| 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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| 10/20/2009 | CA2471074C Infrared suppressing two dimensional vectorable single expansion ramp nozzle |
| 10/15/2009 | WO2009125157A2 Turbofan engine nacelle |
| 10/15/2009 | US20090255269 Gas Turbine Engine Systems Involving Variable Nozzles with Sliding Doors |
| 10/14/2009 | EP2108806A1 Gas turbine engine systems involving variable nozzles with sliding doors |
| 10/14/2009 | CN101558230A Translatable thrust inverter for jet engine |
| 10/13/2009 | US7603207 Surrogate air processor |
| 10/13/2009 | US7600384 Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl |
| 10/08/2009 | WO2009122037A2 Device for reducing turboprop infrared emissions |
| 10/08/2009 | WO2009122026A1 Bypass turbojet engine nacelle |
| 10/08/2009 | WO2009101274A3 Control system for turbojet engine nacelle |
| 10/08/2009 | CA2717357A1 Device for reducing turboprop infrared emissions |
| 10/06/2009 | US7596951 Exhaust nozzle for a gas turbine engine |
| 10/01/2009 | WO2009118472A1 Trailing edge for an aircraft engine, of the type with moving chevrons |
| 10/01/2009 | US20090241550 Gas Turbine Engine Systems Involving Variable Nozzles with Flexible Panels |
| 10/01/2009 | US20090241549 Subsonic and stationary ramjet engines |
| 10/01/2009 | US20090241505 Re-heat combustor for a gas turbine engine |
| 10/01/2009 | CA2713183A1 Trailing edge for an aircraft engine, of the type with moving chevrons |
| 09/30/2009 | CN100545037C Annular acoustic panel |
| 09/24/2009 | US20090235643 Valve system for a gas turbine engine |
| 09/24/2009 | US20090235641 T-Jet |
| 09/24/2009 | US20090235638 Variable area nozzle assisted gas turbine engine restarting |
| 09/24/2009 | DE102004007145B4 Strömungsleitelement und eine damit ausgestattete strömungstechnische Anlage Flow guide and a fluidic system equipped therewith |
| 09/23/2009 | EP2103799A2 Rocket nozzle and control method for combustion of the exhaust gas flow in rocket engine |
| 09/23/2009 | EP2103784A2 Valve system for a gas turbine engine |
| 09/23/2009 | EP2102480A2 Translatable thrust inverter for jet engine |
| 09/23/2009 | CN101537397A Fuel prefilming air atomizer spray nozzle |
| 09/23/2009 | CN100543289C Metal sheet comprising means for fixing to a support and a seal |
| 09/23/2009 | CN100543283C Gas turbine engine component having bypass circuit |
| 09/22/2009 | US7591647 Support structure |
| 09/22/2009 | CA2516437C Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 09/22/2009 | CA2511432C Thrust reverser comprising optimised deflector gratings |
| 09/17/2009 | WO2009112749A2 Thrust reverser for bypass turbojet engine nacelle |
| 09/17/2009 | WO2009053560A3 Structure for thrust inverter |
| 09/17/2009 | US20090230212 Pintle-Controlled Propulsion System With External Ring Actuator |
| 09/17/2009 | US20090229241 Hybrid missile propulsion system with reconfigurable multinozzle grid |
| 09/15/2009 | US7587899 Shape memory alloy actuated adaptive exhaust nozzle for jet engine |
| 09/15/2009 | CA2494433C One-piece flame-retention nozzle arm for a turbofan after-burner |
| 09/15/2009 | CA2436993C Aero-engine exhaust jet noise reduction assembly |
| 09/11/2009 | WO2006011978A3 Propulsion device with enclosed plenum |
| 09/09/2009 | EP2098704A2 Variable area fan nozzle fan flutter management system |
| 09/09/2009 | CN101529073A Thrust reverser with grids for jet engine |
| 09/09/2009 | CN101529072A Cascade-type thrust reverser for jet engine |
| 09/08/2009 | US7584615 Method of improving the ignition performance of an after-burner device for a bypass turbojet, and an after-burner device of improved ignition performance |
| 09/03/2009 | WO2009107646A1 Noise reducing device, and jet propulsion system |
| 09/03/2009 | WO2009106763A2 Twelve-hour structure for thrust reverser, in particular with grids |
| 09/03/2009 | WO2009087282A3 Door-type thrust reverser for a jet engine |
| 09/03/2009 | US20090217671 Exhaust nozzle seal with segmented basesheet |
| 09/03/2009 | US20090217670 Exhaust nozzle seal with segmented basesheet disposed between side rails |
| 09/03/2009 | DE102008011502A1 Düsenerweiterung und Verfahren zur Herstellung einer Düsenerweiterung Expansion nozzle and method of making a nozzle extension |
| 09/03/2009 | CA2706375A1 Twelve-hour structure for thrust reverser, in particular with grids |
