高抗氧化Ti- 4mo合金与双尺度网络结构的Ti- 5Si - 3增强

Q. Lu, Y. Lv, Chi Zhang, Hong-bo Zhang, Wei Chen, Zhanyuan Xu, P. Feng, J. Fan
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引用次数: 0

摘要

钛合金是先进高超声速飞机发动机和燃气轮机应用的理想材料,但目前很少有材料能够满足相关的高温氧化要求。本文采用低能铣削和放电等离子烧结的方法,设计并制备了Ti5Si3增强Ti-4Mo双尺度网络结构复合材料。由于原位形成多组分表面层,在800°C时表现出优异的抗氧化性能。结果表明,该氧化层具有致密的晶粒尺寸梯度结构,由外层TiO2氧化层和内部具有核壳结构的TiO2和SiO2混合氧化层组成,具有显著的抗氧化性和热稳定性。此外,还发现氧化过程中Ti5Si3增强剂与氮之间的相互作用有助于形成TiN纳米孪晶界面层,该界面层可容纳氧化层与基体之间的热失配应变。这与高附着力一起赋予优秀的热循环寿命,在长期氧化过程中没有开裂或剥落。在这方面,安全工作温度可以提高到800°C,这可以为高温应用的新型钛基复合材料家族提供设计途径。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Highly Anti-Oxidized Ti-4Mo Alloy With Two-Scale Network Architectured Ti 5Si 3 Reinforcement
Titanium alloys are desirable for applications in advanced hypersonic aircraft engines and gas turbines, but currently few materials can satisfy the associated high temperature oxidation requirements. Herein, we designed and fabricated a Ti5Si3 reinforced Ti-4Mo composite with a two-scale network architecture by low energy milling and spark plasma sintering. It displays superior oxidation resistance at 800°C owing to the in-situ formation of a multi-component surface layer. This oxide layer has been revealed to have a dense grain size gradient structure that consists of an outer TiO2 oxide layer and an inner TiO2 and SiO2 mixed oxide layer with a core-shell structure, which has remarkable oxidation resistance and thermal stability. Furthermore, it was revealed that the hitherto unknown interaction between Ti5Si3 reinforcements and nitrogen during oxidation would contribute to the formation of a TiN nano-twin interface layer, which accommodates the thermal mismatch strain between oxide layer and matrix. This along with high adhesion confers excellent thermal cycling life with no cracking or spallation during long term oxidation. In this regard, the secure operating temperature can be increased to 800°C, which can provide a design pathway for a new family of titanium matrix composites for high-temperature applications.
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