COMBUSTOR WITH DILUTION OPENINGS

A gas turbine engine (10) including a compressor section (12) and a combustion section (14) in serial flow arrangement along an engine centerline (21), the combustion section having an annular dome wall circumscribing the engine centerline; an annular combustor liner extending from the annular dome...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BENJAMIN, Michael, NAIK, Pradeep, VISE, Steven, VUKANTI, , Perumallu, BUCARO, Michael, LAKSHMANAN, Varun
Format:	Patent
Sprache:	eng ; fre ; ger
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
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