Gas turbine engine combustor can with trapped vortex cavity

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Bibliographische Detailangaben
Hauptverfasser:	JOSHI NARENDRA DIGAMBER, HAYNES JOEL MEIER, FEITELBERG ALAN S, BURRUS DAVID LOUIS
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR 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 METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN WEAPONS
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