TY - JOUR
T1 - Preparation of high-energy Al-Li alloy powders with enhanced compatibility and combustion performance by dense fluorosilane polymer composite coating
AU - Fu, Hongdi
AU - Wang, Shuo
AU - Song, Tinglu
AU - Xiong, Weiqiang
AU - Liu, Xuanyan
AU - Xu, Kangcheng
AU - Li, Xiaodong
AU - Zou, Meishuai
N1 - Publisher Copyright:
© 2024 Elsevier B.V.
PY - 2024/11/12
Y1 - 2024/11/12
N2 - The superior combustion heat, lower ignition temperature, and enhanced combustion efficiency of aluminum–lithium (Al-Li) alloy powders have garnered significant research attention in relation to Al powders. However, the inadequate compatibility between Al-Li alloy powders (especially when Li > 3 wt%) and propellant components limits its application in the development of composite solid propellants. This study focuses on the surface-coating active Al-4.3Li (wt.%) alloy powder using a composite fluorosilane coupling agent to improve compatibility and combustion performance. A coating layer with a thickness of 30–40 nm was successfully formed on the surface of Al-4.3Li alloy powder through interactions involving Al-F, Al-O-Si, and Li-O-Si bonds, thereby achieving remarkable hydrophobicity. The heat release increased by 7.5 %, while the ignition delay time of the alloy powder decreased by nearly 200 ms, resulting in a significantly enhanced combustion performance in relation to that of the original Al-4.3Li alloy powder. Moreover, the modified Al-4.3Li alloy powder exhibited better compatibility, and no cracks or bubbles were observed in the cross-section of the propellant containing modified Al-4.3Li metal fuel. This study provides an effective approach for utilizing Al-Li alloy powders in solid propellants, which is of great significance for the development of high-energy propulsion systems.
AB - The superior combustion heat, lower ignition temperature, and enhanced combustion efficiency of aluminum–lithium (Al-Li) alloy powders have garnered significant research attention in relation to Al powders. However, the inadequate compatibility between Al-Li alloy powders (especially when Li > 3 wt%) and propellant components limits its application in the development of composite solid propellants. This study focuses on the surface-coating active Al-4.3Li (wt.%) alloy powder using a composite fluorosilane coupling agent to improve compatibility and combustion performance. A coating layer with a thickness of 30–40 nm was successfully formed on the surface of Al-4.3Li alloy powder through interactions involving Al-F, Al-O-Si, and Li-O-Si bonds, thereby achieving remarkable hydrophobicity. The heat release increased by 7.5 %, while the ignition delay time of the alloy powder decreased by nearly 200 ms, resulting in a significantly enhanced combustion performance in relation to that of the original Al-4.3Li alloy powder. Moreover, the modified Al-4.3Li alloy powder exhibited better compatibility, and no cracks or bubbles were observed in the cross-section of the propellant containing modified Al-4.3Li metal fuel. This study provides an effective approach for utilizing Al-Li alloy powders in solid propellants, which is of great significance for the development of high-energy propulsion systems.
KW - Al-Li alloy powder
KW - Combustion characteristics levels
KW - Fluorosilane surface coating
KW - Solid propellants
UR - http://www.scopus.com/inward/record.url?scp=85200461299&partnerID=8YFLogxK
U2 - 10.1016/j.apsusc.2024.160788
DO - 10.1016/j.apsusc.2024.160788
M3 - Article
AN - SCOPUS:85200461299
SN - 0169-4332
VL - 673
JO - Applied Surface Science
JF - Applied Surface Science
M1 - 160788
ER -