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:
Sep. 29, 2026

Filed:

Feb. 07, 2024
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Brandon W. Miller, Middletown, OH (US);

Andrew Hudecki, Milford, OH (US);

Ryan T. Roehm, West Chester, OH (US);

Ravindra Shankar Ganiger, Bengaluru, IN;

Assignee:

GENERAL ELECTRIC COMPANY, Evendale, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/20 (2006.01); F01M 11/00 (2006.01); F16H 57/04 (2010.01);
U.S. Cl.
CPC ...
F01D 25/20 (2013.01); F16H 57/0435 (2013.01); F16H 57/0442 (2013.01); F01M 2011/0095 (2013.01); F05D 2260/98 (2013.01);
Abstract

A lubrication system for a turbine engine having one or more rotating components. The lubrication system includes a primary reservoir that stores a lubricant therein. A primary lubrication system supplies the lubricant from the primary reservoir to the one or more rotating components during normal operation of the turbine engine. An auxiliary lubrication system includes an auxiliary reservoir in fluid communication with the primary reservoir and the one or more rotating components. The auxiliary reservoir receives the lubricant from the primary reservoir and is positioned at substantially a six o'clock position of the turbine engine. The auxiliary lubrication system supplies the lubricant from the auxiliary reservoir to the one or more rotating components based on at least one of a pressure of the lubricant in the primary lubrication system, a pressure of fuel in the turbine engine, or a pressure of hydraulics of the turbine engine.


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