| 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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| 07/13/1993 | US5226598 Nozzle wall |
| 07/13/1993 | US5226455 Variable geometry duct seal |
| 07/06/1993 | US5224342 Latching and sealing arrangement for jet engine thrust reverser |
| 06/30/1993 | EP0549402A1 System for damping high frequency combustion instabilities in a combustion chamber |
| 06/29/1993 | US5223320 Perforated two layered sheet for use in film cooling |
| 06/29/1993 | US5222692 Sealing assembly between an aircraft fuselage and the outer nozzle flaps of a turbojet engine mounted in the rear end of the fuselage |
| 06/29/1993 | US5222359 Nozzle system and method for supersonic jet engine |
| 06/29/1993 | CA1319516C Cold-flow channel for a multiflow turbojet thrust reverser, associated with combined means of bleeding air |
| 06/23/1993 | EP0547936A1 Method and device for generating non contaminated air gust by high enthalpy |
| 06/22/1993 | US5221048 Variable area exhaust nozzle |
| 06/19/1993 | CA2085438A1 Method and installation for generating a high mass flow of unpolluted high enthalpy air |
| 06/15/1993 | US5219190 Shear wire flange joint for a gas turbine engine |
| 06/11/1993 | EP0591154A4 Turbofan engine fixed plug noise suppressor. |
| 06/10/1993 | WO1993011042A1 Thrust reverser with a planar exit opening |
| 06/09/1993 | EP0544764A1 Axisymmetric nozzle with gimbled unison ring. |
| 06/08/1993 | US5216879 Propulsion system assembly |
| 06/08/1993 | US5216878 Mixed exhaust flow supersonic jet engine and method |
| 06/03/1993 | DE4137638A1 Component with heat protected wall with cooling channels - has heat conductive layer on surface of cooling channel adjoining wall having matching layer and wall thicknesses |
| 06/01/1993 | US5215257 Divergent seal arrangement for a convergent/divergent nozzle |
| 06/01/1993 | US5215256 Flap hinge arrangement for a convergent/divergent nozzle |
| 05/26/1993 | EP0464050B1 Fluid-tight joints |
| 05/25/1993 | US5212945 Post-combustion device with pivoting flaps |
| 05/19/1993 | EP0542624A1 Thrust reverser configuration for a fan jet |
| 05/19/1993 | EP0542611A1 Safety device for a thrust reverser of an aircraft jet engine |
| 05/19/1993 | DE4202590C1 Thrust vector control for jet aircraft - has movable nozzle part shiftable in both directions along liner or curved line |
| 05/18/1993 | US5211008 Gas ejection nozzle for a jet engine and a jet engine fitted with this nozzle, in particular an engine of the separate flow type |
| 05/18/1993 | US5211007 Method of pressure-ratio control of gas turbine engine |
| 05/18/1993 | CA1317770C Gas turbine engines |
| 05/12/1993 | EP0541422A1 Security locking system with a tiltable retaining hook |
| 05/12/1993 | EP0541346A1 Fluid transfer apparatus |
| 05/11/1993 | US5209432 Aircraft reverser port door |
| 05/11/1993 | US5209059 Active cooling apparatus for afterburners |
| 05/11/1993 | US5209057 Rack and pinion actuation for an aircraft engine thrust reverser |
| 05/05/1993 | EP0540193A1 Reverser inner cowl with integral bifurcation walls and core cowl |
| 05/04/1993 | US5207787 Variable area nozzle |
| 05/04/1993 | US5207055 Volume enhanced turbine engine combustion zone |
| 04/29/1993 | WO1993008397A1 Turbojet engine with a fan or propfan |
| 04/27/1993 | CA1316674C Joint connection for annular flanges |
| 04/22/1993 | DE4134051A1 Turbinenstrahltriebwerk mit geblaese oder prop-fan Turbojet engine with fan or prop-fan |
| 04/20/1993 | US5203164 Method and apparatus for quieting a turbojet engine |
| 04/14/1993 | EP0536954A1 A lock for a thrust reverser mechanism, a thrust reverser mechanism, and a thrust reverser |
| 04/13/1993 | US5201887 Of a gas turbine engine |
| 04/13/1993 | US5201800 Method for discharging combustion gases from an exhaust nozzle |
| 04/06/1993 | US5199643 Model aircraft variable geometry nozzle |
| 04/01/1993 | WO1993006006A1 Ducted fan turbine engine nozzle assembly |
| 04/01/1993 | CA2119440A1 Ducted fan turbine engine nozzle assembly |
| 03/31/1993 | EP0534834A1 Hydraulic equipment with security control |
| 03/31/1993 | EP0534833A1 Locking device with a rotating hook bolt |
