MULTITUBE PILOT INJECTOR HAVING A SPLIT AIRFLOW FOR A GAS TURBINE ENGINE

An injector for a combustor of a gas turbine engine is provided with a plurality of air/fuel mixing tubes divided into radially outer and radially inner subsets of air/fuel mixing tubes with a first fuel manifold in fluid communication with the radially outer subset of air/fuel mixing tubes and a se...

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Bibliographische Detailangaben

Hauptverfasser:	HERNANDEZ, Fred, VOGEL, Gregory, CHONG, Gene, SAM, Bernard Tam Yen, KESHAVA-BHATTU, Ramesh, PARADES, David, KALB, Bryan, BRACKETT, James, MCNALLY, Joshua R, YAQUINTO, Matthew, RIZKALLA, Hany
Format:	Patent
Sprache:	eng ; fre
Online-Zugang:	Volltext bestellen
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