THRUST REVERSER TERTIARY LOCKING SYSTEM

A nacelle (16) for a gas turbine engine, comprising a thrust reverser movable between a stowed position and a deployed position, and a locking system (30) configured to selectively prevent movement of the thrust reverser from the stowed position, the locking system (30) comprising a locking mechanis...

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Bibliographische Detailangaben
Hauptverfasser:	SOMERFIELD, Michael Paul, MORGAN, Antony
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION ENGINES ENGINE PLANTS IN GENERAL HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A nacelle (16) for a gas turbine engine, comprising a thrust reverser movable between a stowed position and a deployed position, and a locking system (30) configured to selectively prevent movement of the thrust reverser from the stowed position, the locking system (30) comprising a locking mechanism (32) and an actuator (42) configured to actuate the locking mechanism (32), wherein the locking mechanism (32) is positioned aft of a blade-off zone (23) defined across the nacelle (16) and the actuator (42) is positioned fore of, or at least partially within, the blade-off zone (23).