| 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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| 10/08/1991 | US5054285 Thrust reverser for turbofan engine |
| 09/24/1991 | US5050803 Actuation system for positioning a vectoring exhaust nozzle |
| 09/18/1991 | CN1013982B Exhaust gas nozzle including cooling air diverter valve |
| 09/10/1991 | US5046307 Thrust reverser for high bypass turbofan engine |
| 09/03/1991 | US5044553 Sidewall deflection control for a two-dimensional nozzle |
| 08/28/1991 | EP0442899A1 Vane-type thrust vectoring nozzle. |
| 08/27/1991 | US5042746 Nozzle assembly for aircraft |
| 08/27/1991 | CA2034472A1 Exhaust nozzle having variable contour exhaust flap |
| 08/20/1991 | US5041323 Honeycomb noise attenuation structure |
| 08/20/1991 | US5040730 Thrust reverser door having an exhaust gas passage |
| 08/13/1991 | US5039171 Multi-panel thrust reverser door |
| 08/13/1991 | US5039014 Axisymmetric vectoring exhaust nozzle seal |
| 08/13/1991 | US5038560 Fluid outlet duct |
| 08/13/1991 | US5038559 Method and apparatus for selectively varying an effective fluid flow area of a jet engine exhaust nozzle |
| 08/13/1991 | CA2034406A1 Exhaust nozzle including idle thrust spoiling |
| 07/26/1991 | CA2023853A1 Mixed flow augmentor pre-mixer |
| 07/23/1991 | US5034172 Process for the manufacture of composite components comprising a web and a reinforcement structure |
| 07/17/1991 | EP0436685A1 An acoustic liner. |
| 07/17/1991 | CA2031085A1 Arrangement for sealing gaps between adjacent circumferential segments of turbine nozzles and shrouds |
| 07/16/1991 | US5031836 Flexible fairing for airframe/nozzle interface |
| 06/26/1991 | EP0434565A1 Versatile combined propulsion engine for aeroplane or space shuttle |
| 06/26/1991 | CN1012984B Joint connection for annular flanges |
| 06/25/1991 | US5025888 Acoustic liner |
| 06/13/1991 | WO1991008379A1 Dual flow turbine engine muffler |
| 06/13/1991 | DE3940381A1 Duct for gas turbine exhaust gases - consists of outer and inner wall, insulating layer and cover plates and rails |
| 06/12/1991 | CN1012833B Nozzle flap edge cooling |
| 06/04/1991 | US5020318 Aircraft engine frame construction |
| 05/21/1991 | US5016818 Integral transition and convergent section exhaust nozzle |
| 05/21/1991 | US5016436 Interturbine duct |
| 05/18/1991 | CA2025244A1 Bolt shield for rotating exhaust duct |
| 05/14/1991 | US5014917 High-temperature, flexible, thermal barrier seal |
| 05/14/1991 | US5014815 Acoustic liner |
| 05/07/1991 | WO1991006750A1 Turbofan engine fixed plug noise suppressor |
| 04/30/1991 | US5011195 Constant volume connector |
| 04/30/1991 | US5011080 Convergent/divergent nozzle construction |
| 04/24/1991 | CN1012445B Transient control system for gas turbine engine |
| 04/17/1991 | CN1012385B Nozzle flap cooling liner assembly for gas turbine |
| 04/17/1991 | CN1012384B Thrust vectoring exhaust nozzle arrangement |
| 04/12/1991 | CA2021627A1 Vibration damping hinge joints for variable area jet engine exhaust nozzles |
| 04/10/1991 | EP0421212A1 Gasturbine jet engine with at least one axially movable closure member |
| 04/02/1991 | US5003770 Thrust reverser for a jet engine of the type with doors equipped with auxiliary flaps |
| 03/20/1991 | EP0250473B1 Device for producing a forward drive force |
| 03/19/1991 | US5000386 Exhaust flaps |
| 03/12/1991 | US4998409 Gas turbine engine |
| 03/08/1991 | CA2021086A1 Exhaust nozzle hinge |
| 02/27/1991 | EP0414609A1 Jet engine cascade thrust reverser without sliding cowling |
| 02/27/1991 | EP0413983A1 Production method for a channeled wall thrust nozzle |
| 02/21/1991 | WO1991001034A3 An acoustic liner |
| 02/20/1991 | EP0413635A1 Thrust reverser for a jet engine |
| 02/19/1991 | US4994660 Axisymmetric vectoring exhaust nozzle |
| 02/19/1991 | US4993641 Gas turbine spherical exhaust nozzle |
| 02/19/1991 | US4993638 Thrust vectoring nozzle assembly |
