FIELD: aircraft engineering and lubricants.
SUBSTANCE: lubricant of invention is composed of, wt %: N-phenyl(nonoxy)-di(anilinophenoxy)silane 0.4-0.6, N-phenyl-α- naphthylamine 0.5-0.7, p,p'-diisooctyldiphenylamine 1.3-1.5, tricresyl phosphate 2.8-3.2, benzotriazole 0.05-0.1, polyethylsiloxane liquid 17-20, and boronized pentaerythritol ester of synthetic fatty acids C5-C9-fraction to 100.
EFFECT: improved thermooxidative resistance and lubricating properties.
1 tbl
Title | Year | Author | Number |
---|---|---|---|
LUBRICATING COMPOSITION | 1984 |
|
SU1840591A1 |
LUBRICATION COMPOSITION | 1988 |
|
SU1840621A1 |
LUBRICATION COMPOSITION | 1987 |
|
SU1840596A1 |
LUBRICATION COMPOSITION | 1987 |
|
SU1840595A1 |
AIRCRAFT OIL | 1987 |
|
SU1840598A1 |
LUBRICATION COMPOSITION | 1987 |
|
SU1840695A1 |
LUBRICATING COMPOSITION | 0 |
|
SU572488A1 |
LUBRICATING COMPOSITION | 0 |
|
SU739083A1 |
LUBRICATING COMPOSITION | 0 |
|
SU704980A1 |
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 |
|
RU2452767C1 |
Authors
Dates
2007-09-10—Published
1984-11-16—Filed