Fuel combustor, combustion turbine, and method of combustion

The RRQL combustor addresses ammonia's combustion challenges by incorporating a relaxation zone to reduce NOx emissions, achieving significantly lower emissions than conventional systems, making ammonia a viable decarbonization fuel.

WO2026010605A9PCT designated stage expired Publication Date: 2026-07-02GEORGIA TECH RES CORP

Patent Information

Authority / Receiving Office
WO · WO
Patent Type
Applications
Current Assignee / Owner
GEORGIA TECH RES CORP
Filing Date
2024-06-25
Publication Date
2026-07-02

AI Technical Summary

Technical Problem

Ammonia combustion produces significantly higher NOx emissions and poses challenges due to its limited flammability range, lower flame temperature, and slower laminar flame speeds, making it less viable as a decarbonization fuel, and existing combustor designs fail to effectively manage these issues.

Method used

A 'rich-relaxation-quench-lean' (RRQL) combustor design with multiple stages: a fuel-rich combustion zone, a relaxation zone for NOx level relaxation, a quench zone, and a fuel-lean combustion zone, allowing high NOx levels to relax to equilibrium levels before further combustion.

Benefits of technology

The RRQL combustor design effectively reduces NOx emissions to low levels, achieving up to two orders of magnitude lower emissions than conventional systems, without requiring water or steam injection, and is applicable in various power generation and heating applications.

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Abstract

A fuel combustor for nitrogen-containing fuel minimizes NOx emissions from the combustion of nitrogen-containing fuels such as ammonia fuel. A turbine for generating power includes a drivable turbine and at least one of the fuel combustors for nitrogen-containing fuel. Methods of combusting nitrogen-containing fuel with the fuel combustor, minimizing NOx emissions formed by the combustion of nitrogen-containing fuel, and generating power are disclosed.
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