PIVOT DOOR THRUST REVERSER WITH VARIABLE AREA NOZZLE

A gas turbine engine includes a nacelle assembly having a core nacelle defined about an engine axis and a fan nacelle assembly mounted at least partially around the core nacelle to define a fan bypass flow path. The fan nacelle assembly includes a fan duct nacelle section and a fan nozzle nacelle se...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SAWYERS-ABBOTT, NIGEL DAVID, LOFFREDO, CONSTANTINO V
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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