Gaseous (NOx, CO) and non-volatile particulate matter (nvPM) emissions from a small-core high-pressure Axially Controlled Stoichiometry (ACS) combustor are reported. NOx and CO emissions characteristics are similar to a previous version of ACS combustor. Emissions of nvPM at low-power (fuel-rich front end) was found to procude significantly higher nvPM emissions compared to a high-power configuration (fuel-lean front end). NOx emissions for the ACS combustor were 82-89% below the ICAO CAEP/6 standard for aggressive NASA N+3 high-pressure cycles based on NOx correlations developed from experimental measurements.


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    Titel :

    Emission Characteristics of an Axially Staged Sector Combustor for a Small Core High OPR Subsonic Aircraft Engine


    Beteiligte:
    He, Zhuohui J. (Autor:in) / Capil, Tyler G. (Autor:in) / Podboy, Derek P. (Autor:in) / Chang, Clarence T. (Autor:in) / Smith, Lance L. (Autor:in)

    Kongress:

    AIAA SciTech Forum ; 2020 ; Orlando, FL, United States


    Erscheinungsdatum :

    06.01.2020


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





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