OALib Journal期刊
ISSN: 2333-9721
费用:99美元
|
|
|
2a12铝合金疲劳裂纹的成核与扩展机理
Keywords: 金属材料,铝合金,疲劳,裂纹成核,裂纹扩展,微观结构
Abstract:
?进行了不同应力水平下和不同应力比下2a12铝合金试验件的疲劳试验,并对试验件疲劳断口显微结构进行分析和对比,以揭示疲劳裂纹成核与扩展的微观特征。结果表明:2a12铝合金的疲劳裂纹在靠近试验件表面较为粗大的第二相粒子或试验件棱角缺陷处成核;成核位置距试验件表面的距离与应力水平和应力比有关,疲劳裂纹扩展区域也与应力水平和应力比有关。应力水平较小或应力较大时,疲劳裂纹沿晶扩展和穿晶扩展尤为明显。疲劳断口的裂纹成核粒子越小(大),试验件疲劳寿命越短(长),微裂纹成核寿命是疲劳全寿命计算中不可忽视的部分。
References
[1] | (胡仁伟,刘文珽,结构原始疲劳质量分布方法的改进,北京航空航天大学学报,1,41(1999))
|
[2] | 8bianguixue,chenyueliang,yudazhao,studyoninitialdiscontinuitystateofly12aluminiumalloy,structure&environmentengineering,34(5),58(2007)
|
[3] | (卞贵学,陈跃良,郁大照,ly12铝合金初始不连续状态研究,强度与环境,34(5),58(2007))
|
[4] | 9bianguixue,chenyueliang,zhangdanfeng,studyonfatiguelifeofpre–corrodedaluminiumalloybasedonids,actaaeronauticaetastronauticasinica,29(6),1526(2008)
|
[5] | 11zhongqunpeng,zhaozihua,fractography(beijing,higheducationpress,2006)p.6
|
[6] | (钟群鹏,赵子华,断口学(北京,高等教育出版社,2006)p.6)
|
[7] | (赫尔(derekhull),李晓刚,董超芳,杜翠薇译,断口形貌学:观察、测量和分析断口形貌学的科学(北京,科学出版社,2009)p.9)
|
[8] | (蹇海根,姜锋,文康,黄宏锋,韦莉莉,蒋龙,不同应力下7b04铝合金的疲劳断口,中南大学学报(自然科学版),41(1),132(2010))
|
[9] | 15caochangnian,wangzhizhi,zhaoxuanmin,evaluationandcoincidencecheckforinitialfatiguequalityoffastenerhole,journalofnorthwesternpolytechnicaluniversity,1,15(2000)
|
[10] | (曹昌年,王志智,赵选民,紧固孔原始疲劳质量评定及符合性检查,西北工业大学学报,1,15(2000))
|
[11] | 16hurenwei,liuwenting,advancedmethodofdurabilityanalysis,journalofbeijinguniversityofaeronauticsandastronautics,1,41(1999)
|
[12] | 1m.liao,g.renaud,probabilisticmodelingofshortcrackgrowthinairframealuminumalloys,aircraft,45,1105(2008)
|
[13] | 2lynneugeneoswald,effectsmicrostructureonhigh–cyclefatigueofanal–zn–mg–cualloy(al–7055),msdegree(pittsburgh,universityofpittsburgh,2003)p.
|
[14] | 3alimerati,graemeeastaugh,determinationoffatiguerelateddiscontinuitystateof7000seriesofaerospacealuminumalloys,engineeringfailureanalysis,14,673(2007)
|
[15] | 4alimerati,astudyofnucleationandfatiguebehaviorofanaerospacealuminumalloy2024–t3,internationaljournaloffatigue,27,33(2005)
|
[16] | 5minliao,probabilisticmodelingoffatiguerelatedmicrostructuralparametersinaluminumalloys,engineeringfailuremechanics,76,668(2009)
|
[17] | 6litang,wangqingyuan,themicrostructureandfatigueinitiationofanaa2524–t34aluminumalloy,journalofsouthwestuniversityofscienceandtechnology,24(3),23(2009)
|
[18] | (李棠,王清远,aa2524--t34铝合金的微观结构与疲劳裂纹萌生机制,西南科技大学学报,24(3),23(2009))
|
[19] | 7wangxishu,tangbin,taosha,in–situobservationtechnologyandapplicationoffatiguecrackinitiationandpropagationforcastmagnesiumalloys,materialsformechanicalengineering,30(2),1(2006)
|
[20] | (王习术,汤彬,陶沙,铸造镁铝合金的微观破坏机理原位观测技术与应用,机械工程材料,30(2),1(2006))
|
[21] | (卞贵学,陈跃良,张丹峰,基于ids的铝合金预腐蚀疲劳寿命研究,航空学报,29(6),1526(2008))
|
[22] | 10zhongqunpeng,zhaozihua,zhangzheng,developmentof“fractography”andresearchoffracturemicromechanism,journalofmechanicalstrength,27(3),358(2005)
|
[23] | (钟群鹏,赵子华,张峥,断口学的发展及微观断裂机理研究,机械强度,27(3),358(2005))
|
[24] | 12derekhull,translatedbylixiaogang,dongchaofang,ducuiwei,fractography:observingmeasuringandinterpretingfracturesurfacetopography(beijing,sciencepress,2009)p.9
|
[25] | 13jianhaigen,jiangfeng,wenkang,huanghongfeng,weilili,jianglong,fatiguefractureof7b04aluminumalloyunderdifferentstresses,journalofcentralsouthuniversity(scienceandtechnology),24(3),23(2009)
|
[26] | 14jianhaigen,jiangfeng,zhengxiuyuan,studyonfatiguefractographyofhighstrengthandtoughnessaluminumalloyforaviation,journalofaeronauticalmaterials,30(4),97(2010)
|
[27] | (蹇海根,姜锋,郑秀媛,航空用高强高韧铝合金疲劳断口特征的研究,航空材料学报,30(4),97(2010))
|
Full-Text
|
|
Contact Us
service@oalib.com QQ:3279437679 
WhatsApp +8615387084133
|
|