| 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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| 06/26/1996 | EP0718190A1 Improvements for helicopters equipped with a jet dilution and deviation device for combustion gases |
| 06/22/1996 | CA2165511A1 Protective shield for a turbo-engine |
| 06/19/1996 | EP0717184A1 Thrust reverser with pivotable doors which are translatable |
| 06/12/1996 | EP0716268A2 Cooled wall part |
| 06/11/1996 | US5524846 Fire protection system for airplanes |
| 06/11/1996 | US5524827 Method and nozzle for producing thrust |
| 06/11/1996 | US5524431 Thrust reverser with doors for jet aircraft engine, the doors being equipped with an auxiliary flap |
| 06/05/1996 | EP0715068A1 Thrust reverser with pivoting doors |
| 06/05/1996 | EP0715067A2 Engine exhaust nozzle seal |
| 06/05/1996 | EP0626039B1 Exhaust eductor cooling system |
| 06/05/1996 | EP0544817B1 Thrust vectoring exhaust nozzle |
| 06/04/1996 | US5522546 In a gas turbine engine casing |
| 05/31/1996 | CA2163920A1 Turbofan thrust reverser with downstream deflectors |
| 05/28/1996 | US5520336 Nozzle for a jet engine containing an adjustable convergent-divergent portion |
| 05/21/1996 | US5518311 Mixing chamber with vortex generators for flowing gases |
| 05/17/1996 | WO1996014516A1 Self-locking sealing device |
| 05/14/1996 | CA2103618C Divergent slave petal for sealing in variable geometry exhaust nozzles for gas turbine propulsion units |
| 05/07/1996 | US5513799 Divergent master petal for orientable nozzles of variable geometry intended for gas turbine engines |
| 05/02/1996 | WO1996012881A1 Variable area fan exhaust nozzle |
| 04/30/1996 | US5511745 Vectorable nozzle having jet vanes |
| 04/30/1996 | US5511376 Of an internal combustion engine |
| 04/25/1996 | WO1996012269A1 Jet engine fan noise reduction system utilizing electro pneumatic transducers |
| 04/23/1996 | US5509669 Gas-path leakage seal for a gas turbine |
| 04/16/1996 | US5508626 Circuit for detecting the position of several bipolar contactors and application for a thrust reverser of a turbojet engine |
| 04/16/1996 | US5507143 Cascade assembly for use in a thrust-reversing mechanism |
| 04/10/1996 | EP0705384A1 Starting fuel pressure schedule for a gas turbine |
| 04/10/1996 | EP0605525B1 Ducted fan turbine engine nozzle assembly |
| 04/03/1996 | EP0704615A2 Failsafe nozzle actuating system |
| 04/03/1996 | EP0704020A1 A syntactic film for thrust reverser blocker doors |
| 03/27/1996 | EP0703358A2 Lock mechanism for a thrustreverser |
| 03/26/1996 | US5501071 Fixing arrangement for a thermal protection tile in a combustion chamber |
| 03/20/1996 | EP0702141A2 Sound absorbing apparatus for a supersonic jet propelling engine |
| 03/19/1996 | US5499765 Nozzle capable of varying the direction of discharge of fluid therefrom |
| 03/06/1996 | EP0699273A1 Cascade assembly for use in a thrust-reversing mechanism |
| 03/05/1996 | US5495710 Dual-flow turbine engine equipped with a thrust reversal system and a device for restricting the annular channel for the ejection of cold gases, and a restriction device equipping such a turbine engine |
| 02/27/1996 | US5494221 Variable geometry turbojet engine exhaust nozzle |
| 02/27/1996 | US5493856 Thrust reverser control mechanism |
| 02/21/1996 | EP0697514A1 Sealing device for the slave flaps of a variable convergent-divergent nozzle for a jet engine |
| 02/13/1996 | US5491307 Porous single expansion ramp |
| 02/08/1996 | DE4433759C1 Strahltriebwerk mit Schubumkehr Jet engine thrust reversers |
| 02/01/1996 | WO1996002746A1 Thrust reverser |
| 01/25/1996 | DE4426195A1 Thrust nozzle for turbo airstream |
| 01/23/1996 | US5485959 Axisymmetric vectoring exhaust nozzle thermal shield |
| 01/23/1996 | US5485958 Mechanism for operating a cascade of variable pitch vanes |
| 01/17/1996 | EP0692619A1 Double flux turbine thrust reverser with external blocker flaps |
| 01/17/1996 | EP0692069A1 External flap vectoring mechanism |
| 01/16/1996 | US5484122 Turbine exhaust gas anti-ice system |
