A thrust reverser system for a jet engine has a thrust reverser sleeve lock, preferably for each thrust reverser sleeve, that provides at least one of the redundant anti-deployment mechanisms of the thrust reverser. The thrust reverser sleeve lock has a lo...

A cascade type thrust reverser for an air duct of a turbofan engine includes a lock mechanism mounted on a track beam (14L) that supports a translating sleeve. A locking portion (42L) of a lock pin (42) of the lock mechanism is engageable with a slideway (...

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...

The thrust reverser comprises a fan duct (10) defined between an inner skin (21) and an outer skin (9) into which integrates the inner skin (5i) of a sliding cowl (3; 3') in the direct thrust situation, said outer skin (5i) of the fan duct (10) having a ra...