材料科学
陶瓷
多孔性
热导率
复合材料
碳化物
化学工程
工程类
作者
Cuiyan Li,Ruinan Gao,Haibo Ouyang,Tianzhan Shen,Zihao Chen,Yanlei Li
标识
DOI:10.26599/jac.2024.9220909
摘要
To meet the emerging demands for thermal protection materials of hypersonic aircraft, developing porous ultrahigh temperature ceramics with both robust mechanical properties and superior thermal insulation performance is a critical challenge. Herein, we report a novel porous (Ta0.2Nb0.2Ti0.2Zr0.2Hf0.2)C high-entropy carbide (PHEC) ceramic fabricated by a self-foaming method using commercially available metal chloride and furfuryl alcohol as the precursor. The PHEC ceramic is constructed by microspheres with a size of 2 µm, leading to a high porosity of 91.3% and an interconnected frame. These microspheres consist of high-entropy carbide grains (20 nm), resulting in abundant interface and nanosized pores in the PHEC ceramic. Due to its unique hierarchical structure, the prepared PHEC ceramic has outstanding compressive strength (28.1±2 MPa) and exceptionally low thermal conductivity at room temperature (0.046 W·m−1·K−1). This makes it a promising thermal insulation material in ultrahigh temperature application. This work provides a cost-effective and facility strategy to produce porous ultrahigh temperature ceramics.
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