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:
Apr. 19, 2022

Filed:

Dec. 04, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Eloise Brightwell, West Chester, OH (US);

Douglas M. Fortuna, West Chester, OH (US);

Gilbert Henry Badeer, West Chester, OH (US);

Steven Keith Handelsman, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/00 (2006.01); F02C 7/232 (2006.01); F02C 7/22 (2006.01); F02C 9/40 (2006.01); F23R 3/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/232 (2013.01); F02C 7/22 (2013.01); F02C 9/40 (2013.01); F23R 3/36 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2270/07 (2013.01); F05D 2270/08 (2013.01);
Abstract

Methods and apparatus to operate a gas turbine engine with hydrogen gas are disclosed. An example combustor nozzle apparatus of a gas turbine engine includes a first circuit to transport a blend of hydrogen gas, inert gas, and/or other combustible gas from a supply to a gas turbine combustor, the blend of hydrogen gas, inert gas, and/or other combustible gas including between 100% hydrogen gas, 100% inert gas, or 100% other combustible gas, a second circuit to transport water from the supply to the gas turbine combustor, and a nozzle tip. The nozzle tip includes a first outlet in connection with the second circuit to provide the water to the gas turbine combustor, and a second outlet in connection with the first circuit, the second outlet concentrically positioned within the first outlet to provide the blend of hydrogen gas, inert gas, and/or other combustible gas to the gas turbine combustor.


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