期刊文献+

30CrMnSiNi2A超高强度钢孔挤压强化残余应力场的模拟 被引量:6

Finite Element Simulation of the Residual Stress Fields of 30CrMnSiNi2A Ultrahigh Strength Steel by Hole Cold Expansion
原文传递
导出
摘要 利用有限元软件ANSYS建立了30CrMnSiNi2A超高强度钢孔挤压强化残余应力场的三维有限元模型,分别模拟分析了不同孔径、过盈量、厚度和孔边距比下30CrMnSiNi2A超高强度钢构件孔挤压强化的三维残余应力场分布.模拟结果表明,残余应力沿厚度在中层和出口处随着孔径的增大而增大,且残余拉应力的增加幅度也大;随着过盈量的增大,残余压应力增大,但达到一定程度后过盈量的增量所引起的有利残余压应力的增量减小;随着厚度的增加,残余压应力在入口表面的孔周处先减小后增大;孔边距的减小,对残余压应力影响较小,而对残余拉应力的影响很大. The residual stress fields of 30CrMnSiNi2A ultrahigh strength steel with different hole diameter, magnitude of interference, thickness and edge distance ratio (EDR) caused by hole cold expansion were simulated by FEM using ANSYS codes. The results show that the residual stresses in the middle location and the exit surfaces increase with the size of hole diameter along the depth, and the residual tensile stresses increase more than the residual compressive stresses. The residual compressive stresses increase with the magnitude of interference significantly and then became increase slowly; with the increase of the thickness, the residual compressive stresses on the surface of the entrance decrease firstly and then increase. The decrease of the EDR has a greater influence on the residual tensile stresses than the residual compressive stresses.
出处 《力学季刊》 CSCD 北大核心 2014年第2期243-252,共10页 Chinese Quarterly of Mechanics
基金 国家自然科学基金(11372226) 国家重点基础研究发展计划(2010CB833105) 同济大学英才计划(1330219133) 中央高校基本业务费专项资金 国家冷轧板带装备及工艺工程技术研究中心开放课题(NECSR-201306)
关键词 30CrMnSiNi2A超高强度钢 孔挤压强化 残余应力场 有限元模拟 30CrMnSiNi2A ultrahigh strength steel hole cold expansion residual stress fields finite element simulation
  • 相关文献

参考文献16

  • 1李成功.航空航天材料[M].北京:国防工业出版社,1999..
  • 2王智,李京珊.影响冷挤压强化效果的因素[J].机械强度,2002,24(2):302-304. 被引量:15
  • 3LIU J, SHAO X J, LIU Y S, et al. Effect of cold expansion on fatigue performance of open holes[J]. Mater Sci Eng A, 2009, 477:271-6.
  • 4DE MATOS P F P, MOREIRA P M G P, CAMANHO P P, et al. Numerical simulation of cold working of rivet holes[J]. Finite Elem Anal Des, 2005, 41:989-1007.
  • 5BABU N C M, JAGADISH T, RAMACHANDRA K, et al. A simplified 3D finite element simulation of cold expansion of a circular hole to capture through thickness variation of residual stresses[J]. Eng Fail Anal, 2008, 15:339-48.
  • 6张永伟,杨庆雄.钉孔挤压强化三维弹塑性有限元分析[J].西北工业大学学报,1993,11(1):96-101. 被引量:4
  • 7刘晓龙,高玉魁,刘蕴韬,陈东风.孔挤压强化残余应力场的三维有限元模拟和实验研究[J].航空材料学报,2011,31(2):24-27. 被引量:24
  • 8AL-ATHEL K S, GADALA M S. Eulerian volume of solid (VOS) approach in solid mechanics and metal forming[J]. Comput Methods Appl Mech Eng, 2011, 200:2145-59.
  • 9MAXIMOV J T, DUNCHEVA G V. A new 3D finite element model of the spherical mandrelling process[J]. Finite Elem Anal Des, 2008, 44:372-382.
  • 10JANG J, CHO M, YANG W. The finite element analysis of the mandrel shape's influence on the residual stress distribution by cold expansion method[J]. J Korean Soc Precis Eng, 2006, 23:127-133.

二级参考文献44

  • 1中国航空科学技术研究院.飞机结构抗疲劳断裂强化设计手册[M].北京:航空工业出版社,1993.
  • 2[1]Buxbaum O,Huth H.Expansion of cracked fastener holes as a measure for extension of lifetime to repair.Engng Fracture Mechanics,1987,28:689~698.
  • 3[2]Wanger R V,Reid L,Easterbrook E T,Rufin A C.Beneficial effects of split sleeve cold expansion TM on the fatigue lives of pre-cycled cold expandedstructure.In 1992 USAF Aircraft Structural Integrity Program Conference,San Antonio,Texas,1~3 December 1992.
  • 4[3]Pell P A,Beaver P W,Mann J Y,Sparrow J G.Fatigue of thick-section cold-expanded holes with and without cracks.Fatigue Fract.Engng.Mater.Struct.,1989,12(6) :761~775.
  • 5[4]Reid L.Airframe life extension through cold expansion techniques.Interna tional Conference on Aircraft Damage Assessment and Repair.Melbourne 26 ~28,August,1991.
  • 6[5]Gaerke J,Zhang X,Wang Z.Life enhancement of fatigue aged fastener holes using cold expansion process.J.of Aerospace Engineering,Proc Instn Mech Eng,,Parl G,2000,214:281~293.
  • 7[6]Bernard M,Bai-Quoc T,Burlat M.Effect of re-coldworking on fatigue life enhancement of a fastener hole.Fatigue Fract.Engng.Mater.Struct.,1995,18(7/8):761~775.
  • 8[7]Phillips J L.Sleeve cold working fastener holes.Air Force Materials Labo ratory,Wright-Patterson AFB OH,1974.
  • 9[8]Len Reid.Split sleeve cold expansion as a rework process for previously cold expanded holes.ICAF'93,International Committee on Aeronautical Fatigue,Stockholm,Sweden,June,1993.
  • 10[9]Ball D L,Lonry D R.Experimental investigation on the effects of cold expap.sion of fastener holes.Fatigue Fract.Engng.Mater.Struct.,1998,21:17~34.

共引文献58

同被引文献69

引证文献6

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