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:
Feb. 04, 2025

Filed:

Sep. 13, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Baha Suleiman, Dammam, SA;

Hatem M. Selim, Dammam, SA;

Majed Sammak, Dammam, SA;

Alaaeldin Elsaeed Dawood, Dammam, SA;

Abdurrahman Abdallah Khalidi, Dubai, AE;

Assignee:

GE Infrastructure Technology LLC, Greenville, SC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/40 (2006.01); F02C 3/30 (2006.01); F02C 7/224 (2006.01);
U.S. Cl.
CPC ...
F02C 9/40 (2013.01); F02C 3/30 (2013.01); F02C 7/224 (2013.01); F05D 2260/213 (2013.01);
Abstract

Liquid fuel systems and methods are provided. A liquid fuel system includes a mixing unit and a plurality of liquid fuel supply systems. Each liquid fuel supply system is fluidly coupled to the mixing unit. The liquid fuel system further includes a controller communicatively coupled to the mixing unit and the plurality of liquid fuel supply systems. The controller includes memory and one or more processors. The memory stores instructions that when executed by the one or more processors cause the liquid fuel system to perform operations including providing one or more liquid fuels from the plurality of liquid fuel supply systems to the mixing unit. The operations further include mixing, with the mixing unit, the one or more liquid fuels to create a liquid fuel mixture. The operations further include providing the liquid fuel mixture to a combustion section of a turbomachine.


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