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

SMA 智能复合构件控制裂纹的数值与试验研究
引用本文:张学仁,聂景旭,杜彦良.SMA 智能复合构件控制裂纹的数值与试验研究[J].航空动力学报,1998,13(4):357-360.
作者姓名:张学仁  聂景旭  杜彦良
作者单位:北京航空航天大学,石家庄铁道学院
摘    要:将TiNi形状记忆合金(SMA)薄带复合于基体材料内部,利用形状记忆合金的特性,可以控制构件裂纹的扩展。本文介绍了智能复合构件控制裂纹的机理,并利用拟温度载荷法,直接应用现有有限元程序对控制裂纹的SMA智能复合构件进行了计算与分析,同时还进行了激光云纹干涉法试验测试。计算和试验结果表明智能复合构件中的记忆合金薄带对构件裂纹有显著的控制效果,同时计算和试验结果的一致性也表明本文的分析方法是可行的。

关 键 词:形状记忆合金  主动  控制  裂纹
收稿时间:5/1/1998 12:00:00 AM
修稿时间:6/1/1998 12:00:00 AM

STUDY ON SMA INTELLIGENT STRUCTURES FOR CRACK CONTROL
Zhang Xueren,Nie Jingxu and Du Yanliang.STUDY ON SMA INTELLIGENT STRUCTURES FOR CRACK CONTROL[J].Journal of Aerospace Power,1998,13(4):357-360.
Authors:Zhang Xueren  Nie Jingxu and Du Yanliang
Institution:4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 100083;4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 100083;Mechanical Engineering Dept.Shijiazhuang Railway Institute,Shijiazhuang 050043
Abstract:The shape memory effect of Shape Memory Alloy (SMA) was used for crack active control in an intelligent component,which was made up with TiNi belts embedded in metal matrix.A linearized constitutive relation of SMA embedded in the matrix has been derived.Such a constitutive relation can be used easily in commercial finite element programs to treat the shape memory effect as the thermal effect of conventional materials.This method was applied to the numerical ananlysis of the intelligent component.Moire Interferometric tests were carried out on the component.Comparison of the calculated with test results shows that the effect of the active control is remarkable,and the computational method is feasible.
Keywords:Shape memory alloys  Active  Control  Cracks  
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》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