全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...

基于堆焊成形钛合金高周疲劳实验数据的r-s-n模型

Keywords: 材料科学基础学科,应力比,疲劳寿命,疲劳极限,r-s-n数学模型

Full-Text   Cite this paper   Add to My Lib

Abstract:

?针对应力比对疲劳寿命影响的问题,以tc18钛合金堆焊成形(利用多层堆焊的方法制备)试样为研究对象,进行了3种应力比(r=0.5、r=0.06、r=-1)的疲劳实验,得出相应的疲劳极限,应用“应力幅值寿命模型”和“三参数寿命模型”得到6条s-n曲线。根据裂纹扩展速率与疲劳寿命的积分关系,以两种疲劳寿命数学模型为基础,系统地研究了应力比(r)与疲劳寿命曲线(s-n)的关系,提出了考虑应力比的疲劳寿命(r-s-n)数学模型。根据本文提出的修正公式,建立了适用tc18钛合金堆焊成形材料的两种r-s-n数学模型,结果表明:用应力幅值寿命模型可对中等疲劳寿命区进行准确的预测,而三参数寿命模型更适合中长寿命区域的预测。提出的两种r-s-n数学模型与实验值吻合良好,并可在工程上预测任意应力比下的疲劳寿命曲线。

References

[1]  guoyanjie,influenceofstressratioonfatiguebehaviorofhighstrengthsteel,worldmetals,2009-11-17(12),(2009)(郭廷杰,高强度钢应力比对疲劳性能影响,世界金属导报,2009-11-17(12),(2009))
[2]  caihuanxin,chenghao,sunjinxiu,influencingregularityofstressratioonfatiguestrengthof16mnsteelweldedjoints,shanxiarchitecture,33(25),102(2007)(蔡焕新,程浩,孙金秀,应力比对16mn钢焊接接头疲劳强度的影响规律,山西建筑,33(25),102(2007))
[3]  xushiwen,dongmansheng,huzongjun,niuzhongrong,fatiguetestresearchonsteel42crmo,journalofhefeiuniversityoftechnology,31(9),1506(2008)(许世文,董满生,胡宗军,牛忠荣,42crmo钢疲劳试验研究,合肥工业大学学报,31(9),1506(2008))
[4]  shaguiying,hanyu,liuteng,wangjie,lichaohua,influenceofstressratioonfatiguebehaviorofmg-3al-2scalloy,lightallowfabricationtechnology,40(9),61(2012)(沙桂英,韩玉,刘腾,王杰,李朝华,应力比对mg-3al-2sc合金疲劳行为的影响,轻合金加工技术,40(9),61(2012))
[5]  h.q.xue,h.tao,r.p.shao,b.claude,effectofstressratioonlonglifefatiguebehaviorofti-alalloyunderflexuralloading,transactionsofnonferrousmetalssocietyofchina,18(3),499(2008)
[6]  c.q.sun,z.q.lei,y.s.hong,effectsofstressratiooncrackgrowthrateandfatiguestrengthforhighcycleandvery-high-cyclefatigueofmetallicmaterials,mechanicsofmaterials,69(1),227(2014)
[7]  s.ishihara,a.j.mcevily,m.sato,k.taniguchi,t.goshima,theeffectofloadratioonfatiguelifeandcrackpropagationbehaviorofanextrudedmagnesiumalloy,internationaljournaloffatigue,31(11-12),(1788)2009
[8]  t.sakai,y.sato,y.nagano,m.takeda,n.oguma,effectofstressratioonlonglifefatiguebehaviorofhighcarbonchromiumbearingsteelunderaxialloading,internationaljournaloffatigue,28(11),1547(2006)
[9]  k.tokaji,effectofstressratioonfatiguebehaviorinsicparticulate-reinforcedaluminiumalloycomposite,departmentofmechanicalandsystemsengineering,28(6),539(2005)
[10]  xiongjunjiang,fatigueandfracturereliabilityengineering,firstedition,(beijing,nationaldefendindustypress,2008)p.60(熊俊江,疲劳断裂可靠性工程学,第一版,(北京,国防工业出版社,2008)p.60)
[11]  p.paris,f.a.erdogan,criticalanalysisofcrackgrowthlaws,journalofbasicengineering,85(3),(528)1963
[12]  wangkunqian,xurenping,linjiehui,fatiguecrackgrowthprobabilitymodelbasedonstressratio,journalofaerospacepower,24(9),2012(2009)(王坤茜,徐人平,林捷晖,考虑应力比的疲劳裂纹扩展概率模型,航空动力学报,24(9),2012(2009))
[13]  xurenoing,lishulan,wangkunqian,theeffectofstressratiop-da/dn-△kcurvefor30crmnsini2asteel,engineeringmechanice,22(2),6(2005)(徐人平,李淑兰,王坤茜,应力比对30crmnsini2a钢p-da/dn-△k曲线影响研究,工程力学,22(2),6(2005))
[14]  ouyanghui,liujunzhou,suxiaoyan,theeffectofstressratioonfatiguecrackgrowthrates,actamechanicasolidasinica,(4),577(1984)(欧阳辉,刘俊洲,苏小燕,应力比r对疲劳裂纹扩展速率的影响,固体力学学报,(4),577(1984))
[15]  gaozhengtong,xiongjunjian,fatiguereliability,1stedition,(beijing,beihanguniversitypress,2000)p.293

Full-Text

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133