论文:2013,Vol:31,Issue(1):98-102
引用本文:
马玉娥, 刘宝琪, 赵振强. 铝锂合金2198-T8机身整体搅拌摩擦焊接壁板的疲劳性能研究[J]. 西北工业大学
Ma Yu'e, Liu Baoqi, Zhao Zhenqiang. Fatigue Properties of Al-Li 2198-T8 Friction Stir Welded Integral Panel[J]. Northwestern polytechnical university

铝锂合金2198-T8机身整体搅拌摩擦焊接壁板的疲劳性能研究
马玉娥, 刘宝琪, 赵振强
西北工业大学 航空学院, 陕西 西安 710072
摘要:
采用铝锂合金2198-T8,对未来搅拌摩擦焊接机身整体壁板的结构形式进行了设计,并把机身整体焊接壁板的结构形式简化为2种典型试验构型。采用中子衍射方法测得铝锂合金2198-T8单焊缝和双焊缝板的残余应力分布,并对2种试验件的残余应力分布进行了研究;对2198-T8母材和2种典型焊接试验件进行疲劳试验,测得不同尺寸的试验件裂纹扩展速率,并进行对比分析。采用ABAQUS软件建立了有限元数值计算模型,计算出2种情况下由残余应力引起的应力强度因子(Kresidual),研究了残余应力对于疲劳各参数的影响,采用Newman闭合模型计算出2种模型的疲劳寿命,并和试验寿命相对比。试验和数值结果表明:双焊缝试件的疲劳寿命比单焊缝试件长4倍;残余应力的存在改变了疲劳参数分布。
关键词:    铝锂合金    搅拌摩擦焊接    残余应力    疲劳性能   
Fatigue Properties of Al-Li 2198-T8 Friction Stir Welded Integral Panel
Ma Yu'e, Liu Baoqi, Zhao Zhenqiang
College of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China
Abstract:
Al-Li alloy 2198-T8 was chosen to be used.The friction stir welded integral panel for fuselage applica-tion was designed and simplified into two typical testing samples.Residual stress profiles in single weld sample anddouble weld sample were respectively measured by neutron diffraction method.The distribution of residual stresswas analyzed.Fatigue tests of two samples and parent material were performed and crack growth rates were meas-ured and compared.In order to study the effect of residual stress, the finite element model was built and K residual ofeach type was calculated.K residual effects on fatigue parameters were analyzed, and Newman closure model was usedto calculate fatigue lives, which were compared with the experimental lives.It was shown that: the fatigue life ofdouble weld sample is four times than that of single weld sample; residual stresses changed the distributions of fa-tigue property parameters with crack growing.
Key words:    aluminium alloys    fatigue crack propagation    friction stir welding    fuselages    residual stresses    stressconcentration   
收稿日期: 2012-04-08     修回日期:
DOI:
基金项目: 西北工业大学基础研究基金(JC201021);西北工业大学新人新方向重点项目;国家青年自然科学基金(11002111)资助
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作者简介: 马玉娥(1975-),女,西北工业大学副教授,主要从事结构强度、复合材料结构和热结构研究。
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参考文献:
[1] Dwight Burford,Christian Widener,Bryan Tweedy.Advances in Friction Stir Welding for Aerospace Applications.AIAA-2006-7730
[2] Brijesh Kumar,et al.Review of the Applicability of FSW Processing to Aircraft Applications.AIAA-2005-2000
[3] Ronald Krueger.The Virtual Crack Closure Technique (VCCT): History,Approach and Applications.NASA/CR-2002-211628
[4] accessed 02042009
[5] American Society for Testing and Materials.E647,2005
[6] Staron P,Kocak M,Williams S,Wescott A.Residual Stress in Friction Stir-Welded Al Sheets.Physics B 350,2004,491-493
[7] Ma Yu E,Staron P,Fisher T,Irving P E.Size Effects on Residual Stress and Fatigue Crack Growth in Friction Stir Welded2195 T8 Aluminium Part II: Modelling.International Journal of Fatigue,2011,33(11): 1426-1434
[8] Newman J C.Fratran-II-A Fatigue Crack Growth Structural Analysis Program.NASA Technical Memorandum 104159,1992