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

有机玻璃残余应力与双折射条纹的关系
引用本文:王自明.有机玻璃残余应力与双折射条纹的关系[J].航空学报,1985,6(2):141-147.
作者姓名:王自明
作者单位:北京航空材料研究所
摘    要: 本文通过实验,讨论了有机玻璃残余应力与双折射条纹(冻结应力条纹和热应力条纹)的定量关系,得出可以根据热应力条纹由应力光学定律直接获取有机玻璃残余应力的结论。作者基于这一论点,考察了不同冷却条件下平板有机玻璃残余应力沿断面的分布规律;研究了热处理工艺参数对消除有机玻璃残余应力的影响;测定了三种不同型号飞机舱玻璃的残余应力。

关 键 词:
收稿时间:1984-05-30;

RELATIONSHIP BETWEEN RESIDUAL STRESS AND BIREFRINGENCE FRINGES IN POLYMETHYLMETHACRYLATE
Wang Ziming.RELATIONSHIP BETWEEN RESIDUAL STRESS AND BIREFRINGENCE FRINGES IN POLYMETHYLMETHACRYLATE[J].Acta Aeronautica et Astronautica Sinica,1985,6(2):141-147.
Authors:Wang Ziming
Institution:institute of Aeronautical Materials
Abstract:It is one of the key technical problems for determining residual stress by means of photoelastic method to clarify the relationship between residual stress and birefringence fringes, i. e. isochromatic fringes caused by frozen stress and thermal stress, in polymethylmethacrylate (PMMA).The relationship is investigated by means of annealing and making a cut in frozen stress specimen only containing the fringe caused by frozen stress and in the first slice of thermal stress specimen prepared by cooling only. It is concluded that the residual stress in PMMA depends only upon the thermal stress caused by cooling, and is irrelevant to the loads added at high elastic state and to the amount of the fringe caused by frozen stress, and furthermore the relationship between the residual stress and the amount of thermal stress fringe conforms to the stress-optical law. Equa-tion( 3 )is the expression for such relationship and can be used to determine the residual stress quantitatively in engineering. In illustration of application, the distributions of the residual stresses in PMMA specimens cooled at different speeds are examined (Fig. 9 ), the residual stresses in two different types of canopies are determined (Fig. 10), quantitative relationship between annealing temperature and residual stress is established (Fig.11), and distributions of the residual stresses in DYB-4 PMMA in different parts of a canopy are considered. It is shown that the conclusions drawn in fhis paper may be useful for quantitative determination of residual stress in PMMA, and benefit the quality control, life prediction and failure analysis of PMMA airplane canopies.
Keywords:
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