| 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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| 10/30/2008 | DE102007019762A1 Schallschutzvorrichtung für ein Strahltriebwerk oder eine Turbine Acoustic shielding device for a jet engine or a turbine |
| 10/29/2008 | EP1985834A1 Flap valve for a cooling system in a turbojet |
| 10/29/2008 | EP1984616A1 A gas turbine engine |
| 10/29/2008 | CN101297107A Turbofan engine for stol aircraft |
| 10/29/2008 | CN101294522A Nuclear reactor and flying disk manufactured by the same |
| 10/27/2008 | CA2629798A1 Check valve for a cooling system in a turbine engine |
| 10/23/2008 | WO2008127260A1 Engine exhaust system with directional nozzle |
| 10/23/2008 | WO2008045053A3 Actuation of a turbofan engine bifurcation to change an effective nozzle exit area |
| 10/23/2008 | US20080256957 Joint for a shape memory material |
| 10/23/2008 | DE112006003493T5 Abgas-Dispergiervorrichtung Exhaust gas disperser |
| 10/22/2008 | CN101292083A Turbojet engine with attenuated jet noise |
| 10/22/2008 | CN100427736C Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions |
| 10/16/2008 | WO2008097247A3 Engine exhaust system |
| 10/16/2008 | US20080250771 Actuator Arrangement |
| 10/16/2008 | US20080250770 By-pass turbojet including a thrust reverser |
| 10/15/2008 | EP1980739A2 Bypass jet engine comprising a thrust reverser |
| 10/15/2008 | EP1980723A2 Out-flow margin protection for a gas turbine engine |
| 10/15/2008 | CN100425819C Steam booster of rocket propeller |
| 10/13/2008 | CA2629055A1 Bypass turbofan engine comprising a thrust reverser |
| 10/09/2008 | WO2008121542A1 Pintle-controlled propulsion system with external ring actuator |
| 10/09/2008 | US20080245072 Damping of Vibration of a Combustion Chamber By Resonators |
| 10/09/2008 | US20080245062 Passive cooling system for auxiliary power unit installation |
| 10/08/2008 | EP1978233A2 Actuator arrangement for a thrust reverser |
| 10/08/2008 | EP1978232A2 Variable area fan nozzle and thrust reverser |
| 10/08/2008 | EP1978231A2 Actuator arrangement |
| 10/08/2008 | CN100424334C Thrust reverser lock comprising locking device |
| 10/07/2008 | US7430867 Gas turbine multiple sectioned exhaust duct |
| 10/07/2008 | US7430852 Turbojet having a large bypass ratio |
| 10/02/2008 | US20080236167 Variable-section flow mixer for a double-flow turbojet for a supersonic airplane |
| 10/02/2008 | US20080236137 Acoustic flow straightener for turbojet engine fan casing |
| 10/01/2008 | EP1975399A2 Mode strut and divergent flap interface |
| 10/01/2008 | EP1975378A2 Linkage system with wear reduction |
| 10/01/2008 | EP1974140A2 Damped coil pin for attachment hanger hinge |
| 09/29/2008 | CA2618812A1 Variable area fan nozzle and thrust reverser |
| 09/25/2008 | US20080230629 Mode strut and divergent flap interface |
| 09/25/2008 | CA2676664A1 Self-calibration method for the electric jacks of a turbojet nacelle |
| 09/24/2008 | EP1972774A2 Coated variable area fan nozzle, engine, and corresponding manufacturing method |
| 09/24/2008 | CN101270703A Coated variable area fan nozzle |
| 09/23/2008 | CA2454808C Built-in test system for aircraft indication switches |
| 09/18/2008 | DE102008013993A1 Düse mit Giervektorsteuerung Nozzle with yaw vectoring |
| 09/18/2008 | CA2677395A1 Method for controlling electric motors of a thrust reverser |
| 09/17/2008 | EP1969222A1 Bearing-like structure to control deflections of a rotating component |
| 09/17/2008 | CN100419236C Gas turbine brush seal arrangement for cabin air supply |
| 09/16/2008 | CA2623644A1 Nozzle with yaw vectoring vane |
| 09/12/2008 | WO2008108847A1 Fan variable area nozzle for a gas turbine engine fan nacelle with drive ring actuation system |
| 09/12/2008 | WO2008107605A2 Aircraft nacelle incorporating a thrust-reversing device |
| 09/12/2008 | WO2008087261A3 Translatable thrust inverter for jet engine |
| 09/12/2008 | CA2676597A1 Aircraft nacelle incorporating a thrust-reversing device |
| 09/11/2008 | US20080217101 Method of Reducing Noise Emissions at the Rear of a Turboshaft Engine and Turboshaft Engine thus Improved |
| 09/10/2008 | EP1967701A2 Flutter sensing and control system for a gas turbine engine |
