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

复杂结构多裂纹扩展相互影响的研究
引用本文:廖敏,杨庆雄.复杂结构多裂纹扩展相互影响的研究[J].航空学报,1993,14(9):524-528.
作者姓名:廖敏  杨庆雄
作者单位:西北工业大学502教研室,西安 710072
基金项目:航空科学基金,西北工业大学青年基金
摘    要:针对多传力路线复杂结构具有多个疲劳源、多条裂纹同时扩展且相互影响的特点,提出一种变柔度方法来考虑多裂纹间的相互影响,并设计专门的双孔板试验验证。应用该方法试算了多钉多层复杂接头全寿命,表明该变柔度方法在工程上是可行的。

关 键 词:复杂结构  多裂纹  变柔度  全寿命  
收稿时间:1992-01-09
修稿时间:1992-05-14

INTERACTION AMONG MULTIPLE CRACKS PROPAGATION FOR COMPLEX STRUCTURE
Liao Min,Yang Qing-xiong.INTERACTION AMONG MULTIPLE CRACKS PROPAGATION FOR COMPLEX STRUCTURE[J].Acta Aeronautica et Astronautica Sinica,1993,14(9):524-528.
Authors:Liao Min  Yang Qing-xiong
Institution:Faculty 502, Northwestern Polvtechnical University, Xi'an, 710072
Abstract:In this paper, the interaction among multiple cracks propagation in some complex engineering structures with multi load-path is studied by varying the local flexibility. A method to calculate the variation of local flexibility and to make a sequence of reanalyzing of stress distribution during crack propagation is provided, and a special designing fatigue experiment using a two hole plate specimen with four hole -edge cracks is carried out. The experimental and calculating results are in good agreement, and some useful conclusions about the interaction among multiple cracks propagation are obtained through this special experiment. Finally, this method is used to predict the total life of a complex joint with multi-fastener and multi-layer. The comparison between predicting and experimental results shows further that this method is suitable for engineering practice.
Keywords:complex structure  multiple cracks  total life  varying the local flexibility  
本文献已被 CNKI 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