| 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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| 07/07/2011 | WO2011082233A1 Exhaust for a gas turbine engine |
| 07/06/2011 | CN1683772B Turbine shroud |
| 06/29/2011 | CN102108915A Turbofan engine for stol aircraft |
| 06/28/2011 | US7967219 Thrust nozzle for a gas turbine engine |
| 06/28/2011 | US7966828 Variable area nozzle with woven sleeve extension |
| 06/28/2011 | US7966827 Gas turbine engine with fan variable area nozzle having a rotational valve system |
| 06/28/2011 | US7966826 Systems and methods for reducing noise from jet engine exhaust |
| 06/28/2011 | US7966825 Exhaust eductor system with a recirculation baffle |
| 06/28/2011 | US7966824 Jet engine nozzle exit configurations and associated systems and methods |
| 06/23/2011 | WO2011073558A1 Reverse thrust device |
| 06/23/2011 | WO2011073551A1 Supporting structure for thrust reverser, in particular having cascades |
| 06/23/2011 | WO2011073549A1 Stub frame for a cascade thrust reverser structure |
| 06/23/2011 | CA2781444A1 Stub frame for a cascade thrust reverser structure |
| 06/23/2011 | CA2780666A1 Supporting structure for thrust reverser, in particular having cascades |
| 06/22/2011 | CN102105670A Dual-flow turbine engine for aircraft with low noise emission |
| 06/22/2011 | CN102105669A Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle |
| 06/22/2011 | CN102105666A Method and device for implementing the thrust reversers of an aircraft |
| 06/21/2011 | US7963099 Fluted chevron exhaust nozzle |
| 06/21/2011 | CA2726503A1 Integrated nacelle assembly |
| 06/16/2011 | US20110139897 Mobile thrust reverser cowl and thrust reverser provided with such a cowl |
| 06/16/2011 | US20110139540 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle |
| 06/15/2011 | EP2333288A2 Thermally actuated venting system for a compartment of an aircraft gas turbine engine |
| 06/15/2011 | EP2333287A1 Vectoring transition duct for turbine engine |
| 06/15/2011 | EP2333286A1 Vectoring transition duct for turbine engine |
| 06/15/2011 | EP2333282A2 Variable area fan nozzle stiffeners and placement |
| 06/14/2011 | US7958733 Jet engine exhaust nozzle flow effector |
| 06/14/2011 | CA2660211C Gas turbine engine exhaust duct ventilation |
| 06/14/2011 | CA2444987C Electromechanical thrust reverser for a turboreactor with permanent position control |
| 06/14/2011 | CA2440527C Variable torque split aircraft gas turbine engine counter rotating low pressure turbines |
| 06/09/2011 | WO2011067520A1 Assembly for an aircraft turbojet engine comprising a thrust reversal cowl |
| 06/09/2011 | US20110133026 Extended plug cold plate |
| 06/09/2011 | US20110131948 Engine Exhaust System with Directional Nozzle |
| 06/09/2011 | CA2780058A1 Assembly for an aircraft turbojet engine comprising a thrust reversal cowl |
| 06/07/2011 | US7954759 Control system for the nacelle of a turboreactor |
| 06/07/2011 | CA2464188C Passive cooling system for auxiliary power unit installation |
| 06/03/2011 | WO2011066368A2 Variable area fan nozzle cowl airfoil |
| 06/03/2011 | WO2011066365A2 Variable area fan nozzle bearing track |
| 06/03/2011 | WO2011064962A1 Railway-train emergency braking apparatus, railway-train emergency braking system, and railway train provided with railway-train emergency braking apparatus |
| 06/03/2011 | WO2011064479A1 Thrust inverter |
| 06/03/2011 | CA2776209A1 Thrust inverter |
| 06/02/2011 | US20110127353 Aircraft nacelle that incorporates a thrust reversal device |
| 06/02/2011 | US20110126544 Air flow passage liner |
| 06/02/2011 | US20110126512 Turbofan gas turbine engine aerodynamic mixer |
| 06/01/2011 | EP2327869A2 Turbofan gas turbine engine aerodynamic mixer |
| 06/01/2011 | EP2326555A1 Nacelle with a variable nozzle section |
| 06/01/2011 | CN101517219B Aircraft propulsion assembly comprising a jet pipe with a notched trailing edge |
| 05/31/2011 | US7950237 Managing spool bearing load using variable area flow nozzle |
| 05/31/2011 | US7950236 Exhaust duct and tail cone attachment of aircraft engines |
| 05/31/2011 | US7950218 Bypass turbomachine with artificial variation of its throat section |
