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)
05/1994
05/24/1994US5313788 Thrust reversing arrangement for a long duct mixed flow exhaust turbofan engine
05/19/1994DE4238633A1 Radial displacement control for jet missile - uses 4 steel rudders rotatable about common axis and axially adjustable
05/17/1994US5311774 Method and installation for generating a high mass flow of unpolluted high enthalpy air
05/17/1994CA1329487C Turbojet thrust reverser with balanced pivoting doors
05/10/1994US5310586 Angled I-beam honeycomb structure
05/10/1994US5310117 Jet engine provided with a thrust reverser
05/10/1994US5309711 Cascade type thrust reverser for fan jet engines
05/04/1994EP0595753A1 Divergent slave petal for variable geometry exhaust nozzles
05/04/1994EP0595693A1 Metal jacket subjected to high temperature gradients
04/1994
04/27/1994EP0442899B1 Vane-type thrust vectoring nozzle
04/26/1994US5305599 Pressure-ratio control of gas turbine engine
04/20/1994EP0592526A1 Apparatus and method for suppressing sound in a gas turbine engine powerplant.
04/20/1994EP0539359B1 Flame tube with a cooled supporting frame for a heat-resistant lining
04/19/1994US5303545 Pressure based close loop thrust control in a turbofan engine
04/13/1994EP0591154A1 Turbofan engine fixed plug noise suppressor.
03/1994
03/31/1994WO1994007018A1 Mechanical lock for jet engine thrust reverser
03/29/1994US5297388 Aircraft power plant
03/29/1994US5297387 Deflector edge for a thrust reverser
03/22/1994US5295645 Aircraft variable geometry nozzle
03/15/1994US5294055 Rotatable arms for thrust vectoring and changing the area of a nozzle throat
03/15/1994CA1327705C Thrust reverse with mobile deviation edges
03/09/1994EP0586000A1 Non-metallic thermally conductive honeycomb thrust reverser inner wall
03/08/1994US5292069 Convertible plug nozzle
03/08/1994US5291672 For mixing airflow with exhaust gases generated in a gas turbine engine
02/1994
02/22/1994US5288020 Seal arrangement for adjoining walls of a propulsion nozzle of an engine
02/15/1994US5285637 Seal centering and restraining device for an axisymmetric convergent/divergent nozzle
02/09/1994EP0582424A1 Noise-suppressed exhaust nozzles for jet engines
02/09/1994EP0582115A1 Propulsive nozzle
02/08/1994US5284015 Turbojet engine thrust reverser with directional control
02/08/1994CA1326767C Jet engine provided with a thrust reverser
02/03/1994WO1994002732A1 Divergent seal arrangement for a convergent/divergent nozzle
02/03/1994WO1994002731A1 Flap hinge arrangement for a convergent/divergent nozzle
01/1994
01/26/1994EP0580352A1 Lock for an engine thrust reverser
01/25/1994US5280704 Lock for a thrust reverser mechanism, a thrust reverser mechanism, and a thrust reverser
01/19/1994EP0578951A1 Jet engine
01/18/1994US5279127 Annular gas turbine combustor
12/1993
12/28/1993US5273213 Variable area nozzle for turbomachines
12/22/1993EP0574730A1 Thrust reversing device for jet aircraft engines
12/21/1993US5271222 Jet propulsion powerplants
12/14/1993US5269467 Vectoring exhaust nozzle seal and flap retaining apparatus
12/14/1993US5269466 Gas turbine engine including a variable area nozzle
12/14/1993US5269139 Jet engine with noise suppressing mixing and exhaust sections
12/14/1993US5269136 Sub-idle stability enhancement and rotating stall recovery
12/14/1993US5269132 From a tail pipe of a jet engine
12/07/1993US5267760 Locking mechanism
12/07/1993US5267438 Thrust reverser for a turbofan engine
12/07/1993US5267436 Vectoring nozzle control of gas turbine engines
12/07/1993US5267435 Thrust droop compensation method and system
12/07/1993CA1324999C Bodies with reduced surface drag
11/1993
11/30/1993US5265807 Aerodynamic stiffening ring for an aircraft turbine engine mixer
