欢迎登录材料期刊网

材料期刊网

高级检索

采用Ag47-Cu18-In17-Sn17-Ti1钎料,分别在560,570,580℃下保温30 min对增强相体积分数为15%的SiCp/A356复合材料进行真空钎焊,研究了钎焊接头的显微组织、显微硬度及抗剪强度,并确定了最优的钎焊温度.结果表明:在560~580℃温度区间进行真空钎焊获得的接头焊缝组织致密,钎料对基体铝合金和SiC颗粒都具有良好的润湿性,钎料中各元素在580℃下的扩散距离远大于在560℃下的;随着钎焊温度升高,焊缝中心及扩散区的显微硬度都逐渐下降;最佳的钎焊温度为560℃,在此温度下制备钎焊接头的抗剪强度可达51.8 MPa,焊缝中心与扩散区的显微硬度分别为99.4 HV和110.7 HV,接头的断裂方式表现为塑性断裂.

Taking Ag47-Cu18-In17-Sn17-Ti1 as brazing filler metal, SiCp/A356 composites containing 15vol% SiCp were welded by using vacuum brazing technology under the parameters of temperature 560 ℃,570 ℃, 580 ℃ and soaking for 30 minutes.Microstructure, microhardness and shear strength of the joints were investigated,and then optimal brazing temperature was confirmed.The result indicate that in the brazing temperature range of 560-580 ℃,the compact brazed seam obtained.The brazing filler metal could wet both of the matrix aluminum alloy and SiC particles very well.The diffusion distance of elements in brazing filler metal at 580 ℃ was much longer than that at 560 ℃.The microhardness in brazed seam centre area and diffusion area gradually decreased with the increase of brazing temperature.The optimal brazing temperature was 560 ℃.At this temperature,the maximum shear strength of the jonts could reach 51.8 MPa,and the microhardness in brazed seam centre area and diffusion area was 99.4 HV and 110.7 HV,respectively.The fracture mechanism of the joint was characterized by ductile fracture.

参考文献

[1] 宋加伟;金培鹏;王金辉;朱云鹏.低体积分数SiCp/Al复合材料热变形行为的研究[J].材料导报,2015(2):163-166.
[2] 杜建全;王开坤;周璐;田丽倩.封装SiCp/Cu复合材料组织性能研究[J].武汉科技大学学报(自然科学版),2013(1):41-44.
[3] 郭素娟;康国政;张娟;轩福贞.SiCP/6061Al复合材料高温单轴拉伸时相关棘轮行为的细观本构模型[J].机械工程材料,2014(5):99-103.
[4] 王少刚;刘红霞.SiCp/101Al复合材料的氩气保护炉中钎焊[J].兵器材料科学与工程,2009(2):25-28.
[5] 崔岩.碳化硅颗粒增强铝基复合材料的航空航天应用[J].材料工程,2002(06):3-6.
[6] 邹家生;陈铮;许如强;赵其章.SiCp/LY12复合材料的真空钎焊[J].中国有色金属学报,2004(1):74-78.
[7] Jitai Niu;Zeng Gao;Dongfeng Cheng.Welding of Aluminum Matrix Composites[J].Materials Science Forum,2013:476-482.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%