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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.

Active Publication Date: 2019-06-18
HUBEI INST OF AEROSPACE CHEMOTECHNOLOGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Compared with liquid hydrogen, endothermic hydrocarbon fuel has the advantages of easy storage, portability, and practical application, but its cooling capacity is limited, and it is easy to coke at high temperatures, which affects the normal operation of the engine. At the same time, its chemical reaction speed is slow (compared to Hydrogen is 3∼5 orders of magnitude slower), and the calorific value is low (the calorific value per unit mass is only 1 / 3 of that of hydrogen)
The main performance is that the effective heat sink value of fuel cannot meet the thermal management requirements of high Mach number aircraft, the ignition and combustion performance of fuel needs to be improved, and the application of fuel engineering is difficult

Method used

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Examples

Experimental program
Comparison scheme
Effect test

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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Abstract

The invention discloses high-heat-absorption fuel for a hypersonic-velocity aircraft and a preparation method and belongs to the field of fuel for aircrafts. The high-heat-absorption fuel is preparedfrom heat-absorption liquid hydrocarbon fuel and metal hydride. The high-heat-absorption fuel is prepared from components in percentage by mass as follows: 55%-86% of heat-absorption liquid hydrocarbon fuel, 12%-40% of metal hydride, 0-5% of a surfactant and 0-2% of other functional additives. The prepared high-heat-absorption fuel has high density Rho larger than or equal to 0.780 g / cm<3> at thetemperature of 20 DEG C, high heat sink value (the effective heat sink value higher than 5.0 MJ / kg at the temperature of 750 DEG C), little high temperature pyrolysis coking amount, high heat value larger than or equal to 35 MJ / Kg and short ignition delay time and can realize rapid organization combustion in a scramjet engine, so that the flight Mach number of a weapon is higher.

Description

technical field [0001] The invention belongs to fuel for hypersonic aircraft. It specifically relates to an endothermic fuel for an actively cooled scramjet engine of a hypersonic aircraft, which belongs to the field of aircraft fuel. Background technique [0002] Hypersonic speed refers to the flight speed greater than 5Ma. Compared with active missiles, hypersonic missiles have the following advantages: rapid strike capability, strong penetration capability, long-range precision strike capability, and powerful target damage capability. Hypersonic weapons are more powerful than existing non-nuclear weapons, and can perform a variety of combat tasks (such as attacking time-sensitive targets, destroying deep underground targets, etc.), and have the same damage effect as nuclear weapons, but they are more flexible than nuclear weapons. Operational Application and Credibility. The emergence of this weapon system with a strategic deterrent effect has enabled conventional weapo...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C10L1/04C10L1/12C10L1/16C10L1/183C10L1/188C10L1/20C10L1/222C10L1/236C10L1/24C10L1/26
CPCC10L1/04C10L1/10C10L1/106C10L1/1216C10L1/1691C10L1/1832C10L1/1881C10L1/201C10L1/2222C10L1/2368C10L1/2406C10L1/2437C10L1/265
Inventor 王芳付晓梦李伟王伟庞爱民
Owner HUBEI INST OF AEROSPACE CHEMOTECHNOLOGY
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