首页|期刊导航|电子元件与材料|IGBT模块在机械振动与循环热载荷耦合作用下的疲劳失效机理研究

IGBT模块在机械振动与循环热载荷耦合作用下的疲劳失效机理研究OA

A study on fatigue failure mechanism of IGBT modules under coupled mechanical vibration and cyclic thermal loading

中文摘要英文摘要

为探究多物理场耦合作用下大功率绝缘栅双极型晶体管(IGBT)模块的内部损伤演化机理与疲劳寿命,基于Miner线性累积损伤等理论模型,通过有限元仿真分析,建立了IGBT在单一热载荷、单一振动载荷及跨时间尺度热-振耦合载荷下的疲劳寿命预测模型.仿真结果显示:热载荷对寿命的影响显著高于振动载荷,而热-振耦合条件会进一步加速材料退化,使疲劳寿命显著降低.为验证仿真结果,开展了直流功率循环加速老化实验,仿真与实验误差为 24.05%,二者均表明危险部位主要集中在芯片和上焊接层区域,并从芯片位置向周围扩散.该研究对IGBT模块的可靠性评估、寿命预测及优化设计具有重要的工程参考价值.

To investigate the internal damage evolution mechanism and fatigue life of high-power Insulated Gate Bipolar Transistor(IGBT)modules under multi-physics field coupling effects,fatigue life prediction models were established for IGBTs under single thermal loading,single vibrational loading,and thermal-mechanical coupled loading across multiple time scales.The establishment of these models was based on the integration of theoretical models(e.g.,the Miner linear cumulative damage rule)and the conduct of finite element simulation analysis.Accelerated aging tests based on DC power cycling were conducted to validate the simulation results.The simulation results demonstrate that thermal loading exerts a substantially more pronounced influence on fatigue degradation than vibrational loading.Furthermore,material degradation accelerates under thermal-mechanical coupling conditions,consequently leading to a significant decrease in fatigue life.Both simulation and experimental results consistently identify the chip and the upper solder layer as primary failure hotspots,with damage initiating from the chip and propagating outward;The deviation between the simulated and experimental data is 24.05%.This study provides significant engineering reference value for the reliability assessment,life prediction,and optimized design of IGBT modules.

刘堰祯;王维民;户东方;陈奕屹

北京化工大学 高端机械装备健康监控与自愈化北京市重点实验室,北京 100029北京化工大学 高端机械装备健康监控与自愈化北京市重点实验室,北京 100029北京化工大学 高端机械装备健康监控与自愈化北京市重点实验室,北京 100029北京石油化工学院 机械工程学院,北京 102617

信息技术与安全科学

IGBT模块热-振耦合疲劳寿命可靠性

IGBT modulethermal-mechanical couplingfatigue lifereliability

《电子元件与材料》 2026 (2)

191-200,207,11

国家重点研发计划(2018YFB1201801-4)

10.14106/j.cnki.1001-2028.2026.1348

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