首页|动车组冷却单元立柱的焊缝疲劳开裂原因分析与结构改进

动车组冷却单元立柱的焊缝疲劳开裂原因分析与结构改进

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针对动车组冷却单元铝立柱焊缝在服役过程中出现的疲劳开裂问题,文中首先基于三区间方法对IEC 61373标准中规定的模拟长寿命随机振动工况进行疲劳损伤计算,结果表明,铝立柱最大疲劳损伤为0.27,满足使用要求.然后参考线路实测气动载荷数据,计算底板在500 Pa气动压力条件下铝立柱1的疲劳寿命为4.14×105次,与实际服役寿命和开裂位置较为吻合,表明立柱疲劳开裂的原因应归结为服役过程中的动态气动载荷.最后针对改进后的钢立柱开展了疲劳评估,结果表明,2种疲劳工况下,立柱疲劳寿命均显著提高,参考铝立柱的实际服役寿命,可以推断钢立柱疲劳强度满足使用要求.
Analysis of weld fatigue cracking causes and structural improvement of the cooling unit columns of EMU
For the weld fatigue cracking of the aluminum column of the EMU cooling unit in service,the fatigue damage was firstly calculated based on the three intervals method for the simulated long-life random vibration condition specified in the IEC 61373 in this paper,and the results showed that the maximum fatigue damage of the aluminum column was 0.27,which met the use requirements.Then,with reference to the measured aerodynamic load data of the line,the fatigue life of the aluminum column under the condition of 500 Pa aerodynamic pressure on bottom plate was calculated to be 4.14×105 cycles,which was more consistent with the actual service life and crack location,indicating that the cause of fatigue cracking of the column should be attributed to the dynamic aerodynamic load in the service.Finally,a fatigue evaluation of the improved steel column was carried out.The results showed that the fatigue life of the column was significantly improved under both fatigue conditions,and it could be inferred that the fatigue strength of the steel column met the service requirements by referring to the actual service life of the aluminum column.

cooling unitfatigue damagestructural stressrandom vibration fatiguethree intervals method

李杨、王硕、严兵、李永富、宋宇豪、张欣然

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中车大连机车研究所有限公司,辽宁 大连 116022

大连交通大学机车车辆工程学院,辽宁 大连 116028

冷却单元 疲劳损伤 结构应力 随机振动疲劳 三区间法

国家高速列车技术创新中心研发计划国家自然科学基金辽宁省教育厅基本科研项目

CXKY-02-01-02202052005385LJKZ0497

2024

焊接技术
天津市焊接研究所 中国工程建设焊接协会

焊接技术

CSTPCD
影响因子:0.286
ISSN:1002-025X
年,卷(期):2024.53(2)
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