...
首页> 外文期刊>Surface & Coatings Technology >Effects of scratch tests on the adhesive and cohesive properties of borided Inconel 718 superalloy
【24h】

Effects of scratch tests on the adhesive and cohesive properties of borided Inconel 718 superalloy

机译:划痕试验对硼化型818超合金粘合剂和内聚性能的影响

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

New results about the scratch adhesion resistance of nickel boride layer on Inconel 718 superalloy were estimated in the present study. The nickel boride layer was developed on the surface of Inconel 718 superalloy by means of the powder-pack bonding process conducted at 1173 K with 2, 4, and 6 h of exposure. The microstructure of the nickel boride layer was analyzed from optical microscopy, X-ray diffraction and energy dispersive spectroscopy (EDS). Furthermore, and before the scratch tests, indentation properties of the nickel boride layers such as hardness, Young's modulus, and the distribution of residual stresses were evaluated using Berkovich nanoidentation tests applying a constant load (50 mN) across the diffusion layers. The scratch tests were performed over the surface of the nickel boride layer-substrate systems using a Rockwell-C diamond in-denter with a continuously increasing normal force from 1 to 80 N, whereas the behavior of the coefficient of friction and the residual depth as a function of the scratch length were monitored during the tests. For the determination of the critical loads, the combination of acoustic emission signal with microscopic observations of the worn tracks were used; the critical loads were estimated at which the layer cracks (cohesive failure) or is detached (adhesive failure) and they explained according to the mechanical properties of the nickel boride layer substrate system. For all the set of experimental conditions, the presence of three types of failure mechanisms over the worn tracks were detected, while the results showed that the critical loads increase with enhancing nickel boride layer thickness.
机译:关于在本研究中估计了关于Inconel 718超合金上的镍硼层的刮擦粘附性的新结果。通过在1173k的粉末包装键合工艺,在1173k下进行2,4和6小时,在Inconel 718超合金的表面上显影镍硼层。从光学显微镜,X射线衍射和能量分散光谱(EDS)分析镍硼层的微观结构。此外,在划痕试验之前,使用Berkovich纳米型测试在扩散层上施加恒定负载(50mN),评估镍硼化合物层的压痕性质如硬度,杨氏模量和残余应力的分布。在镍硼层 - 基板系统的表面上使用罗克韦尔-C金刚石衬垫中的牙齿在1至80n中的刚性正常力的表面上进行划痕试验,而摩擦系数和残余深度的行为在测试期间监测划痕长度的函数。为了确定临界负载,使用具有磨损轨道的微观观察的声发射信号的组合;估计临界载荷在该临界载量,其中层裂缝(粘性发生故障)或被分离(粘合衰竭),并且根据镍硼层基板系统的机械性能解释。对于所有的实验条件,检测到在磨损轨道上存在三种类型的故障机制,同时结果表明,临界载荷随着增强的硼化硼层厚度而增加。

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