aerospace Engineering, Pusan National University, Geumjeong-gu, Busan 609-735, South Korea;

    rnDepartment of Aerospace Engineering, Pusan National University, Geumjeong-gu, Busan 609-735, South Korea;

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