Ablation-resistant (Hf,Zr)B2-SiC composite coating with alternating lamellar architecture by one-step atmospheric plasma spraying

被引:0
|
作者
Lv, Junshuai [1 ]
Li, Wei [1 ]
Li, Zhenglong [1 ]
Fu, Yanqin [2 ]
Ma, Yawen [1 ]
Guo, Lingxiang [1 ]
Li, Jiachen [1 ]
Li, Tao [2 ]
Zhang, Yulei [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Shaanxi Key Lab Fiber Reinforced Light Weight Comp, State Key Lab Solidificat Proc, Xian 710072, Peoples R China
[2] Henan Acad Sci, Inst Carbon Matrix Composites, Henan Key Lab High Performance Carbon Fiber Reinfo, Zhengzhou 450046, Peoples R China
基金
中国国家自然科学基金;
关键词
Ultra-high temperature ceramics; Composite coatings; Alternating lamellar architecture; Ablation resistance; Supersonic atmospheric plasma spraying; CARBON/CARBON COMPOSITES; SILICON-CARBIDE; C/C COMPOSITES; OXIDATION; BEHAVIOR; CERAMICS; GRAPHITE;
D O I
10.1016/j.compositesb.2025.112302
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Inspired by the brick-and-mortar arrangement of mollusk shells, constructing an alternating lamellar architecture is an effective strategy to overcome the catastrophic damage of ablation-resistant coatings and their oxide scales in extreme environments. Here, we developed a coating dominantly composed of alternating layers of (Hf,Zr)B2 and SiC by one-step supersonic atmosphere plasma spraying for C/C composites, which improves fabrication efficiency. The coating shows "zero" ablation and cycling reliability at 2200 degrees C. The resulting oxide scale based on a multilayered (Hf,Zr)O2 skeleton with embedded glassy SiO2 layers is responsible for the superior ablation resistance. The refractory skeleton ensures thermal stability and the SiO2 layers inhibit the oxygen inward diffusion. Two energy dissipation mechanisms, including crack deflection and multilayered delamination, contribute to the structural integrity of the oxide scale due to numerous interfaces in the lamellar architecture. The alternating lamellar coatings enable simultaneously superior oxidation resistance and damage tolerance and have great application potential for reusable aerospace components requiring thermal protection.
引用
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页数:9
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