首页 | 本学科首页   官方微博 | 高级检索  
     检索      

单面螺纹抽钉干涉配合复合材料连接结构的疲劳性能研究
引用本文:魏景超,柴亚南,刘风雷,迟坚.单面螺纹抽钉干涉配合复合材料连接结构的疲劳性能研究[J].航空制造技术,2017(22).
作者姓名:魏景超  柴亚南  刘风雷  迟坚
作者单位:1. 中国飞机强度研究所,西安,710065;2. 中国航空制造技术研究院,北京,100024
摘    要:通过疲劳试验研究了单面螺纹抽钉干涉配合复合材料连接结构的疲劳性能,分别考虑了紧固件类型、干涉配合量、搭接板材料及铺层次序等影响因素。采用了拉压疲劳试验,拉压比R=-1,循环应力水平则根据静载极限挤压强度值选定。根据疲劳试验循环应力和疲劳寿命曲线(S-N曲线),得到了不同影响因素对疲劳寿命的影响规律。结果表明,选择适当的干涉配合量、紧固件类型及搭接板均能提高结构的疲劳寿命,4种不同主板铺层次序均对结构疲劳寿命影响不大。

关 键 词:螺纹抽钉  干涉配合  疲劳寿命  循环挤压载荷  复合材料层合板

Effect of Several Influencing Factors on Fatigue Behaviour of Interference-Fit Bolted Composite Joints
WEI Jingchao,CHAI Ya&#;nan,LIU Fenglei,CHI Jian.Effect of Several Influencing Factors on Fatigue Behaviour of Interference-Fit Bolted Composite Joints[J].Aeronautical Manufacturing Technology,2017(22).
Authors:WEI Jingchao  CHAI Ya&#;nan  LIU Fenglei  CHI Jian
Institution:WEI Jingchao,CHAI Ya'nan,LIU Fenglei,CHI Jian
Abstract:An experimental investigation was conducted to determine the effect of several influencing factors on the fatigue behavior of interference-fit bolted composite joints. The types of bolts, the sizes of interference fit, different materials of laps, and stacking sequences of main laminates were separately considered. Tension-compression reversed force/stress ratio, R=-1, was selected to evaluate the fatigue tests. The appropriate levels of fatigue stress were determined by the ultimate bear-ing strength of the fastener structure obtained from the static tensile tests. The bearing stress and the fatigue life (S-N) data of all specimens were presented and the relationship between influencing factors and fatigue life were obtained. The experimental results show that the appropriate size of interference fit, the right type of fasteners, and the matched laps could improve the fatigue life of composite joints; however four stacking sequences of main laminates are not sensitive to the fatigue life of com-posite joints.
Keywords:Bolted joint  Interference fit  Fatigue life  Cyclic bearing load  Composite laminate
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号