A kind of high endothermic fuel for hypersonic aircraft and its preparation method
A hypersonic, aircraft technology, applied in the field of aircraft fuel, can solve problems such as slow chemical reaction speed, limited cooling capacity, and burning performance to be improved, and achieve the effects of high weapon flight Mach number, short ignition delay time, and easy practical application.
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Embodiment 1
[0033] Add 0.50g of octadecylamine to 1.83g of JP-10 fuel, mix well and dissolve to form solution A. In the glove box, add 4.00g of LiBH to the four-neck flask 4 , 3.67g JP-10 was fully mixed to form solution B. Under the protection of argon, solution A was added dropwise to solution B. After the dropwise addition, it was stirred for 5 hours to fully and uniformly mix to obtain a high Endothermic fuel, fuel density 0.909g / cm 3 , volume calorific value 38.1MJ / L.
Embodiment 2
[0035] Add 0.25g of N,N'-sodium diethylsulfonate-N,N'-didehydroabietyl-a,w-diamine into 2.35g of RP-3 fuel, mix well and dissolve to form solution A, glove box In the four-neck flask, add 2.60g LiH, 4.70g RP-3 and mix well to form solution B. Under the protection of argon, add solution A to solution B drop by drop. Add 0.10g of 2,6-di-tert-butyl-p-cresol and stir for 8 hours to fully and evenly mix to prepare a highly endothermic fuel for hypersonic aircraft with a fuel density of 0.794g / cm 3 , volume calorific value 37.3MJ / L.
Embodiment 3
[0037] In the glove box, add 1.20gLiH, 8.60g RP-3, and 0.20g methyl bromide into a four-necked flask under the protection of argon. After fully mixing and sealing, mix in an ultrasonic instrument for 3 hours to obtain a high-endothermic type for hypersonic aircraft. Fuel, fuel density 0.793g / cm 3 , volume calorific value 35.1MJ / L.
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