Solar absorbent, dense, and self-healing ZrB2-SiC anti-oxidative multilayer coating for Carbon/Carbon composites

被引：0

作者：

Cordeiro, Jose C. ^{[1
]}

Zuzelski, Matthew ^{[2
]}

Hart, Jadyn ^{[2
]}

Otanicar, Todd P. ^{[2
]}

Keller, Michael W. ^{[3
]}

Ramsurn, Hema ^{[1
]}

机构：

[1] Univ Tulsa, Russell Sch Chem Engn, 800 S Tucker Dr, Tulsa, OK 74104 USA

[2] Boise State Univ, Mech & Biomed Engn, 1910 Univ Dr, Boise, ID USA

[3] Univ Tulsa, Dept Mech Engn, 800 S Tucker Dr, Tulsa, OK USA

来源：

SOLAR ENERGY | 2025年 / 286卷

基金：

美国能源部;

关键词：

Ceramic matrix composites; Oxide coatings; Oxidation; Thermal cycling; CARBON-CARBON COMPOSITES; OXIDATION PROTECTION; C/C COMPOSITES; PACK CEMENTATION; SIC COATINGS; MICROSTRUCTURE; GROWTH; TEMPERATURE; FABRICATION; RESISTANCE;

D O I：

10.1016/j.solener.2024.113148

中图分类号：

TE [石油、天然气工业]; TK [能源与动力工程];

学科分类号：

0807 ; 0820 ;

摘要：

Due to their high tensile strength, high heat conductivity, and low coefficient of thermal expansion, carbon/carbon composites have been proposed as a material of construction for concentrated solar power (CSP) receivers. A combination of reactive pack cementation, chemical vapor deposition, and slurry coating was used to produce a dense, self-healing, and solar absorbent ZrB2-SiC multilayer protective coating that is effective at moderate to high temperatures (750-850 degrees C) at which CSP receivers are expected to operate. Oxidation in air at 850 degrees C for 150 h showed virtually no weight loss with a final solar weighted absorptance of 0.881.

引用

页数：10

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