...
首页> 外文期刊>Materials Science and Engineering >Mitigation of scan strategy effects and material anisotropy through supersolvus annealing in LPBF IN718
【24h】

Mitigation of scan strategy effects and material anisotropy through supersolvus annealing in LPBF IN718

机译:通过LPBF IN718中的超固溶退火缓解扫描策略效应和材料各向异性

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

The nickel-based superalloy Inconel 718 (IN718) is an excellent candidate among the existing aerospace alloys for laser powder bed fusion (LPBF) manufacturing. LPBF IN718 has a preference for (001) growth, resulting in a non-uniform, anisotropic microstructure which translates into orthotropic mechanical behavior. The most common heat treatment applied to IN718 is AMS 5662. This treatment was developed 60 years ago for wrought and cast metal forming processes. The small grains and columnar grain structure of LPBF IN718 are not affected by treatments per AMS 5662. Recrystallization and the removal of scan strategy effects have big implications for the acceptance of AM parts. If parts can be heat treated to remove any OEM-related microstructural differences, then parts fabricated on different machines can be printed in any orientation and possess the same properties. This research studies the microstructure of LPBF IN718 as it evolves under an annealing treatment of 1160 degrees C for up to 8 hours. It was hypothesized and later confirmed that this higher-temperature annealing would mitigate the scan strategy effects and anisotropy resulting from the LPBF process. The grain size, shape, and re crystallization are compared throughout the evolution. Additionally, the X-Y and X-Z planes are compared to find a point at which the annealing process results in equiaxed, isotropic grains and the scan strategy effects are mitigated. An equiaxed microstructure was successfully achieved through recrystallization and grain growth, resulting in isotropic microstructure for each scan strategy that was considered. Isotropic mechanical properties were achieved following a modified annealing treatment at 1160 degrees C for 4 hours and validated via nanoindentation and tensile testing.
机译:镍基超合金Inconel 718(IN718)是用于制造激光粉末床熔合(LPBF)的现有航空合金中的极佳候选者。 LPBF IN718偏爱(001)生长,因此会产生不均匀的各向异性微观结构,从而转变为正交各向异性的机械行为。 IN718上最常用的热处理是AMS5662。这种热处理是60年前开发的,用于锻造和铸造金属成型工艺。 LPBF IN718的小晶粒和柱状晶粒结构不受根据AMS 5662进行的处理的影响。再结晶和消除扫描策略效应对AM零件的接受具有重大影响。如果可以对零件进行热处理以消除任何与OEM相关的微观结构差异,那么可以在任何方向上印刷在不同机器上制造的零件并具有相同的特性。这项研究研究了LPBF IN718在1160摄氏度的退火处理下长达8小时的演化过程中的微观结构。进行了假设,后来证实,这种较高温度的退火将减轻LPBF工艺导致的扫描策略效果和各向异性。在整个演化过程中,对晶粒尺寸,形状和再结晶进行了比较。另外,将X-Y和X-Z平面进行比较,以找到退火过程导致等轴性各向同性晶粒的点,并减轻了扫描策略的影响。通过重结晶和晶粒生长成功实现了等轴组织,从而为所考虑的每种扫描策略提供了各向同性的组织。经过改进的退火处理,在1160摄氏度下进行了4小时的退火后,各向同性的机械性能得以实现,并通过纳米压痕和拉伸测试得到了验证。

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