| 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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| 05/23/1995 | US5417441 Low friction seal between relatively moving parts |
| 05/23/1995 | US5417055 Valve for diverting fluid flows in turbomachines |
| 05/18/1995 | WO1995013467A1 Turbine exhaust gas anti-ice system |
| 05/03/1995 | EP0436685B1 An acoustic liner |
| 04/27/1995 | WO1995011372A1 Silencer |
| 04/26/1995 | EP0649980A1 Jet engine thrust reverser door equiped with an auxiliary flap |
| 04/23/1995 | CA2118292A1 Thrust reverser with doors for jet airplane engine equipped with auxiliary flap shutters |
| 04/20/1995 | WO1995010748A1 Finless aerodynamic control system |
| 04/18/1995 | US5407133 For a hot gas conveying conduit |
| 04/12/1995 | EP0647777A1 Axis-symmetric, convergent/divergent exhaust nozzle with thrust reverser |
| 04/11/1995 | US5404714 Lock for an engine thrust reverser |
| 04/11/1995 | US5404713 Spillage drag and infrared reducing flade engine |
| 04/05/1995 | EP0646720A1 Spillage drag and infrared emission reducing fan jet engine |
| 04/05/1995 | EP0646719A1 Impingement/film cooling for panels |
| 04/05/1995 | EP0646718A1 Lock for an engine thrust reverser |
| 04/05/1995 | EP0646717A1 Device for yaw and pitch control of an aerospace vehicle with at least one variable bidimensional nozzle |
| 04/05/1995 | EP0646716A1 Bidimensional vectoriable nozzle |
| 04/05/1995 | EP0646715A1 Bidimensional vectoriable nozzle adaptable to different flight conditions |
| 04/04/1995 | US5402964 Interference with vortex formation and control of fluid flow to reduce noise and change flow stability |
| 04/04/1995 | US5402963 Acoustically shielded exhaust system for high thrust jet engines |
| 04/02/1995 | CA2133353A1 Method and nozzle for producing thrust |
| 03/29/1995 | CN1028051C Area controlled, thrust vectoring vane cascade with nutating control vane |
| 03/28/1995 | US5400586 Self-accommodating brush seal for gas turbine combustor |
| 03/22/1995 | EP0644325A1 Exhaust nozzle for a gas turbine |
| 03/21/1995 | US5398887 Finless aerodynamic control system |
| 03/21/1995 | US5398500 Convergent divergent jet engine nozzle |
| 03/21/1995 | US5398499 Orientable axisymmetric nozzle of variable geometry of gas turbine propulsors |
| 03/15/1995 | EP0643234A1 Mounting of a vane bearing and shield provided for this bearing |
| 03/14/1995 | US5396762 Thrust reversal assembly for controlling sidewardly diverted flow |
| 02/28/1995 | US5392991 Thrust reversing device for jet aircraft engines |
| 02/28/1995 | US5392597 Jet mixer noise suppressor using acoustic feedback |
| 02/21/1995 | US5390879 Jet pipe for supporting a thrust reverser for aircraft jet engines |
| 02/21/1995 | US5390877 Vectorable nozzle for aircraft |
| 02/15/1995 | EP0638913A1 Detection circuit for the switch position of several bipolar switches and application for a jet engine thrust reverser |
| 02/15/1995 | EP0502924B1 Dual flow turbine engine muffler |
| 02/14/1995 | US5388765 Gas turbine nozzle construction |
| 02/01/1995 | EP0636780A1 Noise suppression liner for jet engines |
| 01/25/1995 | EP0635632A1 Fixed geometry mixer/ejector noise suppression system for turbofan aircraft engines |
| 01/24/1995 | US5383332 Gas turbine engines |
| 01/24/1995 | CA2009636C Ventral segmented nozzles |
| 01/17/1995 | US5381654 For a turbofan engine thrust reverser |
| 01/17/1995 | CA1333961C Double flow turbojet reverser equipped with deflection edges having mobile lips |
| 01/12/1995 | WO1995001501A1 Starting fuel pressure schedule for a gas turbine |
| 01/12/1995 | DE4322431A1 Kühlstruktur und Verfahren zu ihrer Herstellung The cooling structure and process for their preparation |
| 01/10/1995 | US5379800 Cam operated valve |
| 01/10/1995 | US5379585 Hydraulic control system for a jet engine nozzle |
| 01/05/1995 | WO1995000754A1 A syntactic film for thrust reverser blocker doors |
