The lock is for a bypass aircraft gas turbine thrust reverser with guides (60) for the movable reverser sections (50) having rails (64) attached to the movable sections (50) and slides (62) attached to longitudinal beams (36). The lock has locking assembli...

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...

The thrust reversal system, comprising grids with sliding covers (6) in the engine nacelles, and shutters to deflect a by-pass air flow towards the grids, has the covers actuated by drives (30) in line with the axes of the slideways (14a, 14b, 14c) guiding...