Combustion nozzle fluidic injection assembly

A fluid flow system for use with a gas turbine engine includes an exhaust nozzle (40), a primary air supply valve (24), a distribution manifold (26) connected to the primary fluid supply valve (24) and in fluid communication therewith, and a plurality of fluid injector assemblies (42) positioned at...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HINKEY, JOHN, BERG, GERALD R, LIDSTONE, GARY L, MESSERSMITH, NATHAN L
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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