TY - JOUR
T1 - Synergistic investigation on thermal insulation in Al2O3/RF/SiO2aerogels via silicon source ratios, heat treatment, and simulation
AU - Ye, Xinli
AU - Chai, Qianye
AU - Zhang, Haiyang
AU - Ma, Xiaomin
AU - Zhang, Junxiong
AU - Zhang, Xiaohua
AU - Zheng, Kai
AU - Wen, Kaige
AU - Xu, Wei
N1 - Publisher Copyright:
© 2025 Elsevier Ltd and Techna Group S.r.l. All rights are reserved, including those for text and data mining, AI training, and similar technologies.
PY - 2025/10
Y1 - 2025/10
N2 - Aerogels have long been recognized in the aerospace field for their ultra‐lightweight properties and excellent thermal insulation, making them ideal for insulation in extreme environments. To address the limitations of mechanical brittleness and insufficient high‐temperature stability in traditional single‐component aerogels, this study synthesized Alumina/Resorcinol-Formaldehyde/Silica (Al2O3/RF/SiO2) aerogels via ambient pressure drying. RF resin served as the organic carbon source to form a three-dimensional organic skeleton, which was subsequently oxidized during heat treatment to create a stable Al2O3/SiO2composite framework with enhanced mechanical integrity. The synergistic effects of silicon source ratios and heat treatment temperatures were systematically investigated to enhance both thermal insulation performance and structural integrity. Experimental results revealed that the aerogel with a silicon source ratio of 3.5:3 exhibited the highest specific surface area and pore volume. The 700 °C heat treatment promoted the oxidation of the RF-derived organic framework and the formation of stable Al2O3/SiO2composites, thereby reducing the room-temperature thermal conductivity to 0.0467 W/(m·K). A thermal insulation simulation validated the thermal insulation mechanism, showing that the optimized three-dimensional nanoscale pore network and dense Al2O3/SiO2skeleton effectively retarded heat transfer, resulting in a steady-state cold surface temperature of 104 °C under a 400 °C thermal load. This work provided a novel strategy for designing lightweight, high-temperature-resistant aerogels with potential applications in insulation and catalyst support systems.
AB - Aerogels have long been recognized in the aerospace field for their ultra‐lightweight properties and excellent thermal insulation, making them ideal for insulation in extreme environments. To address the limitations of mechanical brittleness and insufficient high‐temperature stability in traditional single‐component aerogels, this study synthesized Alumina/Resorcinol-Formaldehyde/Silica (Al2O3/RF/SiO2) aerogels via ambient pressure drying. RF resin served as the organic carbon source to form a three-dimensional organic skeleton, which was subsequently oxidized during heat treatment to create a stable Al2O3/SiO2composite framework with enhanced mechanical integrity. The synergistic effects of silicon source ratios and heat treatment temperatures were systematically investigated to enhance both thermal insulation performance and structural integrity. Experimental results revealed that the aerogel with a silicon source ratio of 3.5:3 exhibited the highest specific surface area and pore volume. The 700 °C heat treatment promoted the oxidation of the RF-derived organic framework and the formation of stable Al2O3/SiO2composites, thereby reducing the room-temperature thermal conductivity to 0.0467 W/(m·K). A thermal insulation simulation validated the thermal insulation mechanism, showing that the optimized three-dimensional nanoscale pore network and dense Al2O3/SiO2skeleton effectively retarded heat transfer, resulting in a steady-state cold surface temperature of 104 °C under a 400 °C thermal load. This work provided a novel strategy for designing lightweight, high-temperature-resistant aerogels with potential applications in insulation and catalyst support systems.
KW - AlO/RF/SiOaerogels
KW - Heat treatment temperature
KW - Silicon source ratio
KW - Thermal insulation
UR - https://www.scopus.com/pages/publications/105012743761
U2 - 10.1016/j.ceramint.2025.08.009
DO - 10.1016/j.ceramint.2025.08.009
M3 - 文章
AN - SCOPUS:105012743761
SN - 0272-8842
VL - 51
SP - 47461
EP - 47470
JO - Ceramics International
JF - Ceramics International
IS - 25
ER -