A combustor assembly includes a combustor vessel having a wall, a proximate end defining an opening and a closed distal end opposite said proximate end. A manifold is carried by the proximate end. The manifold defines a combustion products exit. The combustion products exit being axially aligned with a portion of the closed distal end. A plurality of combustible reactant ports is carried by the manifold for directing combustible reactants into the combustion vessel from the region of the proximate end towards the closed distal end.


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    Titel :

    Stagnation Point Reverse Flow Combustor for a Combustion System (2007)


    Beteiligte:
    B. T. Zinn (Autor:in) / Y. Neumeier (Autor:in) / J. M. Seitzman (Autor:in) / J. Jagoda (Autor:in) / B. A. Hashmonay (Autor:in)

    Erscheinungsdatum :

    2005


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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