Combustor with dilution opening

A gas turbine engine includes a compressor section and a combustion section in a serial flow arrangement along an engine centerline, the combustion section having a combustor liner, a dome wall coupled to the combustor liner and a dome inlet in the dome wall, a fuel injector fluidly coupled to the d...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	NAIK PRADEEP, UKANTI PARUMARU, BACCARO MICHAEL T, LAKSHMANAN VARUN S, VISE STEVEN C, BENJAMIN MICHAEL A
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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