SYSTEM FOR LOCKING A THRUST REVERSER WITH FLAPS, COMPRISING LOCKS FOR AN INTERMEDIATE OPENING POSITION

摘要

The present disclosure relates to a system for locking the position of the flaps of a thrust reverser of a turbojet nacelle, said flaps being controlled by actuators, each one swinging about a tranverse pivot in order to partially close off the air stream so as to guide it forwards, further including locks for locking the flaps in an intermediate opening position, between the closed position and the open position.

主权项

1. A thrust reverser for a nacelle of a turbojet engine comprising doors controlled by actuators, the doors tilting about a transverse pivot in order to partially close air flow so as to direct the air flow forwards, and comprising a system for locking the position of the doors, wherein the locking system comprises:
locks configured to lock an intermediate opening position of the doors, between a closed position and a fully deployed position, where an actuation of said locks blocks said intermediate opening position of the doors without biasing the actuators of the doors in order to hold the intermediate opening position.