Turbofan engine

A turbofan engine (100) comprises a nacelle (121) and an engine core having a core cowling (124). The internal surface of the nacelle and the external surface of the core cowling define a bypass duct having an exhaust end defining a bypass duct exit plane (123) generally normal to the longitudinal a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Christopher A Mosley, Nicholas Grech, John R Wells
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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