| 09/10/2008 | CN101263295A Method for attenuating the noise of a turbofan |
| 09/04/2008 | US20080213088 Stator for a Jet Engine, a Jet Engine Comprising Such a Stator, and an Aircraft Comprising the Jet Engine |
| 09/04/2008 | US20080210778 Aircraft engine exhaust shroud |
| 09/04/2008 | CA2676048A1 Method of manufacturing a cmc flow mixer lobed structure for a gas turbine aeroengine |
| 08/28/2008 | WO2008102079A2 Nacelle for aircraft jet engine and aircraft including such nacelle |
| 08/28/2008 | WO2008102067A1 Jack with integrated locking device |
| 08/28/2008 | US20080202847 Method For Attenuating the Noise of a Turbofan |
| 08/28/2008 | CA2678308A1 Jack with integrated locking device |
| 08/28/2008 | CA2674260A1 Nacelle for aircraft jet engine and aircraft including such nacelle |
| 08/27/2008 | EP1961944A2 Convergent divergent nozzle with slot cooled nozzle liner |
| 08/27/2008 | EP1961833A1 Thermal barrier coating systems and materials |
| 08/27/2008 | CN101253095A Dynamically self-locking catching device |
| 08/21/2008 | WO2008100712A2 Systems and methods for reducing noise from jet engine exhaust |
| 08/21/2008 | WO2008054500A3 Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 08/21/2008 | DE102007007568A1 Vorrichtung zur Steuerung der Düsenschubrichtung eines Raketentriebwerks Device for controlling the direction of thrust nozzle of a rocket engine |
| 08/19/2008 | US7412832 Method and apparatus for operating gas turbine engines |
| 08/14/2008 | WO2008095846A1 Device for acoustically treating turbine and combustion noise |
| 08/14/2008 | US20080190111 Thermoacoustic Oscillation Damping In Gas Turbine Combustors With Annular Plenum |
| 08/14/2008 | US20080190096 Fluid mixer with an integral fluid capture ducts forming auxiliary secondary chutes at the discharge end of said ducts |
| 08/13/2008 | EP1956225A2 Convergent divergent nozzle with edge cooled divergent seals |
| 08/13/2008 | EP1956224A2 Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system |
| 08/13/2008 | EP1185779B1 Apparatus and methods for active flow control of a nozzle exhaust plume |
| 08/12/2008 | US7409831 Provision of sealing in a jet engine for bleeding air to the cabin using a tube with a double ball joint |
| 08/07/2008 | WO2008093447A1 Low noise aircraft |
| 08/07/2008 | WO2008092427A1 Gas turbine comprising a guide ring and a mixer |
| 08/07/2008 | DE102007004741A1 Gasturbine mit einem Nachleitkranz und mit einem Mischer Gas turbine having a guide ring and with a mixer |
| 08/06/2008 | EP1952005A1 Control method for actuating a thrust reverser |
| 08/06/2008 | CN100408823C Connector assembly for mounting a gas turbine engine |
| 08/05/2008 | US7406821 Adapter device for a rocket engine nozzle having a movable diverging portion |
| 07/30/2008 | EP1950405A1 Variable-section flow mixer for a double-flow jet engine of a supersonic airplane |
| 07/26/2008 | CA2619561A1 Variable section flow mixer for dual flow turbojet for supersonic aircraft |
| 07/24/2008 | WO2008088328A1 Core reflex nozzle for turbofan engine |
| 07/24/2008 | WO2008087261A2 Translatable thrust inverter for jet engine |
| 07/24/2008 | CA2674927A1 Translatable thrust inverter for jet engine |
| 07/22/2008 | CA2204386C Self-locking sealing device |
| 07/17/2008 | US20080168762 Device for actuating mobile cowls equipping a thrust reverser |
| 07/16/2008 | EP1944496A2 Variable area nozzle with woven sleeve extension |
| 07/16/2008 | EP1606504B1 Toggle interlocked thrust reverser |
| 07/10/2008 | WO2008080567A1 Jet engine |
| 07/10/2008 | WO2008021618A3 Multiple vane variable geometry nozzle |
| 07/10/2008 | US20080163606 Variable area nozzle with woven sleeve extension |
| 07/10/2008 | DE102007001622A1 Strahltriebwerk Jet engine |
| 07/09/2008 | EP1942268A2 Nozzle arrangement |
| 07/09/2008 | EP1942267A2 Exhaust nozzle assembly |
| 07/09/2008 | EP1942266A2 Method of operating an exhaust nozzle assembly |
| 07/09/2008 | EP1941148A1 Turbofan engine for stol aircraft |
| 07/08/2008 | US7395657 Flade gas turbine engine with fixed geometry inlet |
| 07/03/2008 | US20080156900 Exhaust nozzle assembly |
| 07/02/2008 | EP1939438A2 Duct burning mixed flow turbofan |
| 07/02/2008 | EP1937954A1 Turbojet engine with attenuated jet noise |