BP Turbo Oil 2380 - Aircraft-Type Gas Turbine Lubricant
BP Turbo Oil 2380 gas turbine lubricant is a combination of a highly stable synthetic base fluid and a unique chemical additive package. The combination provides outstanding thermal and oxidation stability to resist deterioration and deposit formation in both the liquid and vapour phases, as well as excellent resistance to foaming.
The effective operating range of BP Turbo Oil 2380 is between -40°C and 204°C. Pour point is -57°C. The product has a high specific heat in order to ensure good heat transfer from oil-cooled engine parts. The high degree of oxidation resistance of BP Turbo Oil 2380 permits long periods of operation without significant increase in viscosity or total acidity.
BP Turbo Oil 2380 is recommended for aircraft gas turbine engines of the turbo-jet, turbo-fan, turbo-prop, and turbo-shaft (helicopter) types in commercial and military service. It also is recommended for aircraft-type gas turbine engines in industrial or marine application.
BP Turbo Oil 2380 is approved against U.S. Military Specification MIL-PRF-23699F-STD.
It is also approved by a wide range of engine and accessory manufacturers including:
Allison Engine Co.
General Electric Company
Pratt & Whitney Group, United Technologies Corp.
Pratt & Whitney, Canada
Excellent thermal and oxidation stability minimizes formation of varnish and sludge deposits
Exceptional fluidity at -40°C enables use in critical applications where other Type II lubricants are excessively viscous.
Excellent load carrying performance increasing the life of bearings, gears and other highly loaded lubricated surfaces.