| 01/16/1996 | US5484105 Cooling system for a divergent section of a nozzle |
| 01/16/1996 | US5483794 Multi-hole film cooled afterburner combustor liner |
| 01/16/1996 | US5483793 Gas turbine engine |
| 01/09/1996 | US5481868 Variable area nozzle with fixed convergent-divergent walls and relatively movable parallel sideplates |
| 01/03/1996 | EP0690217A1 Double flux turbine thrust reverser with blocker flaps connected to the engine cowling |
| 12/26/1995 | US5478016 Vectorable nozzle |
| 12/20/1995 | EP0687810A2 Nozzle for a jet engine with variable geometry and orientation |
| 12/19/1995 | US5476237 Syntactic film for thrust reverser blocker doors |
| 12/19/1995 | US5476224 Variable area outlet of a gas turbine engine discharge nozzle |
| 12/19/1995 | CA2009635C Segmented vectoring cruise nozzles |
| 12/12/1995 | US5473886 Thrust reverser with aerodynamically cooled baffle |
| 12/06/1995 | EP0684903A1 Angled i-beam honeycomb structure. |
| 11/29/1995 | EP0683859A1 Turbine engine equipped with thrust reverser |
| 11/28/1995 | US5470020 Combination turbojet engine nozzle and thrust reverser |
| 11/28/1995 | US5469894 Metal duct subjected to steep temperature gradients |
| 11/22/1995 | EP0682744A1 Divergent seal arrangement for a convergent/divergent nozzle |
| 11/21/1995 | US5468073 Bearing arrangement |
| 11/21/1995 | US5467592 Sectorized tubular structure subject to implosion |
| 11/14/1995 | US5465572 Multi-hole film cooled afterburner cumbustor liner |
| 11/08/1995 | EP0544764B1 Axisymmetric nozzle with gimbled unison ring |
| 11/07/1995 | US5463866 Supersonic jet engine installation and method with sound suppressing nozzle |
| 11/02/1995 | EP0679134A1 Radial four-blade thrust vector-------------------------------. |
| 10/31/1995 | US5461856 Divergent slave petal for sealing in variable geometry exhaust nozzles for gas turbine propulsion units |
| 10/25/1995 | EP0678160A1 Turbine exhaust gas anti-ice system |
| 10/04/1995 | EP0674748A1 Flap hinge arrangement for a convergent/divergent nozzle. |
| 10/04/1995 | EP0674747A1 Silencer |
| 09/21/1995 | DE4408260A1 Dichtung Seal |
| 09/12/1995 | US5448884 Mechanical lock for jet engine thrust reverser |
| 08/29/1995 | US5445392 Apparatus for sealing a clearance |
| 08/29/1995 | US5444912 Method for forming aircraft engine nacelle exhaust mixers and similar products |
| 08/22/1995 | US5442909 Control system for limiting the vector angle in an axisymmetric vectoring exhaust nozzle |
| 08/15/1995 | US5440875 Fixed geometry mixer/ejector suppression system for turbofan aircraft engines |
| 08/08/1995 | CA2071862C A turbofan engine fixed plug noise suppressor |
| 08/02/1995 | EP0664852A1 Mechanical lock for jet engine thrust reverser. |
| 08/01/1995 | US5437412 Variable geometry jet engine exhaust nozzle |
| 08/01/1995 | US5437411 Vectoring exhaust nozzle flap and seal positioning apparatus |
| 07/27/1995 | WO1995019075A3 Active muffler |
| 07/25/1995 | US5435489 Engine exhaust gas deflection system |
| 07/25/1995 | US5435128 Pyrotechnically driven nozzle restrictor |
| 07/25/1995 | US5435127 Method and apparatus for boosting ram airflow to an ejection nozzle |
| 07/20/1995 | WO1995019289A1 Engine exhaust gas deflection system |
| 07/18/1995 | US5433070 Flexible engine inlet duct mounting system |
| 07/13/1995 | WO1995019075A2 Active muffler |
| 07/11/1995 | US5431344 Sliding throat gas turbine engine nozzle |
| 07/11/1995 | US5431085 Thrust reverser actuator |
| 07/04/1995 | US5428954 System for suppressing engine exhaust noise |
| 06/13/1995 | US5423123 Method of making impingement/film cooling panels |
| 06/07/1995 | EP0656469A1 Security means for a thrust reverser |
| 05/30/1995 | US5419515 Thrust reverser for jet engines |
| 05/30/1995 | US5419117 Turbo jet/RAM jet propulsion system |
| 05/26/1995 | WO1995014163A1 Pyrotechnically driven nozzle restrictor |
| 05/24/1995 | EP0654598A1 Thrust reverser for a turbofan engine |
| 05/24/1995 | EP0654597A1 Variable geometry thrust vectoning means for a gas turbine |