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首页> 外文期刊>Surface & Coatings Technology >SiC/ZrB2-SiC-ZrC multilayer coating for carbon/carbon composites against ablation
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SiC/ZrB2-SiC-ZrC multilayer coating for carbon/carbon composites against ablation

机译:用于碳/碳复合材料抗烧蚀的SiC / ZrB2-SiC-ZrC多层涂层

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摘要

To improve the ablation resistance of carbon/carbon (C/C) composites at high temperature, a ZrB2-SiC-ZrC coating was prepared on the surface of SiC-coated C/C composites by supersonic atmosphere plasma spray (SAPS). Ablation resistance of the coated C/C composites was tested in an oxyacetylene torch environment with a heat flux of 2400 kW/m(2) for 120,150 and 200 s, respectively. After ablation for 120 s, the coating exhibited a three layered structure consisting of a porous ZrO2 layer, a ZrO2-SiO2 thin layer and a SiC-depleted layer, whereas it transformed into a two-layered structure (ZrO2 recrystallized layer and ZrO2-SiO2 layer) after ablation for 150 s. With the increase of ablation time, the SiC inner coating was almost consumed and a gap emerged between the ZrO2 layer and the C/C matrix after ablation for 200 s. The good ablation resistance of the sprayed coating is mainly attributed to the layered structure acting as a thermal barrier and inhibiting inward diffusion of oxygen. (C) 2016 Elsevier B.V. All rights reserved.
机译:为了提高碳/碳(C / C)复合材料在高温下的耐烧蚀性能,采用超音速等离子体喷涂(SAPS)在SiC包覆的C / C复合材料表面制备了ZrB2-SiC-ZrC涂层。涂覆的C / C复合材料的抗烧蚀性在氧乙炔焊炬环境下分别以2400 kW / m(2)的热通量120,150和200 s进行测试。烧蚀120 s后,涂层表现出由多孔ZrO2层,ZrO2-SiO2薄层和SiC耗尽层组成的三层结构,而转变为两层结构(ZrO2重结晶层和ZrO2-SiO2烧蚀150 s后)。随着烧蚀时间的增加,烧蚀200 s后,SiC内涂层几乎被消耗,ZrO2层与C / C基体之间出现缝隙。喷涂涂层的良好的耐烧蚀性主要归因于用作热障并抑制氧向内扩散的层状结构。 (C)2016 Elsevier B.V.保留所有权利。

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