Synergetic improvement of robustness-oxidation resistance integration with strong microwave absorption in Cf/HfB2-SiC(Hf, rGO) composite PDCs for hypersonic vehicle components

IF 5.8 2区 材料科学 Q2 CHEMISTRY, PHYSICAL
Siqi Lan , Wenyan Huang , Zhichao Xue , Yeqi Zhu , Shengjian Mao , Rongdan Lei , Jiahua Zhan , Ruyin Zhao , Rongqian Yao
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Abstract

High-temperature oxidation resistance and reliability are crucial for thermal protection system (TPS) materials of hypersonic vehicles. Furthermore, the swift development of aerospace industry pushes developments for multi-functional materials to achieve balanced integration in light weight, high strength, thermal insulation/isolation, and electromagnetic (EM) wave absorption. Herein, HfB2-SiC(Hfb, rGO) PDCs were fabricated by re-pyrolyzing ball-milling blends of Hf-modified fillers/precursors with 30 wt.% HfB2. The products with promoted phase compatibility exhibit good mechanical performances, owing to Hf-containing structure like HfOSi. The best combination of fillers/precursors are chosen to construct Cf(x)/SiO2-HfB2-SiC(Hfb, rGO) PDCs to further enhance load bearing capacity. By adjusting the initial Cf length to 2 mm, compressive strength and flexural strength of the material are increased to 264.44 MPa and 83.70 MPa respectively, owing to energy dissipation mechanism including crack deflection, fiber breakage, and fiber pull-out. Notably, the sample maintains stable structure and good mechanical performances after 60 min oxidation under 1300 °C butane torch flame, with hardness of 5.32 GPa and fracture toughness of 4.80 MPa⋅m1/2. Formation of self-healing HfO2(HfSiO4)-SiO2-B2O3 continuous layer timely seals the small cracks and pores left by oxidation of Cf, restrains catastrophic oxidation inside. More interestingly, HfB2-SiC(Hfb, rGO) PDCs doped by Co nanopowders exhibit excellent EM wave absorption capacity especially at the thickness of 1.5 mm with the maximum effective absorption bandwidth (EABmax) of 4.04 GHz (13.04–17.44 GHz) and corresponding minimal reflection loss (RLmin) of −40.03 dB. This work provides a new idea to realize multi-functional application of materials with similar components for TPS in aerospace field.

Abstract Image

高超声速飞行器部件用Cf/HfB2-SiC(Hf, rGO)复合PDCs鲁棒性-抗氧化集成与强微波吸收的协同改进
高温抗氧化性和可靠性是高超声速飞行器热防护系统(TPS)材料的关键。此外,航空航天工业的快速发展推动了多功能材料的发展,以实现轻量化、高强度、隔热/隔离和电磁波吸收的平衡集成。本文采用HfB2改性填料/前驱体与30wt .% HfB2的球磨共混再热解法制备了HfB2- sic (Hfb, rGO) PDCs。由于HfOSi等含hf结构的存在,相相容性提高的产物具有良好的力学性能。选择填料/前驱体的最佳组合,构建Cf(x)/SiO2-HfB2-SiC(Hfb, rGO) PDCs,进一步提高其承载能力。将初始Cf长度调整为2 mm后,材料的抗压强度和抗弯强度分别提高到264.44 MPa和83.70 MPa,主要是由于裂缝挠曲、纤维断裂和纤维拔出等耗能机制。在1300℃丁烷火炬火焰下氧化60 min后,样品结构稳定,力学性能良好,硬度为5.32 GPa,断裂韧性为4.80 MPa⋅m1/2。形成自愈的HfO2(HfSiO4)-SiO2-B2O3连续层,及时封闭Cf氧化留下的细小裂纹和孔洞,抑制内部的灾难性氧化。更有趣的是,Co纳米粉掺杂的HfB2-SiC(Hfb, rGO) PDCs具有优异的电磁波吸收能力,特别是在1.5 mm厚度处,最大有效吸收带宽(EABmax)为4.04 GHz (13.04-17.44 GHz),相应的最小反射损耗(RLmin)为-40.03 dB。本工作为TPS在航空航天领域实现类似部件材料的多功能应用提供了新的思路。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Journal of Alloys and Compounds
Journal of Alloys and Compounds 工程技术-材料科学:综合
CiteScore
11.10
自引率
14.50%
发文量
5146
审稿时长
67 days
期刊介绍: The Journal of Alloys and Compounds is intended to serve as an international medium for the publication of work on solid materials comprising compounds as well as alloys. Its great strength lies in the diversity of discipline which it encompasses, drawing together results from materials science, solid-state chemistry and physics.
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