Patents
Patents for F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (6,699)
06/1997
06/04/1997EP0777045A1 Thrust reverser with doors with linked rear panel
05/1997
05/27/1997US5632142 Stationary gas turbine power system and related method
05/22/1997WO1997018389A1 Jet engine thrust reverser having downstream balance-biased buckets
05/21/1997EP0774578A1 Thrust reverser for a turbojet where the reversing shells are balanced to stay in the closed position
05/15/1997DE19542082A1 Pressure-tight swivelling joint
05/15/1997DE19542081A1 Seal for gap between flat side wall and two pivotably connected flaps
05/07/1997EP0771945A1 Thrust reverser with secondary flaps for a turbofan engine
05/03/1997CA2189217A1 Thrust inverter of a double flow turbojet with secondary doors
04/1997
04/29/1997US5623820 Flow control apparatus for gas turbine engine installation pressure relief doors
04/24/1997DE19634296A1 Aircraft fan jet propulsion unit
04/23/1997EP0769617A1 Fairing for the rear part of pylon for a jet engine with a lobe mixer
04/22/1997US5622472 Protective shield for a turbo-engine
04/03/1997WO1997012142A1 Convertible ejector cooled nozzle
04/03/1997WO1997012141A1 Lock for engine thrust reverser
04/03/1997CA2205536A1 Lock for engine thrust reverser
04/01/1997US5615834 For a jet engine
04/01/1997US5615549 Thrust reverser for a fan-type turbojet engine
03/1997
03/26/1997EP0764779A1 Thrust reverser with doors linked to a primary panel
03/26/1997EP0684903B1 Angled i-beam honeycomb structure
03/25/1997US5613636 Axisymmetric nozzles of variable geometry and orientation of the flow which are intended for gas turbine engines
03/20/1997WO1997010426A1 Exhaust device for a turbine engine
03/20/1997WO1997010425A1 Turbojet thrust reverser having doors combined with a primary panel
03/19/1997EP0763654A1 Electro/hydraulic system for a 2 door thrust reverser
03/19/1997EP0763653A1 Thrust reverser door with jet deflection cascade
03/18/1997US5611489 Actuating system for a variable area exhaust nozzle
03/14/1997CA2185300A1 Turbojet thrust reverser having doors associated with a primary panel
03/13/1997WO1997009526A1 Turbojet thrust reverser having doors combined with an upstream scoop panel
03/12/1997EP0761957A1 Thrust reverser for a jet engine with doors linked to a front panel
03/12/1997EP0761956A2 Double lobed mixer for turbofan engine
03/12/1997EP0761947A1 Noise reduction kit for turbofan engine
03/11/1997US5609020 For a jet engine hydraulic thrust reverser synchronization shaft
03/07/1997CA2184675A1 Turbofan thrust reverser with doors associated to a front bucket
03/05/1997EP0739291A4 Engine exhaust gas deflection system
03/01/1997CA2181963A1 Turbofan engine with reduced noise
02/1997
02/25/1997US5605046 Cooled liner apparatus
02/18/1997US5603531 Blind assembly-swivel crossover tube
02/18/1997US5603471 Ducted fan turbine engine nozzle assembly
02/05/1997EP0757170A1 Jet engine thrust reverser with a single door
02/04/1997US5598701 Frangible connection for a thrust reverser for a ducted fan gas turbine
01/1997
01/30/1997WO1997003284A1 Turbofan engine thrust reverser with asymmetrical doors
01/29/1997EP0756078A1 Bypass turbofan engine with thrust reverse deflector doors
01/28/1997US5596870 Gas turbine exhaust liner with milled air chambers
01/23/1997WO1997002419A1 Single-clamshell turbojet thrust reverser
01/22/1997EP0754849A1 Double flux turbine thrust reverser with asymmetric doors
01/15/1997EP0753654A1 Ramjet for supersonic and/or hypersonic vehicle
01/15/1997EP0753653A1 Ramjet for supersonic and/or hypersonic vehicle
01/15/1997EP0683859A4 Turbine engine equipped with thrust reverser.
