激光粉末床熔合和热等静压后处理ni3al基金属间合金的微观开裂、显微组织和力学性能

Mingyu Liu , Jiang Wang , Tao Hu , Songzhe Xu , Sansan Shuai , Weidong Xuan , Shuo Yin , Chaoyue Chen , Zhongming Ren
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摘要

ni3al基合金具有优异的高温性能,是涡轮发动机结构材料的理想候选材料。研究了高γ′体积分数ni3al基IC-221 M合金的激光粉末床熔合和热后等静压(HIP)处理。成形样品存在不可避免的凝固裂纹和塑性倾斜裂纹,激光参数优化可将裂纹密度降低至1.34 mm/mm2。透射电子显微镜(TEM)分析显示,由于快速凝固过程中的高冷却速率,在构建样品中存在超细的纳米级γ′相。经过HIP处理后,获得了完全致密的无裂纹缺陷组织,晶粒尺寸为~ 120 ~ 180 μm的等轴组织和形状不规则的~ 1 ~ 3 μm γ′析出物,含量高达86%。室温拉伸试验表明,试样的极限抗拉强度(σUTS)为1039.7 MPa,断裂伸长率为6.4%。经HIP处理后,裂纹缺陷消除,延展性明显提高(15.7%),强度略有下降(σUTS为831.7 MPa)。在900℃时,试样的σUTS值分别为589.8 MPa和786.2 MPa。HIP样品的延展性略有下降至12.9%,表明其具有优异的高温力学性能。此外,强度的异常增加和塑性的异常降低表明高γ′分数在裂纹形成中的关键作用。重复热循环过程中的本征热处理会在热影响区诱发脆性并引发裂纹萌生,塑性显著恶化。结果表明,LPBF与HIP复合可以有效降低ni3al基合金的裂纹密度,提高其力学性能,是一种很有前途的高温材料。
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Laser powder bed fusion of a Ni3Al-based intermetallic alloy with tailored microstructure and superior mechanical performance

Ni3Al-based alloys are excellent candidates for the structural materials used for turbine engines due to their excellent high-temperature properties. This study aims at laser powder bed fusion and post-hot isostatic pressing (HIP) treatment of Ni3Al-based IC-221 ​M alloy with a high γ′ volume fraction. The as-built samples exhibits unavoidable solidification cracking and ductility dip cracking, and the laser parameter optimization can reduce the crack density to 1.34 ​mm/mm2. Transmission electron microscope (TEM) analysis reveals ultra-fine nanoscale γ′ phases in the as-built samples due to the high cooling rate during rapid solidification. After HIP treatment, a fully dense structure without cracking defects is achieved, which exhibits an equiaxed structure with grain size ∼120–180 ​μm and irregularly shaped γ′ precipitates ∼1–3 ​μm with a prominently high fraction of 86%. The room-temperature tensile test of as-built samples shows a high ultimate tensile strength (σUTS) of 1039.7 ​MPa and low fracture elongation of 6.4%. After HIP treatment, a significant improvement in ductility (15.7%) and a slight loss of strength (σUTS of 831.7 ​MPa) are obtained by eliminating the crack defects. Both the as-built and HIP samples exhibit retained high σUTS values of 589.8 ​MPa and 786.2 ​MPa, respectively, at 900 ​°C. The HIP samples exhibita slight decrease in ductility to ∼12.9%, indicating excellent high-temperature mechanical performance. Moreover, the abnormal increase in strength and decrease in ductility suggest the critical role of a high γ′ fraction in cracking formation. The intrinsic heat treatment during repeating thermal cycles can induce brittleness and trigger cracking initiation in the heat-affected zone with notable deteriorating ductility. The results indicate that the combination of LPBF and HIP can effectively reduce the crack density and enhance the mechanical properties of Ni3Al-based alloy, making it a promising material for high-temperature applications.

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