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A-100钢开缝衬套孔挤压强化残余应力场 被引量:13

Residual Stress Induced by Cold Expansion With Sleeve Process of A-100 Steel
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摘要 为研究A-100钢开缝衬套挤压工艺,提高孔的抗疲劳性能,使用X射线衍射方法和中间开孔的板状试样,研究开缝衬套挤压过盈量、挤后铰削量和保温温度对残余压应力场的影响。研究表明,由于孔受挤压发生弹塑性变形而引入切向残余压应力(σh),σh值随开缝衬套挤压过盈量(Ice)增加而显著增大,当Ice为0.4mm时,σh值可达-500 MPa以上。未铰削的挤压试样,孔边缘残余压应力最大,可达到-680MPa,随着铰削量(R)的增大,σh降低,而当绞削量达到0.7mm时,σh仅剩余28%。保温10h后,各点σh值均明显降低,350℃下孔边缘σh仅存14%。 In order to investigate cold expansion with sleeve process(CESP) of A-100 steel and improve the fatigue property of hole,the sample with a hole was prepared,on which the residual stress inducing by CESP was studied by XRD.The influence of interference value of CESP,the amount of material removal and holding temperature on the distribution of residual stress was studied.The results showed that,as the mandrel with sleeve removed from the hole,surrounding of hole generated elastically and plastically deformation,this resulted in a zone around the hole containing residual compressive hoop stress(σh).With the increasing of interference value(Ice) of CESP,σh became higher observably.When Ice reach 0.4 mm,σhcould reach more than-500 MPa.It had the highest σh on the edge of hole without material removal,the value was-680 MPa.In contrast,σh could remain only 28% when the amount of material removal was 0.7 mm.σh would have a significant reduction after both 200 ℃ and 350 ℃ holding for 10 hours.When the temperature was 350 ℃,σh could remain only 14%.
出处 《中国表面工程》 EI CAS CSCD 北大核心 2011年第5期64-67,共4页 China Surface Engineering
关键词 开缝衬套挤压 残余应力 过盈量 应力松弛 CESP residual stress interference value relaxing of stress
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参考文献6

  • 1米谷茂.残余应力的产生和对策[M].北京:机械工业出版社,1983..
  • 2Chakherlou N, Vogwell L, A novel method of cold expansion which creates near-uniform compressive tangential residual stress around a fastener hole[J]. Fatigue and Fracture of Engineering Materials , 2004,27(5), 343-351.
  • 3Rufin A C. Extending the fatigue life of aircraft en- gine components by hole cold expansion technology [J]. Journal of Engineering for Gas Turbines and Power, 1993 ,115(1):7-15.
  • 4O'Brien E W. Beneficial residual stress from the cold expansion of large holes in thick light alloy plate. The Journal of Strain Analysis for Engineer- ing Design, 2000, 35(4):261-276.
  • 5高玉魁.孔挤压强化对23Co14Ni12Cr3MoE钢疲劳性能的影响[J].金属热处理,2007,32(11):34-36. 被引量:21
  • 6高玉魁.TC18超高强度钛合金喷丸残余压应力场的研究[J].稀有金属材料与工程,2004,33(11):1209-1212. 被引量:48

二级参考文献11

  • 1FTI Process Specification-8101D (USA).Cold Expansion of Holes Using the Standard Split Sleeve System and Countersink Cold ExpansionTM (CsCxTM)[S].
  • 2Abel Osagie Obabueki.A new unified phenomenological model for fatigue crack initiation,short crack propagation,long crack propagation and closure effects[D].Palo Alto,California,USA:Stanford University.1987:2-8.
  • 3Juijerm P,Altenberger I,Scholtes B.Fatigue and residual stress relaxation of deep rolled differently aged aluminium alloy AA6110[J].Materials Science and Engineering A,2006,426(1~2):4-10.
  • 4Guagliano M,Vergani L.An approach for prediction of fatigue strength of shot peened components[J].Engineering Fracture Mechanics,2004,71(4):501-512.
  • 5King A,Steuwer A,Woodward C,Withers P J.Effects of fatigue and fretting on residual stress introduced by laser shock peening[J].Materials Science and Engineering A,2006,435~436(11):12-18.
  • 6Gao Yu-kui,Li Xiang-bin,Yang Qing-xiang and Yao Mei.Influence of surface integrity on fatigue strength of 40CrNi2Si2MoVA steel[J].Materials Letters,2007,61 (2):466-469.
  • 7Suresh S.Fatigue of Materials[M].Cambridge,UK:Cambridge University Press,1998:10-35.
  • 8Jean-Claude E Stranart.Mechanically induced residual stresses:modeling and characterization[D].Toronto,Canada:University of Toronto,2000:1-18.
  • 9高玉魁,姚枚,邵培革,王仁智.金属疲劳极限与静强度的相关性[J].机械强度,2001,23(1):15-18. 被引量:21
  • 10高玉魁,殷源发,李向斌,赵宇新.GH909合金喷丸强化残余应力场的研究[J].材料工程,2002,30(4):40-42. 被引量:18

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