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    ZHENG Xiao-ping, ZHANG Wei-wen, SHAO Ming, LI Yuan-yuan. Heat Treatment Process for 7075/6009 Aluminum Alloy Laminated Composite Plate[J]. Materials and Mechanical Engineering, 2012, 36(7): 41-45.
    Citation: ZHENG Xiao-ping, ZHANG Wei-wen, SHAO Ming, LI Yuan-yuan. Heat Treatment Process for 7075/6009 Aluminum Alloy Laminated Composite Plate[J]. Materials and Mechanical Engineering, 2012, 36(7): 41-45.

    Heat Treatment Process for 7075/6009 Aluminum Alloy Laminated Composite Plate

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    • Received Date: February 07, 2012
    • Different solid solution and aging treatments were performed with 7075/6009 aluminum alloy laminated composite plate to obtain the optimal heat treatment process, and the mechanical properties and tensile fracture of the composite plate after heat treatment were analyzed. The results show that the optimal heat treatment process of the composite plate was solid solution at 485 ℃ for 30 min followed by water quenching and aging at 175 ℃ for 8 h followed by cooling in furnace. The tensile strength, yield strength and elongation of the composite plate were 404 MPa, 364 MPa and 15.3 %, respectively. A lot of dimples was found on the tensile fracture of outer layer 6009 aluminum alloy and the innerlayer and outerlayer alloys had a good metallurgical bonding.
    • [1]
      KIM J K, YU Tong-xi.Forming and failure behaviour of coated, laminated and sandwiched sheet metals a review[J].Journal of Materials Processing Technology, 1997, 63(1/3):33-42.
      [2]
      LI Yuan-yuan, ZHANG Wei-wen, CHEN Wei-ping. Preparation and tensile property of a high-strength, anticorrosion functionally graded 2024/3003 composite [J].Journal of Materials Science, 2004, 39(16/17):5607-5609.
      [3]
      ZHANG Y X, YANG C H. Recent developments in finite element analysis for laminated composite plates[J].Composite Structures, 2009, 88(1):147-157.
      [4]
      GRISHABER R B, SERGUEEVA A V, MISHRA R S, et al.Laminated metal composites-high temperature deformation behavior[J].Materials Science and Engineering A, 2005, 403(1/2):17-24.
      [5]
      AYDOGDU M. A new shear deformation theory for laminated composite plates[J].Composite Structures, 2009, 89(1):94-101.
      [6]
      YU G. Method for manufacturing gradient material by continuous and semi-continuous casting:United States, 6089309[P].2000-07-18.
      [7]
      张卫文, 张大童, 龙雁, 等.高强耐蚀复合铝合金材料:中国, ZL02115163.6[P].2005-06-29.
      [8]
      张卫文, 李元元.半连续铸造法制备AlCu/Al梯度材料[J].中国有色金属学报, 2002, 12(增1):188-191.
      [9]
      郑小平.梯度复合7075/6009铝合金材料的制备与力学性能研究[D].广州:华南理工大学, 2009.
      [10]
      LI Yuan-yuan, ZHENG Xiao-ping, ZHANG Wei-wen, et al.Effect of deformation temperature on microstructures and properties of 7075/6009 alloy[J].Transactions of Nonferrous Metals Society of China, 2009, 19(5):1037-1043.
      [11]
      郑小平, 张卫文, 王珺文, 等.内熔体浇口位置对7075/6009合金铸锭内层组织的影响[J].中国有色金属学报, 2009, 19(1):26-31.
      [12]
      陈康华, 刘红卫, 刘允中.升温固溶对Al-Zn-Mg-Cu合金组织与力学性能的影响[J].中南工业大学学报, 2000, 31(4):339-341.
      [13]
      王祝堂, 田荣章.铝合金及其加工手册[M].长沙:中南大学出版社, 2000.
      [14]
      高革.关于飞机用铝合金7075的热处理[J].轻合金加工技术, 1974(4):12-19.
      [15]
      陈康华, 刘允中, 刘红卫.7075和2024铝合金的固溶组织与力学性能[J].中国有色金属学报, 2000, 10(6):819-822.
      [16]
      曾苏民.影响铝合金固溶保温时间的多因素相关规律[J].中国有色金属学报, 1999, 9(1):79-86.

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