THRUST REVERSER SYSTEM AND ENGINE ASSEMBLY WITH LOCKOUT MECHANISM

An engine assembly having a turbine engine, a nacelle surrounding the turbine engine and defining an annular bypass duct between the nacelle and the turbine engine and extending through the turbofan engine to define a generally forward-to-aft bypass airflow path, a thrust reverser having at least on...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	WILLETT, KENNETH R
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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