FUEL PREMIXING MODULE FOR GAS TURBINE ENGINE COMBUSTOR

An apparatus for mixing gas and fuel comprises a premixer including a first axial inflow swirler having a first plurality of vanes. The premixer includes a housing having a longitudinal centerline and a plurality of spaced fueling passages that allow the discharge of fuel onto the first axial inflow...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	RAZDAN, MOHAN, K, MARSHALL, ANDRE, W, RIZK, NADER, K, CHIN, JUSHAN
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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