| 02/19/1991 | US4993314 Convectively cooled hot gas exhaust structure to reduce infrared radiation |
| 01/24/1991 | WO1991001034A2 An acoustic liner |
| 01/22/1991 | US4986734 Overspeed protection system for aircraft fan engine |
| 01/22/1991 | CA1279199C Variable area exhaust nozzle for a gas turbine engine |
| 01/15/1991 | US4984741 Vectorable variable flow area propulsion nozzle |
| 01/15/1991 | US4984732 Method of superplastically forming and diffusion bonding a laminate assembly |
| 01/09/1991 | CN1048429A Infrared suppressor for gas turbine engine |
| 01/02/1991 | EP0406155A1 Infrared suppressor for a gas turbine engine |
| 01/02/1991 | EP0405796A1 Jet engine noise suppression system |
| 12/18/1990 | US4978071 For directing exhaust flow of the nozzle |
| 12/11/1990 | US4976466 Thrust reverser for a turbojet engine |
| 12/04/1990 | US4974638 Transition pipe for a jet pipe assembly of a turbojet engine |
| 11/22/1990 | EP0398787A1 Tufted thermal protection layer and production method therefor |
| 11/14/1990 | EP0397566A1 Heat insulation structure for an afterburner liner or turbine transition piece |
| 11/14/1990 | EP0396736A1 Sustainer propulsion system |
| 11/06/1990 | US4968217 Variable pitch arrangement for a gas turbine engine |
| 10/30/1990 | US4966327 Jet engine provided with a thrust reverser |
| 10/25/1990 | DE3940424A1 Dichtung fuer eine axialsymmetrische strahlumlenkungsschubduese Gasket for an axisymmetric strahlumlenkungsschubduese |
| 10/24/1990 | CN1046371A Axisymmetric vectoring exhaust nozzle seal |
| 10/24/1990 | CN1046370A Axisymmetric vectoring exhaust nozzle |
| 10/18/1990 | WO1990012168A1 Sound attenuating laminate and installation for jet aircraft engines |
| 10/18/1990 | DE3912331A1 Nozzle for hypersonic turbo-ram-jet engine |
| 10/17/1990 | EP0392526A1 Thrust nozzle |
| 10/11/1990 | DE3619652C1 Jet aircraft manoeuvring aid - has three movable flaps each suspended from four point linkage |
| 10/11/1990 | CA2013934A1 Axisymmetric vectoring exhaust nozzle seal |
| 10/11/1990 | CA2013931A1 Nozzle with thrust vectoring in the yaw direction |
| 10/10/1990 | CN1046019A Nozzle with thrust vectoring in yaw direction |
| 10/02/1990 | US4960243 Thrust reverser for a turbojet engine |
| 10/02/1990 | US4959955 Method of operating gas turbine engine with fan damage |
| 09/27/1990 | DE4008447A1 Verfahren und einrichtung zum regeln eines gasturbinentriebwerks Method and device for control of a gas turbine engine |
| 09/20/1990 | WO1990010812A1 Fluid-tight joints |
| 09/18/1990 | US4957249 Thrust vector control flap with a merging convex, concave inner contour, for jet aircraft and method for operating the same |
| 09/12/1990 | EP0387123A1 Thermic protection liner for hot pipe of turbo-jet engine |
| 09/12/1990 | CN1045228A Sustained release bolus effective for prolonged prevention, treatment or control of nematode, acarid and endo-and ectoparasi-infestations of ruminants |
| 09/11/1990 | US4955541 Two dimensional nozzle for a turbojet engine |
| 09/05/1990 | EP0385912A2 Gas turbine jet engine |
| 09/05/1990 | EP0385834A1 Variable and vectorable nozzle unit for a jet engine |
| 09/05/1990 | EP0385106A1 Sustained release bolus effective for the prolonged prevention, treatment or control of nematode, acarid and endo- and ectoparasitic infestations of ruminants |
| 08/28/1990 | US4951973 Joint connection for annular flanges |
| 08/14/1990 | US4948072 Segmented vectoring cruise nozzles |
| 08/14/1990 | US4947644 Diverging portion of discontinuous curvature for a rocket engine nozzle |
| 08/14/1990 | US4947643 Active geometry control system for gas turbine engines |
| 08/09/1990 | DE3903713A1 Strahltriebwerk Jet engine |
| 08/08/1990 | EP0120856B1 Thrust reverser blocker door assembly |
| 07/31/1990 | US4944362 For a gas turbine engine duct |
| 07/26/1990 | WO1990008254A1 Propelling nozzle |
| 07/24/1990 | US4942653 Production method for a channeled wall thrust nozzle |
| 07/03/1990 | US4938021 For a missile |