FIELD: chemistry.
SUBSTANCE: invention relates to lubricant compositions for aviation power installations and more specifically: for gas-turbine engines of aeroplanes, main reduction gears and heavy loaded transmission assemblies and the oil system of the turbocharger of helicopter engines. The composition contains the following in wt %: bis [4-(1,1,3-tetramethylbutyl)phenyl]amine 1-3; C7-C9 alkyl ether 3,5-bis-(1,1 dimethylethyl)-4-hydroxybenzo propanoic acid 0.5-4; N,N-bis-(2ethylhexyl)-4 methyl-1H-benzotriazole-1-methylamine 0.05-0.25; tricresyl phosphate 1-5; 3-(bis-isobutoxy-thiophosphoryl sulphanyl)-2-methyl-propanoic acid 0.05-1.5; ester of neopentylpolyol and fatty acids C5 - C10 - the rest.
EFFECT: improved anticorrosion properties at high temperature (more than 200°C) with retention of lubricating power.
2 tbl
Title | Year | Author | Number |
---|---|---|---|
LUBRICATING COMPOSITION FOR UNIVERSAL SYNTHETIC OIL, CAPABLE OF OPERATING IN GAS-TURBINE ENGINES AND HELICOPTER GEAR ASSEMBLIES, AS WELL AS TURBINE-PROPELLER ENGINES AND TURBINE-PROPELLER-FAN MOTORS OF AIRPLANES | 2010 |
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LUBRICATING COMPOSITION OF SYNTHETIC COMPRESSOR OIL FOR USE IN HIGH-PRESSURE COMPRESSORS | 2013 |
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Authors
Dates
2010-04-27—Published
2008-05-06—Filed