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. 24, 2025

Filed:

Apr. 12, 2024
Applicant:

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

Inventors:

Joel Meador Hall, Simpsonville, SC (US);

John Farrior Woodall, Greer, SC (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/18 (2006.01); F23R 3/20 (2006.01); F23R 3/22 (2006.01);
U.S. Cl.
CPC ...
F23R 3/18 (2013.01); F23R 3/20 (2013.01); F23R 3/22 (2013.01);
Abstract

A system includes a gas turbine having a turbine shaft disposed along a rotational axis, a turbine casing disposed circumferentially about the turbine shaft, a combustion gas path disposed between the turbine shaft and the turbine casing, and a turbine stage disposed in the combustion gas path. The turbine stage includes a plurality of turbine vanes disposed upstream from a plurality of turbine blades. The gas turbine includes an isothermal expansion system coupled to the turbine stage, wherein the isothermal expansion system includes a plurality of flame stabilizers configured to vary axial positions of combustion within a turbine stage expansion of the turbine stage to reduce temperature variations over the turbine stage expansion. The flame stabilizers are disposed in different axial positions over an axial length between leading and trailing edges of the turbine blades, wherein at least one flame stabilizer is coupled to a plurality of the turbine blades.


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