GAS TURBINE ENGINE COMBUSTOR WITH A SET OF DILUTION PASSAGES

A combustor comprising a dome wall, an annular liner, a combustion chamber, a set of fuel cups, and a set of dilution passages for each fuel cup of the set of fuel cups. The set of fuel cups circumferentially spaced along the dome wall relative to the combustor centerline. The set of dilution passag...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Naik, Pradeep, Vukanti, Perumallu, Chiranthan, R Narasimha, Patra, Ajoy, Badhuk, Pabitra, Pal, Sibtosh, Bucaro, Michael T, Sinha Roy, Arijit, Chakraborty, Aritra, Benjamin, Michael A, Panduri, Bhavya Naidu
Format:	Patent
Sprache:	eng
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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