期刊文献+

钉孔挤压强化三维弹塑性有限元分析 被引量:4

On Three-Dimensional Finite Element Analysis of Coldworked Fastener Hole Using Flow Theory
下载PDF
导出
摘要 采用三维增量弹塑性有限元方法对钉孔挤压强化过程进行了模拟计算,给出了残余应力、应变及位移的分布.计算结果表明,应力、应变沿厚度的分布具有不均匀性,并可用来说明挤压强化钉孔的疲劳源的可能位置等情况. Shao et al[1] analyzed the conditions under which fatigue crack source of coldworked fastener hole did not occur on the edge of the hole but occurred in the sheet material close to the edge. But the 2-dimensional deformation theory used by Shao to obtain residual stresses neglected the variation of residual stresses across the thickness of the sheet. Only 3-D theory can reflect such variation of residual stresses. Besides, the theoretical analysis of Zhang et al[7] showed that flow theory was better than deformation theory in the computation of residual stresses of coldworked fastener hole. Therefore the authors in this paper use 3-D flow theory to calculate residual stresses of coldworked fastener hole. The authors propose the 'Coldworking Displacement Compatible Method' for iterative calculations. From the calculations, the following conclusions can be drawn: 1. When D_m is the diameter of mandrel. D_k is the diameter of hole, and coldworking amount δ=(D_m-D_h)/ D_k is larger than 0.02 (δ for coldworked fastener hole is usually Jarger than 0.02) then flow theory needs to be used. 2. When sheet thickness h is equal or greater than 6 mm, then both circumferential residual stress σ_(θr) and radial residual stress σ_ vary conspicuously across sheet thickness. When δ=0.0342 and h=6mm,σ_(θrmax)/σ_(θrmin)≈1.5. Evidently, 3-D model instead of 2-D one should be used when h>6 mm. 3. The non-uniformity of residual stresses σ_(θr) and σ_(rr) can explain quantitively why the fatigue crack source occurs in the sheet material close to the edge.
机构地区 西北工业大学
出处 《西北工业大学学报》 EI CAS CSCD 北大核心 1993年第1期96-101,共6页 Journal of Northwestern Polytechnical University
基金 航空科学基金资助课题
关键词 钉孔 残余应力 有限元 挤压强化 coldworked hole residual stress 3-dimensional model flow theory
  • 相关文献

参考文献4

二级参考文献2

同被引文献56

  • 1杨洪源,刘文珽.孔挤压强化疲劳增寿效益的试验研究[J].机械强度,2010,32(3):446-450. 被引量:14
  • 2罗治平,宋德玉,杨玉荣,张少卿.GH169合金孔内表面层的挤压强化对孔边疲劳性能的影响[J].材料工程,1994,22(8):24-25. 被引量:1
  • 3宋德玉,罗治平,杨玉荣,张少卿.GH169高温合金孔挤压强化层的微观结构[J].航空学报,1996,17(1):125-128. 被引量:9
  • 4李成功.航空航天材料[M].北京:国防工业出版社,1999..
  • 5Lai M O, Siew Y H. Fatigue properties of cold worked holes. Journal of Material Processing Technology, 1995 ;48:533---40.
  • 6Maximov J T, Kuzmanov T V, Anch A P, et al. A finite element simulation of the spherical mandrelling process of holes with cracks. Journal of Materials processing Technology, 2006; 2, 171 ( 3 ) : 459--466.
  • 7Chakherlou T N, Vogwell Jdian. The effect of cold expansion on improving the fatigue life of fastener holes. Eng Failure Anal 2003; 13:24.
  • 8Chandawannich N, Sharpe Jr W N. An experimental study of fatigue crack initiation and growth from cold worked holes. Engineering Fracture Mechanics, 1979 ; 1 ( 1 ) :609--20.
  • 9Link R E, Sanford R J. Residual strains surrounding split-sleeve cold expanded holes in 7075-T651 Aluminum. J Aircraft, 1990;27 (7): 599--604.
  • 10Nigrelli V, Pasta S. Finite-element simulation of residual stress induced by spilt-sleeve cold-expansion process of holes. Journal of Materials processing Technology,2008 ;205:290--296.

引证文献4

二级引证文献26

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