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通过原位反应合成使用镍/铝箔对先进异质层压复合材料进行加工参数优化及力学响应分析

Optimization of Processing Parameter and Mechanical Response Analysis of Advanced Heterogeneous Laminated Composites Using Ni/Al Foils by In Situ Reaction Synthesis.

作者信息

Sun Ying, Yuan Shijian

机构信息

Institute of Precision Forming for High Performance, Dalian University of Technology, Dalian 116024, China.

National Key Lab for Precision Hot Processing of Metals, Harbin Institute of Technology, Harbin 150001, China.

出版信息

Materials (Basel). 2022 Dec 13;15(24):8892. doi: 10.3390/ma15248892.

Abstract

The advanced heterogeneous laminated composites were successfully fabricated by vacuum hot pressing using Ni and Al foils by in situ solid-state reaction synthesis. The effects of holding time and temperature on the microstructure and phase distribution were analyzed using scanning electron microscopy. Based on the optimized processing parameters, the microstructure and phase transformation, and the relationship between the microstructure and the corresponding mechanical properties were discussed in detail. To clarify the mechanical response of the laminated structure, the deformation microstructure and fracture characteristics were studied by scanning electron microscopy and electron backscatter diffraction. The results indicated that the evolution of the interfacial phases in the laminated composite occurred via the sequence: NiAl, NiAl, NiAl, and NiAl. An interface between the Ni and NiAl layers without cracks and voids formed due to the uniform pressure applied during hot pressing. The laminated composites hot pressed under 620 °C/5 MPa/1 h + 1150 °C/10 MPa/2 h exhibited the best ultimate tensile strength of 965 MPa and an elongation of 22.6% at room temperature. Extending the holding time during the second stage of the reaction synthesis decreased the thickness of the NiAl layer. This decreased the tensile strength of the laminated composite at 1000 °C but improved the tensile strength at room temperature. Moreover, the layer-thickness relationship of the laminated structure and the matching pattern were important factors affecting the strength and elongation of the laminated composites. The reinforcement form of the materials was not limited to a lamellar structure but could be combined with different forms of reinforcement to achieve continuous reinforcement over a wide range of temperatures.

摘要

采用镍箔和铝箔通过原位固态反应合成法,利用真空热压成功制备了先进的异质层状复合材料。使用扫描电子显微镜分析了保温时间和温度对微观结构和相分布的影响。基于优化的工艺参数,详细讨论了微观结构和相变,以及微观结构与相应力学性能之间的关系。为了阐明层状结构的力学响应,通过扫描电子显微镜和电子背散射衍射研究了变形微观结构和断裂特征。结果表明,层状复合材料中界面相的演变顺序为:NiAl、NiAl、NiAl和NiAl。由于热压过程中施加的均匀压力,镍层和NiAl层之间形成了无裂纹和空隙的界面。在620℃/5MPa/1h + 1150℃/10MPa/2h条件下热压的层状复合材料在室温下表现出最佳的极限抗拉强度965MPa和伸长率22.6%。在反应合成的第二阶段延长保温时间会降低NiAl层的厚度。这降低了层状复合材料在1000℃时的抗拉强度,但提高了室温下的抗拉强度。此外,层状结构的层厚关系和匹配模式是影响层状复合材料强度和伸长率的重要因素。材料的增强形式不限于层状结构,还可以与不同形式的增强相结合,以在很宽的温度范围内实现连续增强。

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