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

An injector (104) for a combustor (1000) of a gas turbine engine is provided with a plurality of air/fuel mixing tubes divided into radially outer (322a) and radially inner (322b) subsets of air/fuel mixing tubes (322) with a first fuel manifold (130) in fluid communication with the radially outer s...

Ausführliche Beschreibung

Gespeichert in:

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
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	An injector (104) for a combustor (1000) of a gas turbine engine is provided with a plurality of air/fuel mixing tubes divided into radially outer (322a) and radially inner (322b) subsets of air/fuel mixing tubes (322) with a first fuel manifold (130) in fluid communication with the radially outer subset of air/fuel mixing tubes and a second fuel manifold (132) in fluid communication with the radially inner subset of air/fuel mixing tubes. Each of the air/fuel mixing tubes of the radially outer subset of air/fuel mixing tubes includes a substantially quadrilateral cross-sectional profile, and each of the air/fuel mixing tubes of the radially inner subset of air/fuel mixing tubes includes a substantially circular cross-sectional profile. Un injecteur pour une chambre de combustion d'un moteur à turbine à gaz est pourvu d'une pluralité de tubes de mélange air/carburant divisés en sous-ensembles radialement externes et radialement internes de tubes de mélange air/carburant avec un premier collecteur de carburant en communication fluidique avec le sous-ensemble radialement externe de tubes de mélange air/carburant et un second collecteur de carburant en communication fluidique avec le sous-ensemble radialement interne de tubes de mélange air/carburant. Chacun des tubes de mélange air/carburant du sous-ensemble radialement externe de tubes de mélange air/carburant comprend un profil de section transversale sensiblement quadrilatéral, et chacun des tubes de mélange air/carburant du sous-ensemble radialement interne de tubes de mélange air/carburant comprend un profil de section transversale sensiblement circulaire.