Axially staged premixed combustion chamber

The invention relates to an axially staged premixed combustion chamber. A combustor for a gas turbine includes a plurality of radially outer nozzles arranged in an annular array, each of the radially outer nozzles having an outlet end located to supply fuel and/or air to a first combustion chamber....

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	VALEEV ALMAZ, ANATOLIEVICH MESHKOV SERGEY, MITROFANOV ALEXANDROVICH VALERY, HADLEY MARK, WIDENER STANLEY, MYERS GEOFFREY
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING BURNERS 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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