| 03/31/1993 | EP0534815A1 Thrust-reverser with improved guidance of the reversed jets |
| 03/31/1993 | CN1020207C Two-dimensional exhaust nozzles with divergent flap actuation system |
| 03/30/1993 | US5197693 Aircraft turbine engine thrust reverser with sliding hinge actuator |
| 03/30/1993 | US5197280 Control system and method for controlling a gas turbine engine |
| 03/18/1993 | WO1993005291A1 Turbo-jet thrust reverser having improved reversed-flow layer control |
| 03/09/1993 | US5192023 Jet engine provided with a thrust reverser |
| 03/04/1993 | WO1993004273A1 Turboreactor thrust reverser having a progressive curvature deflecting edge |
| 03/03/1993 | EP0530078A1 Thrust reverser having a curved downstream edge |
| 03/03/1993 | EP0528894A1 Variable cycle gas turbine engine for supersonic aircraft |
| 02/23/1993 | US5188292 Thermal shields for rotating members in a gas flow path |
| 02/16/1993 | US5186390 Propelling nozzle |
| 02/09/1993 | US5184455 Method of restricting cooling air flow |
| 01/27/1993 | EP0524875A1 Thrust reverser for an aircraft jet engine with hydraulic actuation system with integrated security device |
| 01/26/1993 | US5181676 Thrust reverser integrating a variable exhaust area nozzle |
| 01/26/1993 | US5181379 Gas turbine engine multi-hole film cooled combustor liner and method of manufacture |
| 01/20/1993 | EP0523559A1 Sealing device |
| 01/12/1993 | US5178922 For protecting wall to be submitted to ablative flow at high temperature, thermally insulative matrix, open-weave woven refractory material provided with meshes, refractory armature in form of fringed mat |
| 01/05/1993 | US5176340 Thrust reverser with a planar exit opening |
| 01/05/1993 | US5176323 Reduced weight nozzle actuation mechanism |
| 12/30/1992 | EP0520871A1 Improved thrust reverser for a jet engine |
| 12/30/1992 | EP0520601A1 Conforming plunger seal assembly |
| 12/29/1992 | US5174502 Support for a translating nozzle vectoring ring |
| 12/22/1992 | US5172546 Volume enhanced turbine engine combustion zone |
| 12/17/1992 | DE4119334A1 Accident prevention safety appts. for aircraft - prevents unintentional switching of propulsion system into reverse at preset altitude, speed and undercarriage position |
| 12/16/1992 | EP0518498A1 Thermal shield for axisymmetric vectoring nozzle |
| 12/01/1992 | US5167119 For use on an aircraft |
| 12/01/1992 | US5167118 Jet engine fixed plug noise suppressor |
| 11/25/1992 | EP0515263A1 Thrust reverser for high by-pass ratio turbofan |
| 11/24/1992 | US5165227 Propelling nozzle for a hypersonic engine |
| 11/19/1992 | EP0513959A1 Shear wire flange joint |
| 11/17/1992 | CA1310349C Bearing seal for universal ball joint |
| 11/14/1992 | CA2065680A1 Shear wire flange joint |
| 11/11/1992 | EP0512833A1 Support for a translating nozzle vectoring ring |
| 11/11/1992 | EP0512663A1 Cooled leaf seal |
| 11/10/1992 | US5162620 Dual flow turbine engine muffler |
| 11/10/1992 | US5161752 In-flight reverser |
| 11/10/1992 | CA1309872C Jet engine noise suppression system |
| 11/03/1992 | US5159809 Highly adaptable combined propulsion engine for an aircraft or a space-going airplane |
| 10/27/1992 | US5157917 Gas turbine engine cooling air flow |
| 10/27/1992 | US5157916 Apparatus and method for suppressing sound in a gas turbine engine powerplant |
| 10/21/1992 | EP0509757A1 Jet engine exhaust nozzle |
| 10/21/1992 | EP0509166A1 Honeycomb noise attenuation structure |
| 10/16/1992 | CA2062925A1 Reduced weight nozzle actuation mechanism |
| 10/13/1992 | US5154352 Propelling nozzle for an aircraft engine |
| 10/13/1992 | US5154052 Exhaust assembly for a high speed civil transport aircraft engine |
| 10/13/1992 | US5154050 Thrust vector control using internal airfoils |
| 09/30/1992 | EP0506277A1 Device for operation of a gas turbine engine thrust reverser system |
| 09/29/1992 | US5150862 For gas turbine engine aircraft |
| 09/29/1992 | US5150839 Nozzle load management |
| 09/29/1992 | US5150571 Device for exposing or shutting off a turbo-engine on the intake air side of the engine |
| 09/16/1992 | EP0503963A1 Thrust load path for vectoring nozzle |
| 09/08/1992 | US5144795 Gas turbine engine |