TY - JOUR
T1 - Ablation-resistant (Hf,Zr)B2–SiC composite coating with alternating lamellar architecture by one-step atmospheric plasma spraying
AU - Lv, Junshuai
AU - Li, Wei
AU - Li, Zhenglong
AU - Fu, Yanqin
AU - Ma, Yawen
AU - Guo, Lingxiang
AU - Li, Jiachen
AU - Li, Tao
AU - Zhang, Yulei
N1 - Publisher Copyright:
© 2025 Elsevier Ltd
PY - 2025/5/15
Y1 - 2025/5/15
N2 - 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 °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.
AB - 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 °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.
KW - Ablation resistance
KW - Alternating lamellar architecture
KW - Composite coatings
KW - Supersonic atmospheric plasma spraying
KW - Ultra-high temperature ceramics
UR - http://www.scopus.com/inward/record.url?scp=85218354158&partnerID=8YFLogxK
U2 - 10.1016/j.compositesb.2025.112302
DO - 10.1016/j.compositesb.2025.112302
M3 - 文章
AN - SCOPUS:85218354158
SN - 1359-8368
VL - 297
JO - Composites Part B: Engineering
JF - Composites Part B: Engineering
M1 - 112302
ER -