首页> 外文期刊>Journal of Materials Engineering and Performance >Transient Liquid Phase Bonding of Cu-Cr-Zr-Ti Alloy Using Ni and Mn Coatings: Microstructural Evolution and Mechanical Properties
【24h】

Transient Liquid Phase Bonding of Cu-Cr-Zr-Ti Alloy Using Ni and Mn Coatings: Microstructural Evolution and Mechanical Properties

机译:Cu-Cr-Zr-Ti合金使用Ni和Mn涂层的瞬态液相键合:微观结构演化与机械性能

获取原文
获取原文并翻译 | 示例
       

摘要

High-strength copper alloys are used extensively in the regenerative cooling parts of aerospace structures. Transient liquid phase (TLP) bonding of a Cu-Cr-Zr-Ti alloy was attempted in the present study using thin layers of elemental Ni and Mn coatings applied by electroplating. One of the base metals was given a Ni coating of 4 mu m followed by a Mn coating of 15 mu m, while the other base metal was given only the Ni coating (4 mu m). The bonding cycle consisted of the following: TLP stage-heating to 1030 degrees C and holding for 15 min; homogenization stage-furnace cooling to 880 degrees C and holding for 2 h followed by argon quenching to room temperature. Detailed microscopy and electron probe microanalysis analysis of the brazed joints were carried out. The braze metal was found to undergo isothermal solidification within the 15 min of holding time at 1030 degrees C. At the end of TLP stage, the braze metal showed a composition of Cu-17Ni-9Mn (wt.%) at the center of the joint with a steep gradient in Ni and Mn concentrations from the center of the braze metal to the base metal interfaces. After holding for 2 h at 880 degrees C (homogenization stage), the compositional gradients were found to flatten significantly and the braze metal was found to develop a homogeneous composition of Cu-11Ni-7Mn (wt.%) at the center of the joint. In lap-shear tests, failures were always found to occur in the base metal away from the brazed region. The copper alloy base metal was found to undergo significant grain coarsening due to high-temperature exposure during brazing and, consequently, suffer considerable reduction in yield strength.
机译:高强度铜合金广泛用于航空航天结构的再生冷却部件。在本研究中尝试使用通过电镀施加的薄层和MN涂层的本研究试图Cu-Cr-Zr-Ti合金的瞬态液相(TLP)键合。将其中一种碱金属给予4μm的Ni涂层,然后给出15μm的Mn涂层,而另一个贱金属仅给予Ni涂层(4μm)。粘接循环由以下组成:TLP阶段 - 加热至1030℃并保持15分钟;均匀化阶段炉冷却至880℃并保持2小时,然后氩气淬火至室温。进行了详细的显微镜和电子探针微显微分析分析钎焊接头。发现钎焊金属在1030℃下在1030℃下的15分钟内进行等温凝固。在TLP阶段结束时,钎焊金属在中心的CU-17NI-9MN(WT.%)的组合物中显示出从钎焊金属中心到基础金属界面的Ni和Mn浓度的关节与基础金属界面的关节接头。在880℃(均质化阶段)保持2小时后,发现组成梯度显着变平,发现钎焊金属在关节中心开发Cu-11Ni-7mn(重量%)的均匀组合物。在剪切试验中,始终发现在远离钎焊区域的基础金属中发生故障。发现铜合金基础金属由于在钎焊期间高温暴露而经历显着的晶粒粗化,因此遭受显着降低的屈服强度。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号