FIELD: chemistry.
SUBSTANCE: invention relates to composition of lubricating oil for gas turbines which contains the following, wt %: 2,6-di-tert-butyl-para-cresol 0.1-2.0; amino-derivative antioxidant additive 0.1-2.0; mixture of mono- and di-glycerides of β-(3,5-di-tert-butyl-4-oxyphenyl)propionic acid 0.5-2.0; liquid chlorinated paraffins 0.2-0.6; polymethylsiloxane 0.001-0.005; light isoparaffin oil 10.0-45.0 and mineral oil - the balance.
EFFECT: reduced volatility and corrosive action on silver.
2 cl, 2 tbl, 3 ex
Title | Year | Author | Number |
---|---|---|---|
LUBRICATING OIL FOR GAS TURBINES | 2012 |
|
RU2505591C1 |
LUBRICATING OIL FOR GAS TURBINES | 1997 |
|
RU2125084C1 |
LUBRICANT OIL FOR GAS TURBINE | 1996 |
|
RU2109800C1 |
LUBE OIL FOR GAS TURBINES | 2000 |
|
RU2185423C2 |
LUBRICANT OIL FOR GAS TURBINES | 1997 |
|
RU2125588C1 |
LUBRICANT COMPOSITION | 2009 |
|
RU2398009C1 |
LUBRICANT COMPOSITION OF HIGH-TEMPERATURE OIL FOR HEAT-STRESSED GAS-TURBINE ENGINES OF SUPERSONIC AIRCRAFT | 2010 |
|
RU2476587C2 |
LUBRICATING OIL FOR GAS TURBINES | 1996 |
|
RU2086609C1 |
LUBRICANT COMPOSITION OF SYNTHETIC TURBINE OIL FOR STEAM TURBINE PLANTS | 2013 |
|
RU2550137C2 |
HYDRAULIC LIQUID | 2009 |
|
RU2430146C2 |
Authors
Dates
2014-01-27—Published
2012-09-06—Filed