Please wait a minute...
 
材料工程  2018, Vol. 46 Issue (8): 156-162    DOI: 10.11868/j.issn.1001-4381.2017.000370
  研究论文 本期目录 | 过刊浏览 | 高级检索 |
YB-DM-10航空定向有机玻璃疲劳裂纹扩展性能
赵景云1, Bamber BLACKMAN2, 颜悦1, 张旋1, 张晓雯1
1. 中国航发北京航空材料研究院, 北京 100095;
2. 英国帝国 理工学院, 伦敦 SW7 2AZ
Fatigue Crack Propagation Property of YB-DM-10 Directional PMMA
ZHAO Jing-yun1, Bamber BLACKMAN2, YAN Yue1, ZHANG Xuan1, ZHANG Xiao-wen1
1. AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China;
2. Imperial College London, London SW7 2AZ, UK
全文: PDF(3824 KB)   HTML()
输出: BibTeX | EndNote (RIS)      
摘要 通过研究定向有机玻璃(YB-DM-10)疲劳裂纹扩展性能,得到该种定向有机玻璃疲劳断裂阈值。发现其疲劳裂纹扩展速率曲线遵循Pairs公式以及Walker公式。研究平面内不同角度、不同频率和应力比对疲劳裂纹扩展的影响;通过对比Paris公式以及Walker公式的回归系数以及断裂表面不同阶段的扫描图像,分析不同参数对疲劳裂纹扩展的影响。结果表明:材料板材平面内,不同切割角度的试样疲劳裂纹扩展速率基本相同;加载频率对疲劳裂纹扩展速率影响不大,但在da/dN-△K曲线的第三阶段,数据有分离的趋势;相同的△K情况下,应力比增大,疲劳裂纹扩展速率增加。本工作结果为该种定向有机玻璃的应用以及航空座舱透明件损伤容限性能研究奠定了基础。
服务
把本文推荐给朋友
加入引用管理器
E-mail Alert
RSS
作者相关文章
赵景云
Bamber BLACKMAN
颜悦
张旋
张晓雯
关键词 定向有机玻璃疲劳裂纹扩展阈值切割角度频率应力比    
Abstract:The threshold value of stress intensity factor range was acquired according the study of fatigue crack propagation property of directional PMMA (YB-DM-10). It was found that the plot of fatigue crack propagation rate is accordance with Pairs Law and Walker Law. The effect of angles in plane, frequency and stress ratio on the fatigue crack propagation was studied. According the comparison of coefficient in Pairs Law, Walker Law and morphology SEM in fracture surface under test conditions with different parameters, the effect of different parameters on fatigue crack propagation rate was analysed. Results show that the fatigue crack propagation rates of test specimens with different cutting angle in XY plane of PMMA sheet are nearly the same. The frequency has slight effect on the fatigue crack propagation, except that data become separate in the third region of da/dN-△K plot. On the condition of same stress intensity factor range, the fatigue crack propagation rate accelerates as the stress ration increases. The result of the study established foundation for the application of directional PMMA and the research on the damage tolerance of transparent materials used in aircraft cockpit canopies.
Key wordsdirectional PMMA    fatigue crack propagation    threshold    cutting angle    frequency    stress ratio
收稿日期: 2017-03-27      出版日期: 2018-08-17
中图分类号:  TG335  
通讯作者: 颜悦(1966-),男,研究员,博士,研究方向为透明材料,联系地址:北京市81信箱83分箱(100095),E-mail:yue.yan@biam.ac.cn     E-mail: yue.yan@biam.ac.cn
引用本文:   
赵景云, Bamber BLACKMAN, 颜悦, 张旋, 张晓雯. YB-DM-10航空定向有机玻璃疲劳裂纹扩展性能[J]. 材料工程, 2018, 46(8): 156-162.
ZHAO Jing-yun, Bamber BLACKMAN, YAN Yue, ZHANG Xuan, ZHANG Xiao-wen. Fatigue Crack Propagation Property of YB-DM-10 Directional PMMA. Journal of Materials Engineering, 2018, 46(8): 156-162.
