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

复合材料层板衬套强化孔的疲劳寿命增益分析
引用本文:刘一兵,孟仲伟.复合材料层板衬套强化孔的疲劳寿命增益分析[J].航空学报,1998,19(5):585-587.
作者姓名:刘一兵  孟仲伟
作者单位:西北工业大学强度研究所,西安,710072
摘    要: 介绍了复合材料层板机械连接孔一种衬套强化工艺方法的应用性研究结果。实验分析表明,采用衬套连接技术能够有效改善和提高复合材料连接孔的原始疲劳品质及其耐久性寿命,并具有稳定的寿命增益比。通过改变衬套材料与装配方法,获得了孔的不同疲劳损伤变形对比结果。初步实现了复合材料连接强化技术的可行性尝试。

关 键 词:强化衬套  寿命增益  损伤变形  

ANALYSIS OF INCREMENT FOR THE FATIGUE LIFE OF BUSHING INTENSIFIED HOLE ON COMPOSITE LAMINATE PLATE
Liu Yibing,Meng Zhongwei.ANALYSIS OF INCREMENT FOR THE FATIGUE LIFE OF BUSHING INTENSIFIED HOLE ON COMPOSITE LAMINATE PLATE[J].Acta Aeronautica et Astronautica Sinica,1998,19(5):585-587.
Authors:Liu Yibing  Meng Zhongwei
Institution:Strength Research Institute, Northwestern Polytechnical University, Xi'an, 710072
Abstract:The intensifying bushing technique was used to extend the fatigue life of the mechanical linking hole on the composite laminate plate. The damage deformation analysis for ordinary fit bolt connections hole, interference fit bolt connections hole and bushing fit connections hole under 3×10 5 designed life shows that the bushing technique can improve the original fatigue quality and durability of mechanical holes of laminate plates obviously, and the technique possesses a stable increment ratio of fatigue life. The fatigue life N 95/95  based on the two parameter Weibull distribution makes it known that the intensifying bushing joint can get a life increment by 7.3 times as against ordinary joint, and life increment by 1.5 times as against interference joint. For three typical kinds of bushing materials the specific deformation target and the analysis conclusion are given.
Keywords:intensifying bushing  life increment  damage deformation
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
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