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Synthesis of aluminum nanoparticles as additive to enhance ignition and combustion of high energy density fuels |
Xiu-Tian-Feng E1,2, Lei Zhang1,2, Fang Wang1,2, Xiangwen Zhang1,2, Ji-Jun Zou1,2() |
1. Key Laboratory for Green Chemical Technology of the Ministry of Education, School of Chemical Engineering and Technology, Tianjin University, Tianjin 300072, China 2. Collaborative and Innovative Center of Chemical Science and Engineering (Tianjin), Tianjin 300072, China |
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Abstract High energy density fuels are critical for hypersonic aerospace propulsion but suffer from difficulties of ignition delay and incomplete combustion. This research reports aluminum nanoparticles (Al NPs) assisted ignition and combustion of high energy density JP-10 fuel. Al NPs with a size of 16 nm were fabricated through a mild and simple method by decomposing AlH3·Et2O with the addition of a surfactant ligand. The uniform size distribution, nanoscaled size and surface ligand make Al NPs stably suspend in JP-10, with 80% NPs being dispersed in the liquid fuel after six months. A shock tube test shows that the presence of 1 wt-% Al NPs can significantly shorten ignition delay time at temperature of 1500 to 1750 K, promote the combustion, and enhance energy release of JP-10. This work demonstrates the potential of Al NPs as ignition and combustion additive for high energy density fuel in hypersonic applications.
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Keywords
aluminum nanoparticles
combustion
ignition
shock tube test
high energy density fuel
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Corresponding Author(s):
Ji-Jun Zou
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Online First Date: 07 February 2018
Issue Date: 18 September 2018
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