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U.S. Department of Energy
Office of Scientific and Technical Information

Japanese fuels and lubricants, Article 3: naval research on alcohol fuel

Technical Report ·
OSTI ID:5178477
Toward the end of World War II, Japan used alcohols, especially ethanol, as fuels for some training planes. Fuel tests showed that 99% ethanol could be used in engines of 300 to 500 hp with full-power rating, but for high-output engines, it could be used only in conditions of reduced power. In all carburetted engines, 94% ethanol gave acceleration difficulties; whereas in solid injection engines 94% ethanol could be used for the low-power range. Blends of equal parts of gasoline and 99% ethanol having the same octane number as the base gasoline could be used in high-output engines at reduced power. Blends of gasoline and 94% ethanol could not be used due to insolubility characteristics. Some of the difficulties encountered with ethanol as fuel were because of its low specific heat, low volatility, high latent heat of vaporization, pre-ignition tendencies, and corrosive action on metals. These led to poor distribution of the fuel in multi-cylinder engines, causing wide variations in mixture strength among cylinders. Also these caused difficulties in starting and acceleration, especially at low atmospheric temperatures. In order to improve volatility, tests were run with additives to alcohol fuel, including ethyl ether, acetone, and gasoline. Ethyl ether improved volatility but increased detonation, thus limiting its allowable concentration to about 3%. Ethanol was very corrosive to aluminum and brass in carburetor and engine injection systems, but dibutyl amine and sodium arsenite additives seemed to retard the corrosion. Methanol tended to corrode magnesium and its alloys, but alkaline solutions of potassium chromate were good inhibitors.
Research Organization:
Department of the Navy, Washington, D.C. (USA)
OSTI ID:
5178477
Report Number(s):
TOM-231-559-569
Country of Publication:
United States
Language:
English