研究了不同热处理工艺下7A55铝合金淬火预拉伸(W51)板材的力学性能、腐蚀性能、电导率变化以及相应的微观组织特点.用正交实验分析双级时效工艺,结果表明7A55铝合金双级时效的四因素中第二级时效温度和时间是影响最终性能的主要因素.淬火预拉伸7A55合金板材最佳双级时效热处理工艺分别为:T7651:121℃×5h+170℃×6h,T7451:121℃×5h+160`C×14h.电镜观察结果表明,T7451,T7651时效时晶内析出半共格的η'相和η相,并有不同程度粗化,晶界为断续分布的粗大η平衡相.这种微观结构能有效的提高7A55合金板材的电导率和腐蚀性能,同时使合金具有较高强度.
参考文献
[1] | Chih-Kuang Lin;Sheng-Tseng Yang .Corrosion fatigue behavior of 7050 aluminum alloys in different tempers[J].Engineering Fracture Mechanics,1998(6):779-795. |
[2] | 王洪斌;黄进峰;杨滨 等.AI-Zn-Mg-Cu系合超高强合金的研究现状与发展趋势[J].材料导报,2003,17(09):1-4. |
[3] | Lucasah D A;Hart R M .Aluminum alloy development efforts for compression dominated structure of aircraft[J].Light Metals Age,1991,2(09):11-15. |
[4] | 吴一雷.超高强度铝合金的发展与应用[J].航空材料学报,1994(01):49. |
[5] | Wilson Boulevard;Arlington .International alloy designations and chemical composition limits for wrought aluminum and wrought aluminum alloys[J].Aluminum Association,2006,222(09):11-14. |
[6] | ASTM G34-2001.ASTM G34-2001.Standard test method for exfoliation corrosion susceptibility in 2000 and 7000 series aluminum alloys[S].United States,2001. |
[7] | AMS 2772E.AMS 2772E.Heat treatment of aluminum alloy,materials[S].United States,2008. |
[8] | AMS 4324.AMS 4324.Aluminum alloy,extruded rod bar and profiles(7055-174511)8.Ozn-3Cu-2.OMg-0.16Zr solution heat treated stress-relieved and overaged[S].United States,2002. |
[9] | AMS 4336A.AMS 4336A.Aluminum alloy extruded rod bar,and profiles(7055-176511)8.Ozn-2.3 Cu-OMg-0.16Zr solution heat treated,stress-relieved,and overaged[S].United States,2003. |
[10] | Alloy 7055-174511 and 7055-176511.Alloy 7055-174511 and 7055-176511 extrusions:United States,Alcoa products[S].,2008. |
[11] | YUAN Zhi-shan,LU Zheng,XIE You-hua,DAI Sheng-long,LIU Chang-sheng.Effects of RRA Treatments on Microstructures and Properties of a New High-strength Aluminum-Lithium Alloy-2A97[J].中国航空学报(英文版),2007(02):187-192. |
[12] | X. Z. LI;V. HANSFN .HREM STUDY AND STRUCTURE MODELING OF THF ?' PHASE, THE HARDENING PRECIPITATES IN COMMERCIAL Al-Zn-Mg ALLOYS[J].Acta materialia,1999(9):2651-2659. |
[13] | 褚武扬.应力腐蚀机理研究的新进展[J].腐蚀科学与防护技术,1995(02):97. |
[14] | P. GUYOT;L. COTTIGNIES .PRECIPITATION KINETICS, MECHANICAL STRENGTH AND ELECTRICAL CONDUCTIVITY OF AlZnMgCu ALLOYS[J].Acta materialia,1996(10):4161-4167. |
[15] | 冯春,刘志义,宁爱林,曾苏民.RRA处理对超高强铝合金抗应力腐蚀性能的影响[J].中南大学学报(自然科学版),2006(06):1054-1059. |
[16] | M.J. STARINK;X.M. LI .A Model for the Electrical Conductivity of Peak-Aged and Overaged Al-Zn-Mg-Cu Alloys[J].Metallurgical and Materials Transactions, A. Physical Metallurgy and Materials Science,2003(4):899-911. |
[17] | Dorward R C .Precipitate coarsening during overageing of AI-Zn-Mg-Cu alloy[J].Materials Science and Technology,1999,15:1133-1138. |
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