Multi-stage multi-plane combustion system for a gas turbine engine

A low emissions combustion system with a plurality of tangential fuel injectors to introduce a fuel/air mixture at the combustor dome end (43) of an annular combustion chamber (39) in two spaced injector planes (3,4). Each of the spaced injector planes includes multiple tangential fuel injectors del...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	WILLIS, JEFFREY W, PONT, GUILLERMO, MCKEIRNAN, ROBERT D. JR, TOBY, BENJAMIN E
Format:	Patent
Sprache:	eng ; fre ; ger
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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