A thrust reverser for a nacelle of an aircraft turbojet engine is provided that includes a thrust reverser cowl movable along a direction parallel to a longitudinal axis of the nacelle and a variable section outlet nozzle extending from the thrust reverser cowl. The thrust reverser further includes an actuator, a first locking device to lock the thrust reverser cowl, a second locking device to lock the variable section outlet nozzle, and a reset lever. The reset lever is pivotally driven by a locking pin secured to the cowl and pivots from a rest position to a reset position.
Thrust reverser for a nacelle of an aircraft turbojet engine
2019-10-29
Patent
Electronic Resource
English
TURBOJET ENGINE NACELLE COMPRISING A THRUST REVERSER DRIVE MECHANISM
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