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Ablation Resistance of C/C Composites with Atmospheric Plasma-Sprayed W Coating

机译:C / C复合材料与大气等离子体喷涂W涂层的消融抗性

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摘要

To improve the ablation resistance of carbon/carbon (C/C) composites, tungsten (W) coating with thickness of 1.2 mm was applied by atmospheric plasma spraying. The antiablation property of the coated composites was evaluated by oxyacetylene flame ablation experiments. The phase composition of the coating was investigated by a combination of x-ray diffraction analysis and scanning electron microscopy with energy-dispersive x-ray spectroscopy analysis. The ablation resistance of the coated C/C substrates was compared with that of uncoated C/C composites and C/C-CuZr composites after ablation for 30 s. The properties of the coated C/C composites after ablation time of 10, 30, 60, 90, 120, and 180 s were further studied. The results indicated that the mass and linear ablation rates of the W-coated C/C composites were lower than those of uncoated C/C or C/C-CuZr composites after ablation for 30 s. The coating exhibited heat stability after 120 s of ablation, with mass loss and linear ablation rates of 7.39 x 10(-3) g/s and 3.50 x 10(-3) mm/s, respectively. However, the W coating became ineffective and failed after ablation for 180 s. Three ablation regions could be identified, in which the ablation mechanism of the coating changed from thermochemical to thermophysical erosion to mechanical scouring with increasing ablation time.
机译:为了提高碳/碳(C/C)复合材料的抗烧蚀性能,采用常压等离子喷涂技术,在碳/碳(C/C)复合材料表面涂覆了厚度为1.2mm的钨(W)涂层。通过氧乙炔火焰烧蚀实验评价了涂层复合材料的抗烧蚀性能。采用x射线衍射分析、扫描电镜和能量色散x射线光谱分析相结合的方法研究了涂层的相组成。比较了涂层C/C基片与未涂层C/C复合材料和C/C-CuZr复合材料在烧蚀30s后的抗烧蚀性能,并进一步研究了涂层C/C复合材料在烧蚀10s、30s、60s、90s、120s和180s后的性能。结果表明,W涂层C/C复合材料在烧蚀30s后的质量和线性烧蚀率低于未涂层C/C或C/C-CuZr复合材料。烧蚀120s后,涂层表现出热稳定性,质量损失和线性烧蚀率分别为7.39x10(-3)g/s和3.50x10(-3)mm/s。然而,W涂层在烧蚀180 s后失效。可以确定三个烧蚀区域,其中涂层的烧蚀机制随着烧蚀时间的增加从热化学烧蚀到热物理烧蚀再到机械烧蚀。

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