| 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) |
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| 03/28/1989 | US4815281 Air take-off for a turbojet engine cold flow duct |
| 03/21/1989 | US4813608 Use in high temperature aircraft engine environment |
| 03/21/1989 | US4813607 Variable-area thrust vectoring and reversing asymmetric aircraft exhaust nozzle |
| 03/21/1989 | US4813230 Gas turbine nozzles |
| 03/16/1989 | DE3829908A1 Multipurpose gas turbine |
| 03/07/1989 | US4810677 Heat-insulating lining for a gas turbine |
| 03/07/1989 | US4809932 Thrust vector control for aircraft |
| 03/07/1989 | US4809500 Transient control system for gas turbine engine |
| 02/28/1989 | US4807434 Thrust reverser for high bypass jet engines |
| 02/21/1989 | US4805840 Thrust deflectors for propulsion nozzles of turbomachines |
| 02/21/1989 | US4805401 Control vent for diverting exhaust nozzle |
| 02/15/1989 | EP0303399A2 Coupling for a linear displacement transducer |
| 02/07/1989 | US4802629 Plug-type exhaust nozzle having a variable centerbody and translating shroud |
| 02/01/1989 | EP0301955A1 Turbine thrust reverser having a device for re-orientating the gas flow |
| 02/01/1989 | EP0301939A1 Turbine thrust reverser having a mobile deflector |
| 01/31/1989 | US4801112 Aircraft power unit of the type with faired blower equipped with a thrust reverser wth doors |
| 01/31/1989 | US4801087 Exhaust nozzle for a gas turbine engine |
| 01/31/1989 | US4800718 Surface cooling system |
| 01/31/1989 | US4800715 Apparatus for suppressing infrared radiation emitted from gas turbine engines |
| 01/24/1989 | US4799623 For a supersonic aircraft |
| 01/18/1989 | EP0299832A1 Axis-symmetric convergent-divergent ejection nozzle for a jet engine |
| 01/17/1989 | US4798328 Area controlled, thrust vectoring vane cascade with nutating control vane |
| 01/17/1989 | US4798048 Augmentor pilot |
| 01/04/1989 | EP0298010A2 Divergent flap actuation system for a two-dimensional exhaust nozzle |
| 01/04/1989 | CN1030122A Divergent flap actuation system for two-dimensional exhaust nozzles |
| 12/27/1988 | US4793134 Fluid propulsion engine with flow exit control device |
| 12/14/1988 | EP0294424A1 Vtol aircraft having combination lift and lift/cruise engines |
| 12/14/1988 | CN88102317A Nozzle flap cooling liner |
| 12/13/1988 | US4790495 For an aircraft jet engine |
| 12/07/1988 | CN88103093A Area controlled thrust vectoring vane cascade |
| 11/30/1988 | CN88102722A Coolable thin metal sheet |
| 11/23/1988 | EP0292422A2 Linkage for area controlled, thrust vectoring vane cascade |
| 11/23/1988 | EP0292421A2 Area controlled, thrust vectoring vane cascade with nutating control vane |
| 11/23/1988 | EP0292419A2 Area controlled, thrust vectoring vane cascade |
| 11/23/1988 | CN88102602A Temperature resistant fastener arrangement |
| 11/22/1988 | US4786016 Annular nacelle adapted to surround a gas turbine engine |
| 11/16/1988 | CN88102721A Exhaust gas nozzle including cooling air diverter valve |
| 11/15/1988 | US4784326 Convergent flap bearing with integral hold-down device |
| 11/09/1988 | EP0290371A1 Exhaust gas nozzle including a cooling air diverter |
| 11/09/1988 | EP0290370A1 Coolable thin metal sheet |
| 11/09/1988 | CN88102206A Thrust vectoring exharst nozzle arrangement |
| 11/08/1988 | US4783085 Segmented rigid sliding seal |
| 11/02/1988 | EP0289443A2 Temperature resistant fastener arrangement |
| 11/02/1988 | EP0289376A1 Acoustic panel for sound-proof lining, and turbo jet engine comprising such a lining |
| 11/02/1988 | CN88102318A Nozzle flap edge cooling |
| 11/01/1988 | CA1243848A1 Gas compressor for jet engine |
| 10/26/1988 | CN88101862A Flap support arrangement |
| 10/19/1988 | EP0287499A2 Nozzle flap edge cooling |