01/14/1997US5593112 Nacelle air pump for vector nozzles for aircraft
01/14/1997US5592814 Attaching brittle composite structures in gas turbine engines for resiliently accommodating thermal expansion
01/14/1997US5592813 Noise reduction assembly
01/13/1997CA2180818A1 Thrust reverser for bypass turbojet with unsymmetric doors
01/07/1997US5590849 Active noise control using an array of plate radiators and acoustic resonators
01/07/1997US5590520 Method of eliminating mach waves from supersonic jets
12/1996
12/27/1996WO1996041940A1 Supersonic jet with a controllable critical cross section
12/27/1996EP0750107A1 Exhaust nozzle flap
12/24/1996US5586431 Aircraft nacelle ventilation and engine exhaust nozzle cooling
12/18/1996EP0748932A1 Nozzle with a variable geometry throat
12/17/1996US5584447 Noise control using a plate radiator and an acoustic resonator
12/17/1996US5584173 Nozzle seal assembly with removable baseplate
12/05/1996WO1996038661A1 Double door thrust reverser assembly
12/04/1996EP0745530A1 Airborne apparatus for ground erosion reduction
12/03/1996USRE35387 Superfragile tactical fighter aircraft and method of flying it in supernormal flight
12/03/1996US5581054 One-piece engine inlet acoustic barrel
12/03/1996US5579999 Shock-free supersonic elliptic nozzles and method of forming same
11/1996
11/27/1996EP0744544A1 Engine exhaust nozzle seal
11/27/1996EP0744543A1 Cooled gas turbine engine augmentor
11/27/1996EP0692069B1 External flap vectoring mechanism
11/26/1996US5577381 Exhaust nozzle cooling scheme for gas turbine engine
11/20/1996EP0743490A1 Combustion chamber having a multitude of cooling holes which are inclined in varying axial and tangential directions
11/20/1996EP0743443A1 Thrust reverser synchronization shaft lock
11/19/1996US5575147 Compact thrust reverser
11/07/1996WO1996035051A1 Method of eliminating mach waves from supersonic jets
11/05/1996US5571262 Supersonic nozzle for a turbojet engine
10/1996
10/31/1996WO1996034193A1 Thrust reverser mechanism for reducing fan distortion
10/30/1996EP0739291A1 Engine exhaust gas deflection system
10/30/1996CN1134505A Cooled Wall part
10/29/1996US5568724 Turbofan engine with means to smooth intake air
10/23/1996EP0615506B1 Thrust reverser with a planar exit opening
10/22/1996US5566884 Supersonic nozzle for a turbojet engine
10/01/1996US5560198 Cooled gas turbine engine augmentor fingerseal assembly
10/01/1996US5560197 Fixing arrangement for a thermal protection tile in a combustion chamber
09/1996
09/24/1996US5557932 Low thermal stress impingement cooling apparatus
09/10/1996US5553452 Control system for a jet engine hydraulic system
08/1996
08/29/1996WO1996026359A1 Thrust reverser with downstream flaps for turbojet engines
08/28/1996EP0728934A1 Thrust reverser for a turbofan engine
08/28/1996EP0728933A1 Thrust reverser with doors linked to rear panel
08/27/1996US5548954 Turbojet engine thrust reverser with rear support structure
08/22/1996CA2169876A1 Thrust reverser with swinging doors associated with downstream installed panel
08/20/1996US5547130 Lock for an engine thrust reverser
08/14/1996EP0664852B1 Mechanical lock for jet engine thrust reverser
08/14/1996EP0591154B1 Turbofan engine fixed plug noise suppressor
08/07/1996EP0725209A1 Sealing ring between an air inlet and a fan shroud of a fan engine
08/06/1996US5542607 Supersonic nozzle, in particular for a turbojet engine
07/1996
07/24/1996EP0723075A2 Thermal shield for axisymmetric vectoring nozzle
07/16/1996US5535585 For a gas turbine engine
07/11/1996WO1996020867A1 Fluidic control thrust vectoring nozzle
06/1996
06/27/1996WO1996019656A1 Compact thrust reverser
06/27/1996WO1996019641A1 Protective shield for a turbomachine
06/26/1996EP0718486A2 Jet engine thrust reverser with perforated inner cover
06/26/1996EP0718471A1 Containment ring for a turbomachine
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