摘要
本工作以TA1自冲铆接头为研究对象,基于拉伸-剪切和疲劳试验分析了接头的力学性能,并采用扫描电镜从微观层面研究了接头的拉伸-剪切失效机理、疲劳失效机理及微动行为。结果表明:拉伸-剪切失效模式为铆钉腿部从下板拉脱,铆钉颈部存在不同程度的断裂。疲劳失效模式主要为上板断裂失效,其疲劳极限约为1.18kN。疲劳裂纹从上板与铆钉头接触部位萌生,在持续微动磨损及疲劳循环应力作用下,沿板厚和板宽方向不断扩展,直至接头疲劳断裂。微动磨损的剧烈程度直接影响接头疲劳失效模式。上板与铆钉头接触区的微动磨损源于板宽W区域,随着微动过程的不断进行,逐步向板长L区域扩展。
The present work mainly focused on the self-piercing riveted(SPR)joint of TA1 titanium alloy.The tensile-shear test and fatigue test were conducted to analyze the mechanical performance of the joints,and the tensile-shear failure mechanism,fatigue failure mechanism and fretting behavior of the joints were investigated at a microscopic level by scanning electron microscope.The results exhibited that the tensile-shear failure mode assumed rivet shank pull-out from the bottom sheet and some degree of fracture located at the rivet neck,while the main fatigue failure mode was fracture of the upper sheet whose fatigue limit was approximately 1.18 kN.Fatigue cracks initiated at pierced sheet surface’s contact site with rivet head,and were propagated along the sheet thickness direction and sheet width direction under continuous fretting wear and fatigue cyclic stress,and finally resulted in joint break.The severity of fretting wear could influence fatigue failure mode of the joints.Fretting wear of the upper sheet initiated from W direction of sheet width,and spread gradually to L direction of sheet length with fretting wear process.
作者
赵伦
何晓聪
张先炼
丁燕芳
刘洋
邓聪
ZHAO Lun;HE Xiaocong;ZHANG Xianlian;DING Yanfang;LIU Yang;DENG Cong(Faculty of Mechanical and Electrical Engineering,Kunming University of Science and Technology,Kunming 650500;Department of Mechanical Engineering,Blekinge Tekniska H gskola,Karlskrona 37179)
出处
《材料导报》
EI
CAS
CSCD
北大核心
2018年第20期3579-3583,共5页
Materials Reports
基金
国家留学基金委(201500090194)
国家自然科学基金(51565023)。
关键词
钛合金
自冲铆接头
裂纹萌生
裂纹扩展
微动行为
力学性能
titanium alloy
self-piercing riveted joint
crack initiation
crack propagation
fretting behavior
mechanical performance