时效热处理消减2A02铝合金淬火残余应力的微观机理Micro-mechanisms of quenching residual stress reduction for 2A02 aluminum alloy under aging treatment
王岩,彭桃,张麦仓
摘要(Abstract):
将2A02铝合金进行500℃/2 h固溶淬火处理后的不同温度及时间的时效热处理,结合压痕硬度法及透射电镜精细结构分析,研究2A02铝合金时效前后的组织和相演化及与残余应力变化的关联性。结果表明,170℃时效处理时,随着时效时间的延长,2A02铝合金表面淬火残余应力的消减效果越好,当时效时间达到16 h时,残余应力消减程度最为显著,可达原淬火残余应力的42.9%,而190℃时效热处理后淬火残余应力消减不明显。进一步的组织分析表明,170℃时效时,随着时效时间的延长,针状S'(Al2Cu Mg)相的数量增多且不断长大粗化,S'相产生的共格应力场与淬火残余应力叠加,达到消减淬火残余应力的目的;而190℃时效热处理后S'相的数量极少,使得样品表面淬火残余应力消减并不明显。
关键词(KeyWords): 时效热处理;淬火残余应力消减;2A02铝合金;S'(Al2Cu Mg)相
基金项目(Foundation):
作者(Author): 王岩,彭桃,张麦仓
DOI: 10.13289/j.issn.1009-6264.2015.06.014
参考文献(References):
- [1]李永春.2A02铝合金铸锭氧化膜缺陷生成原因及预防[J].轻合金加工技术,2005,33(7):20-22.LI Yong-chun.Reasons of causing alumina diaphragm defects in 2A02 aluminum alloy ingot and concerned preventive[J].Light Alloy Fabrication Technology,2005,33(7):20-22.
- [2]刘兵,彭超群,王日初,等.大飞机用铝合金的研究现状及展望[J].中国有色金属学报,2010,20(9):1705-1715.LIU Bing,PENG Chao-qun,WANG Ri-chu,et al.Recent development and prospects for giant plane aluminum alloys[J].The Chinese Journal of Nonferrous Metals,2010,20(9):1705-1715.
- [3]袁望姣,吴运新.基于预拉伸工艺的铝合金厚板残余应力消除机理[J].中南大学学报:自然科学版,2011,42(8):2304.YUAN Wang-jiao,WU Yun-xin.Mechanics about eliminating residual stress of aluminum alloy thicken-plates based on pre-stretching technology[J].Journal of Central South University:Science and Technology,2011,42(8):2304.
- [4]Cina B M.Reducing the susceptibility of the alloys,particularly aluminum alloy,to stress corrosion cracking:US.3856584[P].1974-12-24.
- [5]Islam M U,Wallace W.Retrogression and reaging response of 7475 aluminium alloy[J].Metals Technology,1983,10(1):386-392.
- [6]Brown M H.Improving strength and corrosion resistance of aluminum,zinc,magnesium and copper alloys by three step aging process,US:Patent Number US 4477292 A[P].1984-10-16.
- [7]Kersker M M,Liu J.Heat treatment of precipitation hardening alloys:US,5108520[P].1992-04-28.
- [8]Hall M B,Martin J W.The effect of retrogression temperture on the properties of an RRA(retrogressed and Re-aged)7150 aluminium alloy[J].Zeitschrift für Metallkunde,1994,85(2):134-139.
- [9]胡云卿,万海涛.残余应力消除方法研究[J].科技广场,2011(4):188-190.HU Yun-qing,WAN Hai-tao.Research on residual stress relief[J].Science Mosaic,2011(4):188-190.
- [10]聂波,王志超,刘显东,等.2A70铝合金预拉伸厚板热处理工艺研究[J].轻合金加工技术,2004,32(7):41-45.NIE Bo,WANG Zhi-chao,LIU Xian-dong,et al.Study of heat treatment process of 2A70 Aluminium Alloy pre-stretching plate[J].Light Alloy Fabrication Technology,2004,32(7):41-45.