链接本文:  
http://jme.biam.ac.cn/CN/10.11868/j.issn.1001-4381.2017.000370      或      http://jme.biam.ac.cn/CN/Y2018/V46/I8/156
[1] 张志林,姚卫星,傅祥炯.座舱玻璃划伤容限研究[J].航空学报,2004, 25(6):569-572. ZHANG Z L,YAO W X,FU X J. Investigation on scratch tolerance of the cabin glass[J].Acta Aeronautica et Astronautica Sinica,2004, 25(6):569-572.
[2] WILLOAMSJ G. A model of fatigue crack growth in polymers[J]. Journal of Material Science, 1977, 12(1):2525-2533.
[3] CHOU Y F, SUN C T. Modeling of the frequency effect on fatigue crack propagation in PMMA[J]. Engineering Fracture Mechanics,1983, 17(1):17-26.
[4] YUEN B K C, TAHERI F. The effects of loading frequency, tensile overload and compressive underload on the fatigue crack propagation behavior of polymethyl methacrylate[J]. Polymer Testing, 2004, 23:491-500.
[5] RAMSTEINER F, ARMBRUST T. Fatigue crack growth in polymers[J]. Polymer Testing, 2001, 20:321-327.
[6] EVANS S L. Fatigue crack propagation under variable amplitude loading in PMMA and bone cement[J]. J Mater Sci, 2007, 18:1711-1717.
[7] 高宗战,刘伟,岳珠峰,等.有机玻璃疲劳裂纹扩展[J].材料科学与工程学报, 2008, 26(1):90-93. GAO Z Z,LIU W,YUE Z F, et al. Fatigue crack propagation in polyethylene methacrylate[J].Journal of Materials Science and Engineering,2008, 26(1):90-93.
[8] LIU Y S, GAO Z Z, LIU W, et al. Analytical and experimental investigation of fatigue crack propagation for polyethylene methacrylate[J].Materials Science and Engineering:A, 2008, 486(1):363-368.
[9] 贾敬华,李亚智,肖健. YB-MD-3有机玻璃的疲劳裂纹扩展特性研究[J]. 航空材料学报, 2006,26(5):109-112. JIA J H, LI Y Z, XIAO J. Study on fatigue crack propagation behavior of YB-MD-3 PMMA plates[J].Journal of Aeronautical Materials,2006, 26(5):109-112.
[10] 王泓,鄢君辉,郑修麟. 有机玻璃疲劳裂纹扩展表达式及控制参量[J]. 航空学报, 2001, 26(5):83-86. WANG H, YAN J H, ZHENG X L. Formulae and governing parameters of fatigue crack propagation in polymethyl methacrylate[J].Acta Aeronautica et Astronautica Sinica,2001,26(5):83-86.
[11] 肖健. MDYB-3航空有机玻璃疲劳裂纹特性的实验研究[D].西安:西北工业大学,2004. XIAO J. Experimental investigation on fatigue crack propagation characteristic of aeronautical PMMA called YB-MD-3[J].Xi'an:Northwestern Polytechnical University,2004.
[12] HAO W, MA L T, CHEN X W, et al. Comparison of the fatigue crack propagation behavior of two different forms of PMMA using two-stage zone model[J]. Journal of Materials Engineering & Performance, 2016, 25(2):493-501.
[13] 朱子华.双轴定向有机玻璃的定向度均匀性的研究[J].材料工程,1993(3):42-44. ZHU Z H. Study on the phenomenon and pattern of orientation of biaxial stretching orientated organic glass[J]. Journal of Materials Engineering, 1993(3):42-44.
[14] KANTERS M J W, STOLK J, GOVAERTAN L E. Direct comparison of the compliance method with optical tracking of fatigue crack propagation in polymers[J]. Polymer Testing, 2015, 46(1):98-107.
[15] De SOUZA J M, YOSHIMURA H N, PERES F M,et al. Effect of sample pre-cracking method and notch geometry in plane strain fracture toughness tests as applied to a PMMA resin[J].Polymer Testing, 2012, 31:834-840.
[16] 许凤和, 薛建高.有机玻璃疲劳裂纹扩展实验分析[J].材料工程,1999(10):40-41. XU F H, XUE J G. Experimental analysis of fatigue crack growth for PMMA[J]. Journal of Materials Engineering, 1999(10):40-41.
