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:
Mar. 26, 2024

Filed:

Aug. 05, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Baha Suleiman, Schenectady, NY (US);

Hatem Selim, Schenectady, NY (US);

Assignee:

GE INFRASTRUCTURE TECHNOLOGY LLC, Greenville, SC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/30 (2006.01); F02C 7/22 (2006.01); F02C 9/40 (2006.01); F23K 5/12 (2006.01);
U.S. Cl.
CPC ...
F02C 3/30 (2013.01); F02C 7/22 (2013.01); F02C 9/40 (2013.01); F23K 5/12 (2013.01); F05D 2240/36 (2013.01); F05D 2260/99 (2013.01); F23K 2300/103 (2020.05);
Abstract

A gas turbine engine includes a first combustor having a first fuel nozzle, wherein the first fuel nozzle is configured to supply a water fuel emulsion into the first combustor. The water fuel emulsion includes a water-in-fuel (WIF) emulsion having a plurality of water droplets dispersed in a fuel, wherein the plurality of water droplets is configured to vaporize within the fuel to cause micro-explosions to atomize the fuel, and the atomized fuel is configured to combust to generate a combustion gas. The gas turbine engine further includes a turbine driven by the combustion gas from the first combustor.


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