2219铝合金厚板TIG焊接头组织与力学性能研究
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四川航天长征装备制造有限公司,成都 610100

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TG444.2

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四川省科技计划重点研发项目(2020YFG0197);四川航天技术研究院重大工艺研究项目(F70520)


Research on Joint Microstructure and Mechanical Properties of TIG Welding of 2219 Aluminum Alloy Thick Plate
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Sichuan Aerospace Changzheng Equipment Manufacturing Co., Ltd., Chengdu 610100

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    摘要:

    采用氦弧打底+氩弧填充、盖面的焊接工艺对2219-T87铝合金15 mm厚板进行TIG焊接试验,研究其焊缝成形和组织力学性能。结果表明,此工艺焊缝成形美观,无可见焊接缺陷,气孔抑制效果好,接头平均抗拉强度为278.22 MPa,平均断后延伸率为3.89%,接头平均强度系数达到58.94%。接头硬度整体表现为焊缝中心最低,从焊缝中心到母材呈现先增大后局部降低再增大的趋势;且焊缝中心填充层硬度高于打底层和盖面层。熔合区的微观组织为柱状树枝晶和胞状树枝晶,且垂直于熔合线生长,在靠近熔合区两侧出现了等轴细晶带。焊接接头断面有较多撕裂棱和韧窝,局部发现第二相粒子和微孔,其断裂机制为典型的韧性断裂。

    Abstract:

    In this paper, the welding process of helium arc bottoming + argon arc filling and covering was used to conduct TIG welding experiment on 15 mm thick plate of 2219-T87 aluminum alloy to study its weld formation,microstructure and mechanical properties. The results show that this process has good weld appearance, no visible welding defects, and good porosity inhibition effect. The average tensile strength of the joint is 278.22 MPa, the average elongation after fracture is 3.89%, and the average strength coefficient of the joint reaches 58.94%. The overall performance of the joint hardness is the lowest in the center of the weld. From the center of the weld to the base material, the hardness first increases, then decreases locally, and then increases; and the hardness of the filler layer in the center of the weld is higher than that of the bottom layer and the cover layer. The microstructure of the fusion zone is columnar dendrite and cellular dendrite, and grows perpendicular to the fusion line. Equiaxed fine grain bands appear on both sides of the fusion zone. There are many tearing edges and dimples on the cross section of the welded joint, and micropores and second phase particles are found locally. The fracture mechanism of the welded joint is typical ductile fracture.

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陈志元,张晓鸿,林鹏,范翼飞,黄色贤.2219铝合金厚板TIG焊接头组织与力学性能研究[J].宇航材料工艺,2023,53(1):64-68.

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  • 收稿日期:2021-07-13
  • 最后修改日期:2023-02-14
  • 录用日期:2021-09-27
  • 在线发布日期: 2023-03-29
  • 出版日期:
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