- [11]冯春,刘志义,宁爱林,等.超高强铝合金RRA热处理工艺的研究进展[J].材料导报,2006,20(4):98-101.FENG Chun,LIU Zhi-yi,NING Ai-lin,et al.Research and progress in retrogression and reaging treatment of superhigh strength aluminum alloy[J].Materials Review,2006,20(4):98-101.
- [12]林高用,郑小燕,冯迪,等.铝合金厚板淬火残余应力的研究进展[J].材料导报,2008,22(6):70-74.LIN Gao-yong,ZHENG Xiao-yan,FENG Di.Research development of quenching-induced residual stress of aluminum thick plates[J].Materials Review,2008,22(6):70-74.
- [13]张园园,吴运新,李丽敏,等.7075铝合金预拉伸板淬火后残余应力的有限元模拟[J].热加工工艺,2008,37(14):88-91.ZHANG Yuan-yuan,WU Yun-xin,LI Li-min,et al.Finite element simulation of residual stress in pre-stretching thick-plates of 7075 Aluminum alloy after quenching[J].Hot Working Technology,2008,37(14):88-91.
- [14]Carlsson S,Larsson P.On the determination of residual stress and strain fields by sharp indentation testing.Part I:theoretical and numerical analysis[J].Acta Materialia,2001,49(12):2179-2191.
- [15]Carlsson S,Larsson P.On the determination of residual stress and strain fields by sharp indentation testing.Part II:experimental investigation[J].Acta Materialia,2001,49(12):2193-2203.
- [16]Larsson P.Investigation of sharp contact at rigid-plastic conditions[J].International Journal of Mechanical Sciences,2001,43(4):895-920.
- [17]Larsson P.On the mechanical behavior at sharp indentation of materials with compressive residual stresses[J].Materials&Design,2011,32(3):1427-1434.
- [18]Larsson P,Blanchard P.On the correlation between residual stresses and global indentation quantities:Numerical results for general biaxial stress fields[J].Materials&Design,2012,37:435-442.
- [19]王顺才,李春志.2024高强铝合金中等弥散相Al20Cu2Mn3结构的确定[J].机械工程学报,1990,26(4):16-19.WANG Shun-cai,LI Chun-zhi.The microstructure determination of the dispersed phases in 2024 aluminum alloys[J].Chinese Journal of Mechanical Engineering,1990,26(4):16-19.
- [20]CHEN Y Q,Yi D Q,Jiang Y,et al.Twinning and orientation relationships of T-phase precipitates in an Al matrix[J].Journal of Materials Science,2013,48(8):3225-3231.
- [21]王顺才,李春志.Al-Cu-Mg合金中时效相S'的二次衍射效应研究[J].航空材料学报,1993,13(3):41-48.WANG Shun-cai,LI Chun-zhi.Study on double diffractions of S'precipitate phase in Al-Cu-Mg alloy[J].J Aeron Mater,1993,13(3):41-48.
- [22]Silcock J M.The structural ageing characteristics of Al-Cu-Mg alloys with copper-magnesium weight ratios of 7-1 and 2.2-1[J].Journal of the Institute of Metals,1961,89(6):203-210.
- [23]Bagaryatsky Y.Charateristics of natural aging of aluminum alloy[J].Dokl Akad SSSR,1952,87(3):559-568.
- [24]Perlitz H,Westgren A.The crystal structure of Al2Cu Mg[J].Arkiv Kemi Mineral Geol B,1943,16(13):1-5.
- [25]米谷茂,朱荆璞,邵会孟.残余应力的产生和对策[M].北京:机械工业出版社,1983.
- [26]张定铨.X射线应力测定基本知识第一讲:残余应力的基本概念[J].理化检验:物理分册,2007,43(4):211-213.ZHANG Ding-quan.Basic knowledge of stress determination by X-ray——lecture No.1 basic concept of residual stress[J].Physical Testing and Chemical Analysis:Part A:Physical Testing,2007,43(4):211-213.
文章评论(Comment):
|
||||||||||||||||||
|
||||||||||||||||||