收稿日期:2023-04-10
修回日期:2023-05-16
接受日期:2023-06-26
出版日期:2024-02-15
发布日期:2023-07-11
通讯作者:
柳彦博
E-mail:boobbyy@163.com
基金资助:
Zhiting GAO1,2, Zhuang MA1,2, Yanbo LIU1,2(
)
更多阅读
Received:2023-04-10
Revised:2023-05-16
Accepted:2023-06-26
Online:2024-02-15
Published:2023-07-11
Contact:
Yanbo LIU
E-mail:boobbyy@163.com
Supported by:摘要:
使用飞秒激光在化学气相沉积(CVD)-SiC中间层表面制备不同尺寸的阵列,研究了阵列结构对ZrB2/SiC涂层性能的影响。 更多阅读结果表明,随着激光刻蚀频次的增大,阵列结构的深度从30 µm增大到150 µm。采用氧乙炔烧蚀600 s,ZrB2/SiC涂层烧蚀表面温度随CVD-SiC微结构深度增大而逐步降低,最低的表面温度达到1 700 °C,下降了约200 ℃。烧蚀中心区域的颜色从白色过渡到浅灰色。对于激光刻蚀频次为5的试样,在600 s的单次烧蚀后,质量烧蚀率和线性烧蚀率分别为-7.4 × 10-5 g/s和-13.3 µm/s。阵列结构增大了ZrB2/SiC涂层与CVD-SiC中间层的接触面积,从而增强了导热性能,减少了热积聚,进而改善了ZrB2/SiC涂层的抗烧蚀性能。
中图分类号:
高志廷, 马壮, 柳彦博. CVD-SiC阵列结构对ZrB2/SiC涂层抗烧蚀性影响[J]. 航空学报, 2024, 45(3): 428842.
Zhiting GAO, Zhuang MA, Yanbo LIU. Effect of CVD-SiC array structure on ablation resistance of ZrB2/SiC coatings[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 428842.
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