机翼盒段静态破坏试验夹具补强的数值模拟  

Numerical Simulation on Clamping Fixture of Composite Wing Box in Static Broken Test

作　　者：刘华峰[1] 赵凯辉[2] 林涛[3] 游进[3] 

机构地区：[1]西北工业大学力学和土木建筑学院,陕西西安710072 [2]河南理工大学机械与动力工程学院,河南焦作454000 [3]成都飞机工业(集团)有限责任公司,四川成都610091

出　　处：《热加工工艺》2010年第17期45-47,共3页Hot Working Technology

基　　金：国家863高技术研究发展计划资助项目(2009AA04Z418);国家自然科学基金资助项目(50775183)

摘　　要：针对复合材料中厚蒙皮机翼盒段静态弯曲破坏试验中盒段加载部分遭到破坏试验无法进行的问题,运用Abaqus对盒段局部破坏部分建立三维有限元模型进行应力分析。结果表明:盒段加载部分刚度分配不均,致使外力在加载螺栓中分布不均,导致结构加载部分局部应力集中造成强度不足引起破坏。重新优化设计夹具并对盒段加载部分提出了三种补强试验装置的设计方案,根据应力分析和对比,确定了最终的补强试验装置。补强后的盒段顺利通过了试验,解决了工程难题。Aiming to the problem of the broken of the load part of wing box in the static bending experiment,which was used in the thick skin,the stress was ananlyzed by 3D-finite element model which was established by Abaqus.The results show that the non-uniform distributed pin load which is caused by non uniform rigidity distribution of the broken structure leads to the stress concentration,the stress concentration makes the structure damage.Three remedial treatments for the new clamping fixture is presented.According to the contrast of the contours of Mises stress,the final improved clamping fixture is confirmed.The improved clamping fixture can pass the test,solving the problems in engineering.

关 键 词：数值模拟 刚度分配 钉载分配 优化设计 

分 类 号：TP391[自动化与计算机技术—计算机应用技术] V214.8[自动化与计算机技术—计算机科学与技术]