PREMIXED FUEL NOZZLE

PREMIXED FUEL NOZZLE A fuel injector assembly (70) for a gas turbine engine (10) is generally provided. The first fuel injector (100) includes a first centerbody (110) surrounding a first walled fuel injection circuit (120). A first fuel injection port (130) is extended at least partially radially t...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Naik, Pradeep, Patra, Ajoy, Lind, David Albin, Mishra, Ranjeet Kumar, Boardman, Gregory Allen, Boehm, Randall Charles
Format:	Patent
Sprache:	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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