The objective of this eighteen-month program were to further develop two low-emission combustors-the prechamber combustor and the modified conventional combustor to install them in a Detroit Diesel Allison Model 250-C20B engine, and to evaluate their performance in an engine environment. The combustors were to retain the 50% overall reduction in gas turbine mass emissions with no increase in any individual pollutant when tested over a typical Army light observation helicopter (LOH) duty cycle.


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    Titel :

    Low-Emissions Combustor Demonstration


    Beteiligte:
    D. L. Troth (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    405 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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