#F02K1/006

THRUST REVERSER FOR VARIABLE AREA NOZZLE

A variable area nozzle assembly (46) for a gas turbine engine includes a fixed structure (48) surrounding an exhaust duct extending along a nozzle centerline. The fixed structure (48) further includes…

DRIVE·Sep 24·2 min read

F02K1/006 ROHR INC [US]

GAS TURBINE ENGINE EXHAUST NOZZLE AND CORRESPONDING GAS TURBINE ENGINE

A gas turbine engine exhaust nozzle comprises a nozzle body (8) defining a nozzle exit (6). An array of movable slats (16, 18) is disposed round the nozzle exit (6). Flow control walls (20) are fixed …

DRIVE·Jan 16·1 min read

F02K1/006 ROLLS ROYCE PLC [GB]

Nozzle with adjustable throat

The nozzle (20) has a collar (200) placed at inside a frame (21) in upstream of a shroud. The collar comprises two side walls (210, 220) assembled in a pivoting manner in the frame. The walls are conn…

DRIVE·Sep 28·1 min read

F02K1/006 SNECMA PROPULSION SOLIDE [FR]

Vectoring transition duct for turbine engine

A transition duct (112) is provided at the outlet of a turbine engine (10). The transition duct transitions the outlet of the tip turbine engine from round to rectangular. The transition duct also pro…

DRIVE·Jun 15·1 min read

F02K1/006 UNITED TECHNOLOGIES CORP [US]

Variable area throat exhaust nozzle with vectorable sideways shifting of exhaust flow

A nozzle (12) includes a sideways split and aftwardly swept nozzle ramp (18) extends between a fixed lower nozzle wall (16) and a pivotal upper nozzle wall (14) pivotally connected to an aft end (104)…

DRIVE·Mar 29·2 min read

F02K1/006 GEN ELECTRIC [US]

Vectorable nozzle with sideways pivotable ramp

A vectorable nozzle (12) includes a longitudinally extending upper fixed wall (14) spaced upwardly and aftwardly of a longitudinally extending lower fixed wall (16) and an aftwardly swept fixed ramp (…

DRIVE·Mar 1·2 min read

F02K1/006 GEN ELECTRIC [US]

Two-dimensional vectorable single expansion ramp nozzle

A two dimensional gas turbine engine exhaust nozzle (50) includes transversely spaced apart upper and lower convergent and divergent flaps (54, 56) and (58, 60) extending longitudinally in a downstrea…

DRIVE·Dec 21·2 min read

F02K1/006 GEN ELECTRIC [US]

Gas turbine engine two dimensional exhaust nozzle mechanism with reverse exhaust capability

A gas turbine engine exhaust nozzle mechanism, including two side walls (7), two convergent flaps (10, 46), an upper and a lower reverse flow duct (15, 58) and at least one actuator mechanism. The con…

DRIVE·Apr 23·2 min read

F02K1/006 TURBO PROPULSORES IND [ES]