A gas engine turbine comprising a thrust augmentation system

One embodiment of the present invention is a gas turbine engine (10), comprising a thrust augmentation system (64) with a fluidic flameholder, which ejects the fuel (82) by generating an obstruction to the exhaust flow of the turbine engine.

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Bibliographische Detailangaben
Hauptverfasser:	EIFERT, ANDREW, VETTERS, DANIEL KENT, AUKER, BRADLEY EUGENE, OECHSLE, VICTOR LEWIS
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	One embodiment of the present invention is a gas turbine engine (10), comprising a thrust augmentation system (64) with a fluidic flameholder, which ejects the fuel (82) by generating an obstruction to the exhaust flow of the turbine engine.