| 10/19/1988 | EP0287498A2 Nozzle flap cooling liner |
| 10/19/1988 | EP0286800A1 Infrared radiation shielding device |
| 10/19/1988 | CN88101725A Method and linkage for positioning convergent flap and coaxial arc valve |
| 10/19/1988 | CN88101623A Segmented rigid sliding seal |
| 10/18/1988 | US4778110 Modular composite cascade assembly |
| 10/18/1988 | US4778109 Adjustable two dimensional nozzle for aircraft jet engines |
| 10/12/1988 | EP0286572A2 Thrust vectoring exhaust nozzle arrangement |
| 10/12/1988 | EP0286567A1 Flap support arrangement |
| 10/04/1988 | USH528 Method and apparatus for increasing service life of augmentor and combustion chamber liners |
| 10/04/1988 | CA1242589A1 Vectorable exhaust nozzle for gas turbine engines |
| 09/28/1988 | EP0284540A2 Method and linkage for positioning a convergent flap and coaxial arc valve |
| 09/28/1988 | EP0284539A2 Segmented rigid sliding seal |
| 09/27/1988 | US4773593 Coolable thin metal sheet |
| 09/20/1988 | US4772033 In an aircraft engine |
| 09/07/1988 | EP0281494A1 Exhaust nozzle flap assembly |
| 09/07/1988 | EP0281455A1 Fan jet engine with a thrust reverser |
| 09/07/1988 | EP0281264A1 Vectorable variable flow area propulsion nozzle |
| 09/07/1988 | CN88101072A Exhaust nozzle flap assembly |
| 09/06/1988 | US4769196 Method of manufacture of a non metallic laminate |
| 08/30/1988 | US4767055 Method and linkage for positioning a convergent flap and coaxial arc valve |
| 08/25/1988 | DE3803992A1 Gasturbinentriebwerk mit nachbrenner und verstellbarem bypass-injektor Gas turbine engine with afterburner and adjustable bypass injector |
| 08/17/1988 | EP0278068A2 Thrust vectoring control system for aircraft |
| 08/17/1988 | CN88100576A Transient control system for gas turbine engine |
| 08/16/1988 | US4763840 Thrust vectoring exhaust nozzle arrangement |
| 08/16/1988 | CA1240599A1 Device for thermal protection from ablation and vibrations and manufacturing method |
| 08/10/1988 | EP0277904A2 Transient control system for gas turbine engine |
| 08/09/1988 | US4761949 Thrust reverser position indicator shaft bearing assembly |
| 08/02/1988 | USH500 Exhaust nozzle flap assembly |
| 08/02/1988 | US4760964 Actuator system for jet nozzle flap |
| 08/02/1988 | US4760960 Exhaust gas thrust |
| 07/27/1988 | EP0275757A1 Bidimensional, controllable jet nozzle |
| 07/26/1988 | US4759513 Noise reduction nacelle |
| 07/12/1988 | US4756053 For a gas turbine engine exhaust nozzle |
| 07/05/1988 | US4754924 Variable geometry nozzle |
| 07/05/1988 | US4754694 Fluid actuator with lock position indicating means |
| 06/28/1988 | US4753392 Two dimensional gas turbine engine exhaust nozzle |
| 06/16/1988 | WO1988004257A1 Vtol aircraft having combination lift and lift/cruise engines |
| 06/07/1988 | US4749298 Temperature resistant fastener arrangement |
| 06/07/1988 | US4748806 Attachment means |
| 05/31/1988 | US4747543 Nozzle flap cooling liner |
| 05/31/1988 | US4747542 Nozzle flap edge cooling |
| 05/11/1988 | EP0267078A1 Position detection ramp bearing for a turbo blower thrust reverser |
| 05/10/1988 | US4742961 Exhaust gas nozzle including a cooling air diverter |
| 04/26/1988 | US4739932 Propulsion nozzle for gas turbine engine |
| 04/26/1988 | US4739931 Flap support arrangement |
| 03/22/1988 | US4732535 Fluid flow reversing apparatus |
| 03/22/1988 | US4732324 Variable flow area nozzle |
| 03/22/1988 | US4731991 Gas turbine engine thrust reverser |
| 03/02/1988 | EP0257147A1 Turbomachine ejector nozzles |
| 02/23/1988 | US4726545 VTOL aircraft having combination lift and lift/cruise engines |
| 02/10/1988 | EP0255796A2 Gas turbine outlet arrangement |
| 02/02/1988 | US4722821 Metal skeletal frames covered with pressure injection molded thermosetting resin |