| 09/02/2009 | EP2096292A2 Exhaust nozzle seal with segmented basesheet disposed between side rails |
| 09/02/2009 | EP2096291A1 Exhaust nozzle seal with segmented basesheet |
| 09/02/2009 | CN101523041A Jet engine nacelle for an aircraft and aircraft comprising such a nacelle |
| 09/01/2009 | US7581692 Fluidic chevrons and configurable thermal shield for jet noise reduction |
| 09/01/2009 | US7581400 Elbow-shaped propulsion gas exhaust assembly in an aircraft |
| 09/01/2009 | US7581399 Damped coil pin for attachment hanger hinge |
| 09/01/2009 | US7581385 Metering sheet and iso-grid arrangement for a non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct |
| 09/01/2009 | US7581384 Turbomachine nozzle cover provided with triangular patterns having a point of inflexion for reducing jet noise |
| 09/01/2009 | US7581382 Gas turbine engine air valve assembly |
| 09/01/2009 | US7581381 Ducted air power plant |
| 09/01/2009 | US7581301 Method for attaching a non-metal component to a metal component |
| 08/27/2009 | WO2009103905A1 Nacelle for aircraft engine having a nozzle with a variable section |
| 08/27/2009 | US20090211258 Rocket nozzles for unconventional vehicles |
| 08/27/2009 | US20090211224 Outlet device for a jet engine and a craft comprising such an outlet device |
| 08/27/2009 | CA2705136A1 Nacelle for aircraft engine having a nozzle with a variable section |
| 08/26/2009 | EP2093407A2 Gas turbine engine with variable area fan nozzle bladder system and method of varying such fan nozzle exit area |
| 08/26/2009 | EP2092184A1 A liner for a turbine section, a turbine section, a gas turbine engine and an aeroplane provided therewith |
| 08/26/2009 | CN101517219A Aircraft propulsion assembly comprising a jet pipe with a notched trailing edge |
| 08/25/2009 | US7578369 Mixed-flow exhaust silencer assembly |
| 08/25/2009 | US7578133 Reduced radar cross section exhaust nozzle assembly |
| 08/25/2009 | US7578132 Gas turbine engine exhaust nozzle |
| 08/20/2009 | WO2009102528A1 Stave and ring cmc nozzle |
| 08/20/2009 | WO2009101370A1 System for controlling a plurality of functions of a turbojet engine |
| 08/20/2009 | WO2009101274A2 Control system for turbojet engine nacelle |
| 08/20/2009 | WO2009029401A3 Variable area fan nozzle with bypass flow |
| 08/20/2009 | US20090205312 Swept fan ramp for pivot door thrust reverser |
| 08/20/2009 | CA2714622A1 System for controlling a plurality of functions of a turbojet engine |
| 08/20/2009 | CA2711836A1 Control system for turbojet engine nacelle |
| 08/19/2009 | EP2090769A1 Apparatus, method and system for gas turbine engine noise reduction |
| 08/19/2009 | CN100529544C Multihole facing of combustor lining for gas turbine |
| 08/13/2009 | US20090199565 Stave and ring cmc nozzle |
| 08/11/2009 | US7571610 Extendible exhaust nozzle bell for a rocket engine |
| 08/05/2009 | EP2084386A2 Combined cycle missile engine system |
| 08/05/2009 | EP2084385A1 Thrust reverser with grids for jet engine |
| 08/05/2009 | EP2084063A1 Jet engine nacelle member |
| 08/05/2009 | EP2084062A1 Side-opening jet engine nacelle |
| 08/05/2009 | CN101501319A Engine exhaust system with directional nozzle |
| 08/05/2009 | CN100523472C Axial symmetric vector spray-pipe A9 action emergency resetting hydraulic system |
| 08/04/2009 | US7568348 Nozzle assembly for rocket and ramjet applications |
| 07/30/2009 | WO2009092872A2 Monitoring system and monitoring method |
| 07/30/2009 | WO2008110677A3 Method for controlling electric motors of a thrust reverser |
| 07/30/2009 | CA2704552A1 Control and monitoring system and method |
| 07/29/2009 | EP2021610B1 Turbojet nacelle equipped with means for reducing the noise produced by said turbojet |
| 07/23/2009 | WO2009090319A1 Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator |
| 07/23/2009 | WO2009034247A8 System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 07/23/2009 | WO2009034246A8 System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 07/23/2009 | WO2009034245A8 Method and system for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 07/23/2009 | CA2700184A1 Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator |
| 07/22/2009 | EP1402166B1 Rocket vehicle thrust augmentation within divergent section of nozzle |
| 07/21/2009 | US7562520 Method for opening a mobile cowl equipping a thrust reverser |