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:
Nov. 04, 2025

Filed:

Sep. 17, 2024
Applicant:

Solar Turbines Incorporated, San Diego, CA (US);

Inventors:

James Jonathan Underwood, Chula Vista, CA (US);

Christopher Jeremy Wiggins, Newhall, CA (US);

Nathan James Kirksey, San Diego, CA (US);

Darrel Patrick Zeltner, Escondido, CA (US);

Assignee:

Solar Turbines Incorporated, San Diego, CA (US);

Primary Examiner:
Int. Cl.
CPC ...
F02C 9/28 (2006.01);
U.S. Cl.
CPC ...
F02C 9/28 (2013.01); F05D 2240/35 (2013.01);
Abstract

A system for detecting and responding to a flameout condition in a gas turbine engine includes a probe, a spectral data receiver unit, and a flameout relay. The probe detects a radiation from a gaseous content resulting from a combustion reaction within the gas turbine engine. The spectral data receiver unit processes a signal associated with the radiation for four different wavebands and deduces four different current signals. The flameout relay is triggered to move fueling valves to a shutdown state to halt fuel supply into the gas turbine engine based on at least one of: one or more of the four different current signals meet a predefined condition, or a turbine rotor inlet temperature (TRIT) derived or calculated from the four different current signals is below a temperature threshold or a rate of drop of the TRIT is below a rate threshold.


Find Patent Forward Citations

Underwood, James. (2025). System and method for detecting and responding to flameout conditions in gas turbine engines (U.S. Patent No. 12460586). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12460586

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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