| 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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| 08/12/2004 | WO2004068035A2 Heat shield element, combustion chamber and gas turbine |
| 08/12/2004 | WO2004046533A3 Bifold door thrust reverser |
| 08/12/2004 | US20040154283 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 08/12/2004 | US20040154282 Propulsion system |
| 08/11/2004 | CN1519170A Electromechanical turbojet thrust reverser with containuous position control |
| 08/10/2004 | US6772857 Acoustically resistive layer for an acoustical attenuation panel, panel using such a layer |
| 08/05/2004 | WO2003099654A3 Bifurcated turbofan exhaust nozzle |
| 08/04/2004 | EP1322854A4 Apparatus, method and system for gas turbine engine noise reduction |
| 07/29/2004 | US20040146399 Coolable segment for a turbomachinery and combustion turbine |
| 07/28/2004 | EP1441180A1 Heatshield, combustion chamber and gas turbine |
| 07/28/2004 | EP1440004A1 Passive cooling system for auxiliary power unit installation |
| 07/28/2004 | CN1515463A Turbojet engine electromechanical thrust reverse with synchronous locking device |
| 07/22/2004 | WO2004061286A1 Apparatus and method for controlling primary fluid flow using secondary fluid flow injection |
| 07/22/2004 | US20040140397 Scarf nozzle for a jet engine and method of using the same |
| 07/22/2004 | US20040139726 Turbojet electromechanical thrust reverser with servo-controlled door displacement |
| 07/22/2004 | US20040139725 Turbojet electromechanical thrust reverser with synchronized locking devices |
| 07/22/2004 | US20040139724 Maintenance and inhibition plate for a thrust reverser |
| 07/22/2004 | US20040139721 Rocket engine member and a method for manufacturing a rocket engine member |
| 07/21/2004 | EP1438494A2 Confluent variable exhaust nozzle |
| 07/21/2004 | CN1158454C Hollow nozzle-actuating ring |
| 07/20/2004 | US6764045 Bi-fold thrust reverser door assembly |
| 07/20/2004 | US6763652 Variable torque split aircraft gas turbine engine counter rotating low pressure turbines |
| 07/15/2004 | WO2004059157A1 Thrust reverser comprising optimised deflector gratings |
| 07/14/2004 | EP1436497A1 Jet engine thrust reverser system having torque limited synchronization |
| 07/13/2004 | US6761245 Tubular acoustic attenuation piece for an aircraft jet engine air intake |
| 07/06/2004 | US6758032 System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans |
| 07/01/2004 | US20040123460 Method for manufacturing outlet nozzles for rocket engines |
| 06/30/2004 | CN1155805C Constant pressure mechanism of contact |
| 06/24/2004 | WO2004053321A1 Thurst reverser system power drive unit with dual sequential torque decoupler |
| 06/24/2004 | US20040118974 Electromechanical turbojet thrust reverser with continuous position control |
| 06/24/2004 | US20040118104 Methods and apparatus for generating gas turbine engine thrust |
| 06/23/2004 | EP1431563A1 Methods and apparatus for generating gas turbine engine thrust |
| 06/23/2004 | EP1430212A1 Converging nozzle thrust reverser |
| 06/22/2004 | US6751944 Confluent variable exhaust nozzle |
| 06/17/2004 | US20040112040 Thrust reverser system power drive unit with dual sequential torque decoupler and method |
| 06/16/2004 | EP1427933A1 Device for controlling propulsive flow mixture for aircraft reactor |
| 06/10/2004 | US20040107690 Gas turbine exhaust diffuser |
| 06/09/2004 | EP1425504A2 Device for mixing two flows of fluid, which are initially guided separate from one another, in a two-circuit reaction engine |
| 06/09/2004 | DE20317029U1 Double-axis vector control for model turbines, electric motors, and small turbines for civil and military purposes uses truncated cone to deflect water/air flows without delay |
| 06/08/2004 | US6745570 Methods and apparatus for sealing gas turbine engine nozzles using a flap system |
| 06/03/2004 | WO2004046533A2 Bifold door thrust reverser |
| 06/03/2004 | US20040103640 Outlet nozzle and a method for manufacturing an outlet nozzle |
| 06/03/2004 | US20040103639 Rocket engine member and a method for manufacturing a rocket engine member |
| 06/03/2004 | US20040103638 Rocket engine member and method for manufacturing a rocket engine member |
| 06/03/2004 | CA2501496A1 Bifold door thrust reverser |
| 06/02/2004 | EP1423596A1 Trust reverser actuator including an integrated locking mechanism |
| 06/02/2004 | CN1500693A Electromechanical thrust reverser for a turboreactor used to control door movement |
| 06/01/2004 | CA2221083C Electric control system for thrust reverser of jet turbine engine |
| 05/25/2004 | US6739050 Methods for retaining gas turbine engine nozzle basesheets |
| 05/18/2004 | US6735936 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 05/13/2004 | US20040088967 Suppression of part of the noise from a gas turbine engine |
