Abstract:
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2E12 aluminum alloy is a high strength alloy for aeronautical industry.The tensile property,cupping testing method and bending performance were carried out for 2E12 aluminum alloy sheet under T3 and annealing condition at room temperature.The results reveal that the tensile strength,yield strength and yield ratios of annealing are much lower than that of T3 condition,while the elongation is almost consistent under two conditions.The cupping testing IE value is 12% higher than that of T3 condition,and minimum bending radius decreases by 10%,implying that the formability performance under annealing condition is superior to that under T3 condition.
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Funds:
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国家重点基础研究发展计划(973计划)(2005CB623705)
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AuthorIntro:
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Reference:
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[1]武恭,姚良均,彭如清,等.铝及铝合金材料手册[M].北京:科学出版社,1994.
[2]Wang S C,Starink MJ,Gao N.Precipitation harfing in Al-Cu-Mg alloys revisited[J].Scripta Materialia,2006,54:287-291.
[3]Srivatsan T S,Kolar D,Magnusen P.The cyclic fatigue andfinal fracture behavior of aluminumalloy 2524[J].Materialsand Design,2002,23:129-139.
[4]Manabu Nakai,Takehiku Eto.New aspects of developmentof high strength aluminum alloys for aerospace applications[J].Materials Science and Engineering A,2000,285:62-68.
[5]GB4156-84,金属杯突试验方法[S].
[6]GB/T15825.5-1995,金属薄板成形性能与试验方法-弯曲试验[S].
[7]邓明,许洪斌,刘峰.镁合金板材胀形和扩孔性能研究[J].锻压技术,2004,29(4):33-35.
[8]AMS 4296B-2007,航空材料规范[S].
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