11/30/1993US5265412 Self-accommodating brush seal for gas turbine combustor
11/30/1993US5265409 Uniform cooling film replenishment thermal liner assembly
11/30/1993US5265408 Exhaust eductor cooling system
11/18/1993DE4314160A1 Joint for components for gas turbine - has joint section, located in joint channel, which is formed by merging grooves in components
11/16/1993US5261606 Crossed strut divergent flap vectoring mechanism
11/16/1993US5261605 Axisymmetric nozzle with gimbled unison ring
11/16/1993US5261604 Yaw vectoring blade
11/16/1993US5261229 Noise-suppressed exhaust nozzles for jet engines
11/16/1993US5261227 Variable specific thrust turbofan engine
11/11/1993WO1993022552A1 Apparatus and method for suppressing sound in a gas turbine engine powerplant
11/09/1993US5259188 Method and system to increase stall margin
11/09/1993US5259187 Method of operating an aircraft bypass turbofan engine having variable fan outlet guide vanes
11/02/1993US5257840 Safety locking device having a rocking hook
10/1993
10/28/1993DE4213125A1 Swivelling flap flow control for gas turbine - has convexly curved aerofoil shape constructed of stiffening ribs
10/27/1993EP0567277A1 Bypass injector valve for variable cycle aircraft engines
10/26/1993US5255850 Pivoting flaps and vane pack in a nozzle reverser assembly
10/26/1993US5255849 Cooling air transfer apparatus for aircraft gas turbine engine exhaust nozzles
10/26/1993US5255510 Thrust reverser for a high-bypass ratio turbofan engine
10/21/1993CA2091473A1 Bypass injector valve for variable cycle aircraft engines
10/13/1993CN1022433C Axisymmetric vectoring exhaust nozzle seal
10/12/1993US5251435 For use in an aircraft turbofan engine
10/06/1993EP0563662A1 Sealing device for flaps with a sealing fluid
10/05/1993US5250764 Consecutive plate acoustic suppressor apparatus and methods
10/05/1993US5249877 Apparatus for attaching a ceramic or other non-metallic circular component
10/05/1993US5249419 Nozzle liner for gas turbine engines
09/1993
09/29/1993EP0561791A1 Thrust reverser for a propfan engine.
09/21/1993US5245823 External flap vectoring mechanism
09/15/1993EP0454696B1 Propelling nozzle
09/15/1993CN1022124C Axisymmetric vectoring exhaust nozzle
09/14/1993US5243817 Thrust reverser for fan jet aircraft engines
09/08/1993EP0558472A1 Improvements in attenuators
09/01/1993EP0558381A1 Thrust reverser for a jet engine ensuring the guidance of the deviated jet
09/01/1993CN1021987C Infrared suppressor for gas turbine engine
08/1993
08/31/1993US5239823 Multiple layer cooled nozzle liner
08/31/1993US5239815 Sync-ring assembly for a gas turbine engine exhaust nozzle
08/25/1993EP0557229A1 Thrust vectoring variable geometry exhaust nozzle for gas turbines
08/24/1993US5238189 Convergent-to-divergent seal hinge for a convergent/divergent nozzle
08/19/1993WO1993016280A1 Exhaust eductor cooling system
08/19/1993WO1993016279A1 Latching and sealing arrangement for jet engine thrust reverser
08/17/1993US5236529 Fringed thermal protection device and method of manufacturing it
08/17/1993US5235808 Exhaust nozzle including idle thrust spoiling
08/17/1993US5235807 Fluid flow arrangement
08/10/1993US5233828 Combustor liner with circumferentially angled film cooling holes
08/10/1993US5233827 For masking the outlet of a gas turbine
08/03/1993US5232158 Convergent/divergent nozzle with seal centering
07/1993
07/27/1993US5230540 Fluid-tight joint with inclined flange face
07/27/1993US5230214 Recirculating zone inducing means for an augmentor burning section
07/27/1993US5230213 Aircraft turbine engine thrust reverser
07/22/1993WO1993013980A1 Thrust reverser integrating a variable exhaust area nozzle
07/20/1993US5228641 Cascade type aircraft engine thrust reverser with hidden link actuator
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