#F02K1/1223

MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS AND METHODS

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) c…

DRIVE·Mar 11·1 min read

F02K1/1223 ROHR INC [US]

Device for feeding cooling air to flap nozzle

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 l…

DRIVE·Jul 13·1 min read

F02K1/1223 SNECMA MOTEURS [FR]

Apparatus to reduce turbine engine nozzle base sheet stresses

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…

DRIVE·May 4·1 min read

F02K1/1223 GEN ELECTRIC [US]

Convergent-divergent turboreactor nozzle

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 t…

DRIVE·Feb 16·1 min read

F02K1/1223 SNECMA MOTEURS [FR]