首页|基于模态结构应力法的焊接构架振动疲劳寿命研究

基于模态结构应力法的焊接构架振动疲劳寿命研究

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文章结合模态叠加法,提出了一种基于模态法的结构应力计算方法;然后基于刚柔耦合理论,建立了考虑构架柔性的刚柔耦合动力学模型,并利用虚拟激励法再现了转向架构架的真实服役环境,对服役条件下焊接构架的动态薄弱位置进行了识别,确定了焊接车架上的10个动态薄弱点,在连接侧梁外垂直板和下盖板的焊缝处观察到了最高的结构应力(均方根值为65 MPa).最后,基于主S-N曲线法对焊接构架薄弱位置的服役寿命进行了预测.结果表明:随着曲线半径的增大,构架薄弱位置的损伤呈现出逐渐减小的规律;其损伤最大位置出现在侧梁外立板与抗侧滚扭杆座焊缝处,在1 200万km的寿命要求下,其损伤为2.74,安全裕量较低.
Research on vibration fatigue life of welded frame based on modal structural stress method
Combined with the modal superposition method,a structural stress calculation method based on the modal method is proposed.Then,based on the rigid-flexible coupling theory,a dynamic model of rigid-flexible coupling considering the flexibility of the frame was established,and the real service envi-ronment of the bogie frame was realized by using the virtual excitation method.The dynamic weak posi-tions of the welded frame under service conditions were identified,10 dynamic weak points on the welded frame were determined,and the highest structural stress(root mean square value of 65 Mpa)was ob-served at the weld joint connecting the outer vertical plate and the lower cover plate of the side beam.Fi-nally,based on the main S-N curve method,the service life of the weak position of the welded frame is predicted.The results show that with the increase of the radius of the curve,the damage of the weak posi-tion of the frame shows a gradual decreasing law.The maximum damage position occurs at the weld joint position of the side beam outer vertical plate and the anti-roll torsion bar seat,and the damage is 2.74 under the life requirement of 12 million kilometers,and the safety margin is low.

welded framerigid-flexible coupling dynamicsstructural stressmodal superposition methodfatigue life prediction

吕晓鹏、邹洪伟、董晓华、李世杰、吴兴文

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中车青岛四方机车车辆股份有限公司,山东青岛 266111

成都地铁运营有限公司,四川成都 610031

轨道交通运载系统全国重点实验室,四川成都 610031

西南交通大学机械工程学院,四川成都 610031

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焊接构架 刚柔耦合动力学 结构应力 模态叠加法 疲劳寿命预测

国家重点研发计划国家自然科学基金资助项目四川省应用基础研究

2018YFE0201401518054502020YJ0075

2024

机车车辆工艺
中国南车集团戚墅堰机车车辆厂

机车车辆工艺

影响因子:0.098
ISSN:1007-6034
年,卷(期):2024.60(3)
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