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:
Jul. 14, 2026

Filed:

Dec. 12, 2023
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

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

Arthur W. Sibbach, Boxford, MA (US);

Andrew Hudecki, Milford, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Evendale, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/20 (2006.01); F01M 1/12 (2006.01); F01M 11/06 (2006.01);
U.S. Cl.
CPC ...
F01D 25/20 (2013.01); F01M 2001/123 (2013.01); F01M 2011/068 (2013.01); F05D 2220/323 (2013.01); F05D 2270/301 (2013.01);
Abstract

A method of operating a lubrication system for a turbine engine having a fan and one or more rotating components. The lubrication system includes a primary lubrication system and an auxiliary lubrication system. The method includes supplying lubricant to the one or more rotating components from the primary lubrication system during a normal operation of the turbine engine, determining whether at least one of a fuel pressure is less than a fuel pressure threshold or a hydraulic pressure is less than a hydraulic pressure threshold, and activating the auxiliary lubrication system to supply the lubricant to the one or more rotating components from the auxiliary lubrication system when the fuel pressure is less than the fuel pressure threshold or the hydraulic pressure is less than the hydraulic pressure threshold.


Find Patent Forward Citations

Miller, Brandon. (2026). Method of operating a lubrication system for a turbine engine (U.S. Patent No. 12680474). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12680474

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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