A lock system (120) for an aircraft thrust reverser includes a lock member (122) translatable between a locked position, in which the lock member is extended for preventing deployment of the thrust reverser by the lock member blocking the path of a movable...

The reverser has sliding doors (10a, 10b) movable between opening and closing positions and controlled by electric motors (14a, 14b) assembled on ordering black boxes (18a, 18b) that are connected to an electronic computer with a full authority (20). Locki...

The reverser has a turntable maintenance (30) that swivels between two positions. A turntable prohibits a hand drive operation in case of a manual operation of a moving part (12) e.g. sliding door while authorizing an electric drive and vice-versa when the...

In a thrust reverser of a turbofan engine comprising, in an annular section of an outer cowling, a plurality of movable doors (2, 3) which, in an inactive position during direct jet operation, close off passages separating rigid beams, there is provided, b...

The thrust reverser door (2) emergency locking system comprises a latch (13) having a self-locking profile hook (12) capable of engaging a door locking interface (10) in the event of failure of normal locking systems. The latch (13) is urged against the in...

A thrust reverser actuator lock mechanism comprising a rotatable shaft (12), rotation of which in one direction from a rest position drives an associated thrust reverser from a stowed position towards an operative position in use, retractable abutment mean...