The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 23, 2020

Filed:

Dec. 22, 2017
Applicants:

Exxonmobil Research and Engineering Company, Annandale, NJ (US);

General Electric Company, Schenectady, NY (US);

Inventors:

Meredith R. Gibson, Philadelphia, PA (US);

Angela S. Galiano-Roth, Mullica Hill, NJ (US);

Jessica L. Prince, Cherry Hill, NJ (US);

Andrea B. Wardlow, Newark, DE (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C10M 169/04 (2006.01); C10M 171/02 (2006.01);
U.S. Cl.
CPC ...
C10M 169/042 (2013.01); C10M 171/02 (2013.01); C10M 2203/1006 (2013.01); C10M 2203/1025 (2013.01); C10M 2205/0285 (2013.01); C10M 2205/173 (2013.01); C10M 2205/223 (2013.01); C10M 2207/2835 (2013.01); C10M 2207/2855 (2013.01); C10N 2230/02 (2013.01); C10N 2230/04 (2013.01); C10N 2230/18 (2013.01); C10N 2230/54 (2013.01); C10N 2230/74 (2013.01); C10N 2240/12 (2013.01); C10N 2240/14 (2013.01);
Abstract

This disclosure relates to a low viscosity lubricating turbine oil having a composition comprising a lubricating oil base stock, as a major component, and one or more lubricating oil additives, as minor components. The lubricating turbine oil has a kinematic viscosity of about 16 cSt to about 22 cSt at 40° C., a density of about 0.8 g/ml to about 0.9 g/ml, and an absolute evaporation loss at 150° C. of less than about 4%. This disclosure also relates to a method for improving energy efficiency in a turbomachine lubricated with the low viscosity lubricating turbine oil. This disclosure further relates to a method for improving energy efficiency while maintaining or improving deposit control and lubricating oil additive solvency in a turbomachine lubricated with the low viscosity lubricating turbine oil. This disclosure yet further relates to a method for improving solubility, compatibility and dispersancy of polar additives in the low viscosity lubricating turbine oil.


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