| 05/13/2004 | US20040088858 Flow directing element and a method of manufacturing a flow directing element |
| 05/12/2004 | EP1418331A2 Suppression of part of the noise from a gas turbine engine |
| 05/11/2004 | CA2126539C Turbofan engine exhaust mixing area modification for improved noise reduction |
| 05/06/2004 | US20040083713 Jet blade ejector nozzle |
| 05/06/2004 | EP1416147A1 Cascadeless fan thrust reverser with configuration control of the discharged air flow |
| 05/04/2004 | US6729575 Propulsion system for a vertical and short takeoff and landing aircraft |
| 04/29/2004 | WO2004036020A2 Thrust vectoring and variable exhaust area for jet engine nozzle |
| 04/29/2004 | US20040079073 Cascadeless fan thrust reverser with plume control |
| 04/29/2004 | CA2495804A1 Thrust vectoring and variable exhaust area for jet engine nozzle |
| 04/28/2004 | EP1413737A1 Jet engine electromechanical thrust reverser with synchronisation of its locking elements |
| 04/28/2004 | EP1413736A1 Electromecanical thrust reverser for a turbofan engine with thrust reverser doors |
| 04/28/2004 | EP1413735A1 Electromechanical thrust reverser with a permanent position control for an aircraft engine |
| 04/28/2004 | EP1413734A1 Maintenance and inhibition plate for a thrust reverser |
| 04/28/2004 | CN1492128A Method and device for support high temperature pipeline |
| 04/27/2004 | US6725541 Flow directing element and a method of manufacturing a flow directing element |
| 04/22/2004 | WO2004033885A1 Electro-hydraulic thrust reverser lock actuation system |
| 04/22/2004 | US20040076512 Noise reduction conduit for static components in aircraft engines |
| 04/22/2004 | US20040074224 Convergent/divergent segmented exhaust nozzle |
| 04/21/2004 | EP1409866A1 Thrust reverser position determination system and method |
| 04/20/2004 | US6723972 Method and apparatus for planar actuation of a flared surface to control a vehicle |
| 04/20/2004 | CA2204078C Improvements in axisymmetric nozzles of variable geometry and orientation of the flow, which are intended for gas turbine engines |
| 04/15/2004 | US20040068981 Exhaust mixer and apparatus using same |
| 04/15/2004 | US20040068978 Bifold door thrust reverser |
| 04/15/2004 | US20040068977 Thrust reverser for a jet engine and hydraulic actuator |
| 04/15/2004 | DE3005804B3 Rectangular adjusting thrust nozzle for gas turbine drive with adjusting flaps adjusted parallel to each other to set thrust vector for fast maneuverability |
| 04/14/2004 | EP1407193A1 Coolable segment for a turbomachinery and combustion turbine |
| 04/13/2004 | US6718752 Deployable segmented exhaust nozzle for a jet engine |
| 04/08/2004 | US20040065502 Noise reducing apparatus and exhaust nozzle for jet engine |
| 04/07/2004 | EP1192348B1 Engine nozzle arrangement for an aircraft |
| 04/07/2004 | EP1045971B1 Heat exchanger in composite material and method for making same |
| 04/07/2004 | EP0988446B1 Device for anchoring a member activating an adjustable nozzle |
| 04/06/2004 | US6715297 Methods and apparatus for supporting high temperature ducting |
| 04/01/2004 | US20040060278 Passive cooling system for auxiliary power unit installation |
| 03/31/2004 | EP1403485A2 Gas turbine engine with low pressure turbine comprising counter rotatable low pressure inner and outer shaft turbines |
| 03/31/2004 | EP1402166A1 Rocket vehicle thrust augmentation within divergent section of nozzle |
| 03/25/2004 | US20040055311 Methods and apparatus for supporting high temperature ducting |
| 03/25/2004 | US20040055276 Variable torque split aircraft gas turbine engine counter rotating low pressure turbines |
| 03/24/2004 | EP1400681A2 Methods and apparatus for supporting high temperature ducting |
| 03/24/2004 | EP1399661A1 Pivot fairing thrust reverser |
| 03/24/2004 | CN1143076C Supersonic coherent gas jet for providing gas into liquid |
| 03/24/2004 | CN1143057C Vectoring nozzle calibration |
| 03/18/2004 | WO2004022963A1 Thrust reverser actuator with an automatic relock and lock drop prevention mechanism |
| 03/18/2004 | CA2497914A1 Thrust reverser actuator with an automatic relock and lock drop prevention mechanism |
| 03/17/2004 | EP1398493A1 Thrust reverser for a jet engine and hydraulic actuator |
| 03/17/2004 | EP1398473A1 Acoustic attenuation layer for an acoustic attenuation panel, and a panel with such a layer |
| 03/17/2004 | EP1398472A1 Tubular acoustic attenuation piece for the air inlet of an aircraft engine |
| 03/17/2004 | EP1397586A1 Exhaust flow guide for jet noise reduction |
| 03/16/2004 | US6705547 Active noise reducing nozzle |
| 03/11/2004 | US20040045766 Acoustically resistive layer for an acoustical attenuation panel, panel using such a layer |