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:
Jun. 09, 2026

Filed:

Feb. 03, 2025
Applicant:

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

Inventors:

Christian Xavier Stevenson, Mountville, SC (US);

Joel Meador Hall, Simpsonville, SC (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/18 (2006.01); F02C 3/16 (2006.01); F02C 3/30 (2006.01); F23R 3/12 (2006.01); F23R 3/16 (2006.01); F23R 3/28 (2006.01);
U.S. Cl.
CPC ...
F23R 3/18 (2013.01); F02C 3/16 (2013.01); F02C 3/30 (2013.01); F23R 3/12 (2013.01); F23R 3/16 (2013.01); F23R 3/28 (2013.01);
Abstract

A system includes at least one component of a turbine section. The at least one component includes a fuel port formed into a wall of the at least one component, which is configured to inject fuel into a chamber of the turbine section. The at least one component also includes an inert gas port formed into the wall upstream of the fuel port. The inert gas port is configured to inject an inert gas to flow at least partially around the injected fuel into a buffer region downstream from the fuel port. The presence of the inert gas in the buffer region may mitigate an ignition of the fuel near the surface of the wall downstream of the fuel port (e.g., flame anchoring) and/or help to lift the flame from the ignited fuel into the hot gas flow path.


Find Patent Forward Citations

Quick Actions:

Stevenson, Christian. (2026). System and method for fuel and inert gas injection in turbine section of gas turbine engine (U.S. Patent No. 12650226). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12650226

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