• Login
    View Item 
    •   DSpace Home
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    •   DSpace Home
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Reducing NOx Emissions in Ammonia Combustors

    Thumbnail
    View/Open
    gtp-25-1283.pdf (2.591Mb)
    Date
    2026
    Author
    Rana, Satyendra
    Papas, Paul
    Smith, Lance L.
    Sung, Chih-Jen
    Metadata
    Show full item record
    Abstract
    Abstract. Ammonia continues to attract growing interest as a carbon-neutral replacement fuel, motivating numerous research efforts toward understanding fundamental ammonia combustion characteristics. A major challenge for the use of ammonia is the development of combustor technologies for mitigating potentially high NOx emissions from the fuel-bound nitrogen chemical pathways to acceptable levels. Our work focuses on a staged rich-burn/quick-quench/lean-burn (RQL) combustor architecture for minimizing the NOx emission levels through burning fuel-rich in the primary stage to form combustion products containing significant levels of hydrogen in addition to nitrogen and water with minimal NOx formation. The subsequent quench and burnout stages of the combustor must then quickly burn residual hydrogen with flame-temperatures moderated by nitrogen and water forming in the first stage. Chemical reactor network (CRN) modeling was used to understand and identify optimal stoichiometry and residence times in each stage for minimizing NOx emissions and to quantify pressure and temperature effects. Reducing the overall NOx emissions requires relatively long residence times in the primary stage to achieve near equilibrium NO levels due to kinetically controlling processes. For conditions relevant to gas turbines (e.g., 30 atm), our work indicates that NOx emissions below 20 ppm are theoretically achievable in a staged RQL combustor architecture. However, these emission predictions significantly depend on the accuracies of currently available chemical kinetic mechanisms which have not been extensively validated under elevated pressure and temperature conditions relevant to gas turbines.
    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4314855
    Collections
    • Journal of Engineering for Gas Turbines and Power

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV
     

     

    Browse

    All of DSpaceCommunities & CollectionsBy Issue DateAuthorsTitlesSubjectsThis CollectionBy Issue DateAuthorsTitlesSubjects

    My Account

    LoginRegister

    Statistics

    View Usage Statistics

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV