Gas turbine engine and methods of controlling emissions therefrom

A gas turbine engine that includes a stage of guide vanes, a compressor downstream from the stage of guide vanes, and a combustor downstream from the compressor. The combustor includes a primary combustion zone and a secondary combustion zone downstream from the primary combustion zone. The primary...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Boyd, Haley Marie, Loeven, II, Robert Joseph, Fuller, Jason Dean
Format: Patent
Sprache:eng
Schlagworte:
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