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High-energy alcohol-based fuel additive for military use and preparation method thereof

An alcohol-based fuel and additive technology, applied in fuel additives, fuels, liquid carbon-containing fuels, etc., can solve problems such as the impact on the service life of combustion equipment, corrosion of water and sediment, and low combustion calorific value, and improve corrosion resistance The effect of performance and stability, stable quality, and simple production process

Inactive Publication Date: 2018-03-27
SHANDONG LIANXING ENERGY GRP CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the alcohol-based fuels in the existing technology have the following disadvantages when used: low combustion calorific value and low power; unstable, not conducive to transportation, and prone to knocking; water and sediment generated by combustion are corrosive, and long-term use Will seriously affect the service life of combustion equipment

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0023] A military high-energy alcohol-based fuel additive, comprising the following raw materials in parts by weight:

[0024] 10 parts of ethanol, 5 parts of glycerol triacetate, 7 parts of cationic fluorocarbon surfactant, 4 parts of ferric nitrate, 15 parts of hydrocarbon compound, 15 parts of combustion enhancer, 5 parts of stabilizer, 5 parts of antiknock agent, 4 parts of deodorant share.

[0025] Preferably, the combustion enhancer includes hexyl ether, methyl tert-butyl ether and ethyl tert-butyl ether in a weight ratio of 2:3:5.

[0026] Preferably, the stabilizer is di-tert-butyl-p-cresol and isobutylamine in a weight ratio of 3:5.

[0027] Preferably, the antiknock agent is methylcyclodiene manganese tricarbonyl.

[0028] Performance indicators after adding 25% of the above additives into alcohol-based fuels: no mechanical impurities; copper sheet corrosion (50°C, 3h) level 1a (test method GB / T5096); calorific value 22000 kcal / kg (test method GB / T384-1981); flash...

Embodiment 2

[0030] A military high-energy alcohol-based fuel additive, comprising the following raw materials in parts by weight:

[0031] 5 parts of ethanol, 3 parts of glycerol triacetate, 4 parts of cationic fluorocarbon surfactant, 1 part of ferric nitrate, 10 parts of hydrocarbon compound, 15 parts of combustion aid, 3 parts of stabilizer, 5 parts of antiknock agent, 1 part of deodorant share.

[0032] Preferably, the hydrocarbon compound includes heptane, octane and isooctane in a weight ratio of 1:3:2.

[0033] Preferably, the combustion enhancer includes hexyl ether, methyl tert-butyl ether and ethyl tert-butyl ether in a weight ratio of 2:3:5.

[0034] Preferably, the stabilizer is di-tert-butyl-p-cresol and isobutylamine in a weight ratio of 3:5.

[0035] Preferably, the antiknock agent is methylcyclodiene manganese tricarbonyl.

[0036] Preferably, the deodorant is essence.

[0037] Performance indicators after adding 25% of the above additives into alcohol-based fuels: no ...

Embodiment 3

[0039] A military high-energy alcohol-based fuel additive, comprising the following raw materials in parts by weight: 8 parts of ethanol, 4 parts of glycerol triacetate, 5 parts of cationic fluorocarbon surfactant, 3 parts of ferric nitrate, 13 parts of hydrocarbon compounds, and 14 parts of combustion enhancer 4 parts, stabilizer 4 parts, antiknock agent 4 parts, deodorant 2 parts.

[0040] Preferably, the hydrocarbon compound includes heptane, octane and isooctane in a weight ratio of 1:3:2.

[0041] Preferably, the combustion enhancer includes hexyl ether, methyl tert-butyl ether and ethyl tert-butyl ether in a weight ratio of 2:3:5.

[0042] Preferably, the stabilizer is di-tert-butyl-p-cresol and isobutylamine in a weight ratio of 3:5.

[0043] Preferably, the antiknock agent is methylcyclodiene manganese tricarbonyl.

[0044] Preferably, the deodorant is essence.

[0045] Performance indicators after adding 25% of the above additives into alcohol-based fuels: no mecha...

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Abstract

The invention belongs to the technical field of liquid fuel, and more specifically relates to a high-energy alcohol-based fuel additive for military use and a preparation method thereof. The additivecomprises the following raw materials in parts by weight: 5-10 parts of ethanol, 3-5 parts of triacetin, 4-7 parts of a cation fluorocarbon surfactant, 1-4 parts of ferric nitrate, 10-15 parts of a hydrocarbon compound, 10-15 parts of a combustion improver, 3-5 parts of a stabilizing agent, 3-5 parts of an anti-knock agent, and 1-4 parts of a deodorant. The composite additive can be added into thealcohol-based fuel, in order to substantially improve calorific value of the fuel, ensure fully and thoroughly combustion without generation of carbon deposition phenomenon, and improve corrosion resistance and stability of the fuel.

Description

technical field [0001] The invention belongs to the technical field of liquid fuels, and in particular relates to a military high-energy alcohol-based fuel additive and a preparation method thereof. Background technique [0002] Alcohol-based fuel is a clean fuel with the advantages of sanitation, safety and environmental protection, convenient use, and low cost. It is the most potential new alternative renewable resource in the future. However, the alcohol-based fuels in the existing technology have the following disadvantages when used: low combustion calorific value and low power; unstable, not conducive to transportation, and prone to knocking; water and sediment generated by combustion are corrosive, and long-term use It will seriously affect the service life of combustion equipment. Therefore, it is of great significance to study an additive that can improve the above-mentioned shortcomings of alcohol-based fuels. Contents of the invention [0003] The technical pr...

Claims

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Application Information

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IPC IPC(8): C10L1/12C10L1/16C10L1/182C10L1/183C10L1/185C10L1/19C10L1/20C10L1/222C10L1/30
CPCC10L1/10C10L1/1266C10L1/1608C10L1/1824C10L1/183C10L1/1852C10L1/1905C10L1/201C10L1/2222C10L1/305C10L2300/30
Inventor 车春玲
Owner SHANDONG LIANXING ENERGY GRP CO LTD
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