[17] CICERO S, MADRAZO V, GARCIA T, et al. On the notch effect in load bearing capacity, apparent fracture toughness and fracture mechanisms of polymer PMMA, aluminum alloy Al7075-T651 and structural steels S275JR and S355J2[J].Engineering Failure Analysis, 2013,29(1):108-121.
[1] 于丽新, 兰晓琳, 邵枫, 刘艇安, 张诗琪, 王志江. MWCNT/FeNi复合纳米线制备及其雷达微波和工频电磁波吸收性能[J]. 材料工程, 2018, 46(8): 64-70.
[2] 董慧民, 钱黄海, 程丽君, 苏正涛, 刘嘉, 王文志, 牟维琦. 石墨烯/橡胶导电纳米复合材料的研究进展[J]. 材料工程, 2017, 45(3): 17-27.
[3] 张晓雯, 吴南, 张旋, 马丽婷, 厉蕾. 透明聚碳酸酯材料疲劳断裂行为[J]. 材料工程, 2017, 45(11): 30-35.
[4] 张玉波, 郭荣鑫, 夏海廷, 颜峰, 林志伟. WCp含量对粉末冶金Cu/WCp复合材料疲劳裂纹扩展行为的影响[J]. 材料工程, 2017, 45(1): 85-92.
[5] 黄俊钦, 林有希. 制动频率对CaSO4晶须增强树脂基复合摩擦材料性能的影响[J]. 材料工程, 2016, 44(2): 94-100.
[6] 许天旱, 王荣, 冯耀荣, 雒设计, 王党会, 杨宝. 应力比对K55套管钻井钢疲劳裂纹扩展性能的影响[J]. 材料工程, 2015, 43(6): 79-84.
[7] 杨冬野, 曹福洋, 许文勇, 左欣, 李周, 张国庆, 孙剑飞. 喷射成形GH738合金的疲劳裂纹扩展行为[J]. 材料工程, 2014, 0(7): 55-59.
[8] 朱敏, 杜翠薇, 李晓刚, 刘智勇, 赵天亮, 李建宽, 胡杰珍. 交流电频率对X65钢在CO32-/HCO3-溶液中腐蚀行为的影响[J]. 材料工程, 2014, 0(11): 85-89.
[9] 刘建, 张永振, 杜三明, 刘敬超. PTFE编织复合材料摩擦特性研究[J]. 材料工程, 2012, 0(8): 69-72.
[10] 严益民, 胡正飞, 林富生, 赵双群. 汽轮机转子30Cr1Mo1V钢长期服役状态下的高温疲劳行为[J]. 材料工程, 2012, 0(11): 38-41,96.
[11] 宫玉辉, 刘铭, 张坤, 黄敏, 伊琳娜, 戴圣龙. 不同腐蚀环境对7475-T7351铝合金疲劳性能及裂纹扩展速率的影响[J]. 材料工程, 2010, 0(9): 71-73.
[12] 刘永生, 张金仓, 谷民安, 郁黎明, 杨晶晶, 高湉, 杨正龙, 彭麟. Fe基合金的微结构与频率特性[J]. 材料工程, 2010, 0(11): 39-42.
[13] 于治水, 李瑞峰. 镀锌钢板脉冲电弧钎焊接头界面组织及性能研究[J]. 材料工程, 2008, 0(9): 25-27,31.
[14] 高双胜, 刚铁, 黄宗仁. 铜钢堆焊接头超声弱信号缺陷的提取与量化[J]. 材料工程, 2008, 0(3): 54-57.
[15] 戴剑锋, 高建龙, 乔宪武, 王青, 李维学, 杜晓芳. CNTs定向排列的CNTs/PMMA电导率低突增效应研究[J]. 材料工程, 2008, 0(10): 1-4,9.
Viewed
Full text


Abstract

Cited

  Shared   
  Discussed   
版权所有 © 2015《材料工程》编辑部
地址:北京81信箱44分箱 邮政编码: 100095
电话:010-62496276 E-mail:matereng@biam.ac.cn
本系统由北京玛格泰克科技发展有限公司设计开发 技术支持:support@magtech.com.cn