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Heat-conducting anti-scouring ceramic-based composite material and preparation method thereof
The invention relates to a heat-conducting anti-scouring ceramic-based composite material and a preparation method thereof. The method comprises the following steps: weaving high-thermal-conductivity carbon fibers into high-thermal-conductivity carbon cloth; uniformly coating phenolic resin on the high-thermal-conductivity carbon cloth to obtain a high-thermal-conductivity prepreg; sequentially carrying out mold pressing, curing and cracking on the high-thermal-conductivity prepreg to obtain a high-thermal-conductivity carbon/carbon green body; reacting and infiltrating the high-heat-conductivity carbon/carbon green body and hafnium-zirconium-silicon alloy to obtain a heat-conducting ceramic matrix; the anti-scouring coating is prepared on the surface of the heat-conducting ceramic matrix through a chemical vapor deposition method, and the heat-conducting anti-scouring ceramic-based composite material is prepared. The prepared heat-conducting anti-scouring ceramic-based composite material is high in heat conductivity, excellent in high-temperature anti-ablation performance and excellent in high-temperature anti-scouring performance, and has a wide application prospect in aerospace crafts.
本发明涉及一种热疏导抗冲刷陶瓷基复合材料及其制备方法。所述方法包括:采用高导热碳纤维编织成高导热碳布;将酚醛树脂均匀涂敷高导热碳布上,得到高导热预浸料;将高导热预浸料依次进行模压、固化和裂解,得到高导热碳/碳坯体;将高导热碳/碳坯体与铪锆硅合金进行反应熔渗,得到热疏导陶瓷基体;在热疏导陶瓷基体的表面通过化学气相沉积法制备抗冲刷涂层,制得热疏导抗冲刷陶瓷基复合材料。本发明制得的热疏导抗冲刷陶瓷基复合材料热导率高、高温抗烧蚀性能优异、高温抗冲刷性能优异,在航空航天飞行器上具有广阔的应用前景。
Heat-conducting anti-scouring ceramic-based composite material and preparation method thereof
The invention relates to a heat-conducting anti-scouring ceramic-based composite material and a preparation method thereof. The method comprises the following steps: weaving high-thermal-conductivity carbon fibers into high-thermal-conductivity carbon cloth; uniformly coating phenolic resin on the high-thermal-conductivity carbon cloth to obtain a high-thermal-conductivity prepreg; sequentially carrying out mold pressing, curing and cracking on the high-thermal-conductivity prepreg to obtain a high-thermal-conductivity carbon/carbon green body; reacting and infiltrating the high-heat-conductivity carbon/carbon green body and hafnium-zirconium-silicon alloy to obtain a heat-conducting ceramic matrix; the anti-scouring coating is prepared on the surface of the heat-conducting ceramic matrix through a chemical vapor deposition method, and the heat-conducting anti-scouring ceramic-based composite material is prepared. The prepared heat-conducting anti-scouring ceramic-based composite material is high in heat conductivity, excellent in high-temperature anti-ablation performance and excellent in high-temperature anti-scouring performance, and has a wide application prospect in aerospace crafts.
本发明涉及一种热疏导抗冲刷陶瓷基复合材料及其制备方法。所述方法包括:采用高导热碳纤维编织成高导热碳布;将酚醛树脂均匀涂敷高导热碳布上,得到高导热预浸料;将高导热预浸料依次进行模压、固化和裂解,得到高导热碳/碳坯体;将高导热碳/碳坯体与铪锆硅合金进行反应熔渗,得到热疏导陶瓷基体;在热疏导陶瓷基体的表面通过化学气相沉积法制备抗冲刷涂层,制得热疏导抗冲刷陶瓷基复合材料。本发明制得的热疏导抗冲刷陶瓷基复合材料热导率高、高温抗烧蚀性能优异、高温抗冲刷性能优异,在航空航天飞行器上具有广阔的应用前景。
Heat-conducting anti-scouring ceramic-based composite material and preparation method thereof
一种热疏导抗冲刷陶瓷基复合材料及其制备方法
LIU WEI (Autor:in) / SUN TONGCHEN (Autor:in) / YANG LIANGWEI (Autor:in) / KONG DELI (Autor:in) / YAN DAN (Autor:in) / LI JIMENG (Autor:in) / CHEN HAORAN (Autor:in) / YU YI (Autor:in) / ZUO HONGJUN (Autor:in) / LIU JUNPENG (Autor:in)
12.11.2024
Patent
Elektronische Ressource
Chinesisch
IPC:
C04B
Kalk
,
LIME
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