| 01/05/1995 | DE4321393A1 Wall structure, in particular for a ram-jet engine (ram-jet, ram engine, athodyd) |
| 01/04/1995 | EP0632196A1 Jet engine thrust reverser with aerodynamic cooling |
| 12/28/1994 | EP0631042A1 Turbofan noise reduction nozzle |
| 12/26/1994 | CA2126274A1 Deep core radial noise suppression treatment for jet aircraft engine |
| 12/13/1994 | US5372006 Turbine engine equipped with thrust reverser |
| 12/06/1994 | US5370312 Gas turbine engine exhaust nozzle |
| 12/06/1994 | US5369954 Turbofan engine bypass and exhaust system |
| 11/30/1994 | EP0626039A1 Exhaust eductor cooling system. |
| 11/15/1994 | US5364029 For a gas turbine engine |
| 11/09/1994 | EP0623742A1 Nozzle seal assembly with removable baseplate |
| 11/02/1994 | EP0622538A1 Variable geometry exhaust nozzle for turbomachine |
| 11/02/1994 | EP0622294A1 Variable area convergent-divergent nozzle |
| 11/02/1994 | CN1094479A Centrifugal jet tube |
| 11/01/1994 | US5359851 Variable geometry exhaust nozzle for a turbojet engine |
| 11/01/1994 | US5359848 Device for operation of a gas turbine engine thrust reverser system |
| 10/31/1994 | CA2118989A1 Variable area convergent-divergent nozzle |
| 10/27/1994 | WO1994024430A1 Cascade assembly for use in a thrust-reversing mechanism |
| 10/27/1994 | WO1994019177A3 Angled i-beam honeycomb structure |
| 10/26/1994 | EP0620792A1 Thrust reverser integrating a variable exhaust area nozzle |
| 10/12/1994 | EP0619133A1 Mixing receptacle |
| 10/11/1994 | US5353598 Damping system for high frequency combustion instabilities in a combustion chamber |
| 10/05/1994 | CN1026146C Area controlled, thrust vectoring vane cascade |
| 10/04/1994 | US5352529 Lightweight thrust vectoring panel |
| 10/04/1994 | US5351888 Multi-axis vectorable exhaust nozzle |
| 10/04/1994 | US5351480 Jet engine |
| 09/29/1994 | WO1994021910A1 External flap vectoring mechanism |
| 09/29/1994 | WO1994018446A3 Turbine engine equipped with thrust reverser |
| 09/28/1994 | CN1026022C Linkage for area controlled, thrust vectoring vane cascade |
| 09/20/1994 | US5348252 Vectorable nozzle mounting |
| 09/20/1994 | US5347808 Jet-engine thrust reversers |
| 09/06/1994 | US5344197 Safety locking device having a tilting hook |
| 09/06/1994 | US5343696 Thrust reverser for a propfan engine |
| 09/01/1994 | WO1994019177A2 Angled i-beam honeycomb structure |
| 08/23/1994 | US5339637 Tube segment, in particular flame tube, with a cooled support frame for a heatproof lining |
| 08/18/1994 | WO1994018446A2 Turbine engine equipped with thrust reverser |
| 08/17/1994 | EP0561791B1 Thrust reverser for a propfan engine |
| 08/10/1994 | EP0610091A1 Method of operating an aircraft bypass turbofan engine having variable fan outlet guide vanes |
| 08/09/1994 | US5335489 Gas turbine vectoring exhaust nozzle |
| 08/04/1994 | DE4317807C1 Schubdüse für Strahlantriebe mit Befestigungselementen The thruster of Jet Propulsion with fasteners |
| 07/26/1994 | US5332239 High-temperature, bellows hybrid seal |
| 07/21/1994 | WO1994015830A1 Radial four-blade thrust vector_______________________________ |
| 07/19/1994 | US5329763 Thrust vectoring variable geometry exhaust nozzle for gas turbines |
| 07/19/1994 | US5329759 Method for regulating fuel flow in a gas turbine engine |
| 07/13/1994 | EP0605525A1 Ducted fan turbine engine nozzle assembly. |
| 07/12/1994 | US5328098 Thrust vectoring ejector nozzle |
| 07/05/1994 | US5325661 Jet mixer noise suppressor using acoustic feedback |
| 06/28/1994 | US5323965 In a 2-D nozzle of a gas turbine engine |
| 06/28/1994 | US5323606 Stowable nozzle |
| 06/15/1994 | EP0601910A1 Thrust reverser door with deflector vanes to guide the jet |
| 06/15/1994 | EP0601688A1 Gasturbine engine flow mixer sound suppression means |
| 06/09/1994 | DE4340951A1 Einstückiges Triebwerkeinlaß-Schallrohr One-piece engine inlet sound tube |
| 05/31/1994 | US5315821 Aircraft bypass turbofan engine thrust reverser |
| 05/24/1994 | US5313789 Solid fuel turbine power plant and method |