期刊文献+

表面疲劳裂纹扩展的三维效应 被引量:3

THREE-DIMENSIONAL EFFECT OF SURFACE FATIGUE CRACK PROPAGATION
下载PDF
导出
摘要 以拉伸圆杆为例 ,阐述表面疲劳裂纹扩展中的三维效应及其特点。利用最新的三维断裂力学成果给出一种考虑表面疲劳裂纹扩展三维效应的具体方法 ,通过该方法可以得到考虑三维应力状态的材料da dN—ΔKeff曲线。以2 0CrMo钢为例 ,处理获得 2 0CrMo材料的da dN—ΔKeff基线 ,以此对圆杆表面疲劳裂纹的扩展进行预测分析。分析结果表明 ,使用该方法以及来自标准穿透裂纹试件的材料da dN—ΔK数据可准确地预测圆杆表面疲劳裂纹的扩展寿命。该方法还可用于其他复杂结构的疲劳裂纹扩展分析。 With tensile round rob as a typical instance, the three-dimensional geometry effects and its characteristics of surface fatigue crack propagation are discussed and investigated. Using the latest achievement of three-dimensional fracture mechanics, a new practical method, which can also be used to obtain the geometry independent material base curve of d a /d N -Δ K _ eff ,is developed to eliminate the three-dimensional effects on fatigue crack growth. As a example, 20CrMo steel base curve of d a /d N -Δ K _ eff is obtained and fatigue crack propagation life of 20CrMo steel bar with elliptic surface crack is predicated in the paper. It is demonstrated that the three-dimensional geometry effects of surface fatigue crack growth can been eliminated greatly by use of the method, and surface crack propagation life in 20CrMo steel bar can be predicted accurately by use of the method in addition to fatigue crack growth data from standard through-thickness cracked specimens. The three-dimensional method can also be used to other complicated structures.
出处 《机械强度》 CAS CSCD 北大核心 2003年第2期200-203,221,共5页 Journal of Mechanical Strength
基金 国家自然科学基金 (50 2 750 3) 航空科学基金 (0 1 852 0 1 2 )资助项目~~
关键词 表面疲劳裂纹扩展 三维效应 疲劳寿命预测 三维约束理论 Surface crack Fatigue life prediction Geometrical effect Three-dimension constraint theory
  • 相关文献

参考文献19

  • 1Broek D. The influence of sheet thickness on crack propagation. Aircraft Engng, 1966,38:31~33.
  • 2郭万林.航空结构损伤容限设计中的三维问题[J].航空学报,1995,16(2):129-136. 被引量:17
  • 3Budiansky B, Hutchinson J W. Analysis of closure in fatigue crack growth.J. Appl. Mech., 1978, 45:267~276.
  • 4Newman J C Jr. Effects of constraint on crack growth under aircraft spectrum loading. Fatigue of Aircraft Materials. In: Edit by Beukers A, Proc. of the Specialists' Conf. Dedicated to the 65th birthday ofJ Schijve, Delft: Delft University Press, 1992. 83 ~ 109.
  • 5徐小兵,袁祥忠.表面有横向裂纹的抽油杆寿命估算[J].石油机械,1993,21(5):28-33. 被引量:4
  • 6徐克明,钟伯明,魏嘉荃,陈抡元.拉伸圆杆表面裂纹应力强度因子实验研究[J].大庆石油学院学报,1991,15(2):65-70. 被引量:4
  • 7李中华,陈黄浦,骆竞晞.抽油杆表面椭圆裂纹应力强度因子有限元分析[J].石油机械,1994,22(12):20-24. 被引量:6
  • 8王国丽,魏嘉荃,钟伯明,秦洪.抽油杆材料疲劳裂纹扩展规律的概率研究[J].大庆石油学院学报,1993,17(1):78-83. 被引量:4
  • 9HUANG Shuju, AN Renjie. Discuss on fatigue crack growth rate of bended round bar. In: Edited by Metallurgy Academy of China, Proc. of the FirstMetal Fatigue Science Conference of China. Lanzhou: the First Metal Fatigue Science Conference of China. Beijing: Press of Metallurgy Industry,1984(In Chinese)(黄淑菊,安仁杰.对旋转弯曲圆试样中疲劳裂纹发展速率的初步探讨.中国金属学会第一届金属疲劳学术会议论文集.中国金属学会编,兰州,中国金属学会第一届金属疲劳学术会议论,北京:冶金工业出版社.1984).
  • 10GUO W. Three-dimensional analyses of plastic constraint for throughthickness cracked bodies. Engineering Fracture Mechanics, 1999, 62:383~407.

二级参考文献34

  • 1陈黄浦,骆竞,唐锴.抽油杆表面缺陷及裂纹分析[J].石油机械,1994,22(7):20-24. 被引量:7
  • 2郭万林.航空结构损伤容限设计中的三维问题[J].航空学报,1995,16(2):129-136. 被引量:17
  • 3傅祥炯.随即载荷谱裂纹扩展寿命模型[M].西安:西北工业大学出版社,1989..
  • 4张诗捷 朱亦钢.与塑性相关的因素对疲劳裂纹扩展的影响[J].固体力学学报,1995,(6):59-65.
  • 5郭万林,第五届全国疲劳学术会议论文集,1991年
  • 6郭万林,西北工业大学学报,1991年,9期,411页
  • 7郭万林,博士学位论文,1991年
  • 8Chen X,Eng Fract Mech,1990年,35卷,997页
  • 9Sih G C,Theoret Appl Fract Mech,1989年,12卷,1页
  • 10匿名著者,飞机结构耐久性及损伤容限设计手册.JNS分册,1989年

共引文献30

同被引文献40

引证文献3

二级引证文献23

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部