ROTATING FUEL NOZZLE FOR GAS TURBINE

PURPOSE: A rotating fuel nozzle for a gas turbine is provided to sequentially supply fuel by ignition, acceleration, and fixation steps through each orifice using a fuel injection structure formed in a step shape. CONSTITUTION: A rotating fuel nozzle for a gas turbine comprises a fuel injection hole...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MIN, SEONG GI, KIM, YOU IL, YOU, GYONG WON, LEE, DONG HUN
Format:	Patent
Sprache:	eng ; kor
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 SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF WEAPONS
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