Gas Turbine Slinger Combustor

A slinger combustor for a gas turbine according to an embodiment of the present invention comprises a rotating fuel nozzle for injecting fuel supplied through a hollow main shaft into a combustion chamber, an outer liner, and an inner liner, and also includes an air collection inducing means located...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KIM JAI HO, KANG YOUNG SEOK, KIM HYUNG MO, PARK POO MIN
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 WEAPONS
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