An articulating exhaust nozzle thrust reverser includes an outer articulating panel (210) comprising an outer skin (212) and an outer thrust reverser door (214) and an inner articulating panel (220) comprising a forward inner skin (222), an aft inner skin ...

The device has a conduit (30) connecting a divergent flap (21) of a convergent-divergent duct (1) to a cooling air source (31). The conduit has a telescopic portion (32) situated between two knuckle links (33, 34) and comprising two tubes (32A, 32B) slidin...

An assembly for a gas turbine engine exhaust nozzle includes a backbone and a base sheet (106) configured to couple to the backbone. The base sheet includes at least one relief cut (200) and a pair of circumferentially-spaced sides (114 and 116) coupled to...

The nozzle (1) has follow-up divergent flaps (4b) interposed between control flaps and having a structure in box with internal and external radial walls. The divergent flaps provide lateral openings to deliver cooling air in direction of an internal side o...