| 05/31/2011 | CA2445851C Electromechanical thrust reverser for a turboreactor for synchronizing locking mechanisms |
| 05/31/2011 | CA2434492C Assist and back-up for electrical auxiliary drive |
| 05/26/2011 | US20110120084 Gas turbine engine air valve assembly |
| 05/25/2011 | EP2325443A2 Attaching ceramic matrix composite to high temperature gas turbine structure |
| 05/25/2011 | EP2129901B1 Thrust reverser for a jet engine |
| 05/25/2011 | CN201843699U Metal diaphragm spray pipe structure of small solid engine |
| 05/25/2011 | CN102069913A Method for improving power of propeller and jet engine by increasing number of extra water molecules |
| 05/24/2011 | US7946383 Acoustic load mitigator |
| 05/24/2011 | US7946105 Bi-directional locking ring assembly for aircraft thrust reverser manual drive unit |
| 05/24/2011 | CA2515849C Confluent exhaust nozzle |
| 05/24/2011 | CA2478780C Aircraft equipped with thrust reversers |
| 05/24/2011 | CA2476503C Duplex mixer exhaust nozzle |
| 05/19/2011 | WO2011058041A1 Metal annular connecting structure for an aircraft turbine engine |
| 05/19/2011 | WO2010088069A3 Thermally balanced materials |
| 05/19/2011 | WO2010088068A3 Thermally balanced aero structures |
| 05/19/2011 | CA2780548A1 Metal annular connecting structure for an aircraft turbine engine |
| 05/18/2011 | EP2321515A1 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle |
| 05/18/2011 | EP2321514A2 Flexible abutment links for attaching a part made of cmc |
| 05/18/2011 | CN101595292B Method for controlling electric motors of a thrust reverser |
| 05/17/2011 | US7945353 Adaptive control in the presence of input constraints |
| 05/12/2011 | WO2011055056A1 Reverse thrust device |
| 05/12/2011 | US20110108665 Method and device for implementing the thrust reversers of an aircraft |
| 05/12/2011 | US20110108357 Acoustic panel for an ejector nozzle |
| 05/12/2011 | CA2776262A1 Reverse thrust device |
| 05/11/2011 | EP2318683A2 Acoustic attenuation panel for aircraft engine nacelle |
| 05/11/2011 | EP2198143B1 Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator |
| 05/11/2011 | EP1924498B1 Dynamically self-locking catching device |
| 05/11/2011 | CN102052254A Power generator utilizing wind energy and fuel chemical energy |
| 05/11/2011 | CN102050228A Method for diagnosing spraying tube blocking fault by using combination of spinning top and air spraying time |
| 05/05/2011 | WO2011052642A1 Noise reduction device with chamber |
| 05/05/2011 | WO2011052566A1 Noise reduction device |
| 05/05/2011 | WO2011051611A1 Low-thickness thermostructural composite material part, and manufacture method |
| 05/05/2011 | US20110101159 Nested fairing thrust reverser |
| 05/05/2011 | US20110101158 Thrust Reversers Including Monolithic Components |
| 05/05/2011 | DE102009042163A1 Gas stream producing device i.e. aircraft engine, manufacturing method, involves selecting Mach number such that gas stream fulfills two preset conditions of velocity of sound and speed of gas stream in surrounding |
| 05/05/2011 | DE102009013150B4 Bauteil zum Einsatz in Heißgasströmungen Component for use in streams of hot gas |
| 05/05/2011 | CA2779149A1 Noise reduction system with chamber |
| 05/05/2011 | CA2779050A1 Noise reduction system |
| 05/05/2011 | CA2778383A1 Low-thickness thermostructural composite material part, and manufacture method |
| 05/04/2011 | EP2317108A2 A boundary layer energiser |
| 05/04/2011 | EP2317107A2 A boundary layer energiser |
| 05/04/2011 | EP2315928A1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 04/28/2011 | DE112009001558T5 Ausstromdüse mit Doppelvorsprüngen Ausstromdüse with double projections |
| 04/28/2011 | DE102009048201A1 Drive mechanism for e.g. fixed wing aircraft, has lifting drive turbine actuated by exhaust gas stream of radiation jet engine, and device increasing exhaust gas temperature of burners and arranged in section of exhaust gas channel |
| 04/27/2011 | CN102037233A Method for synchronizing the actuators of a movable thrust reverser cowl |
| 04/27/2011 | CN102037232A Device for reducing noise generated by an aircraft jet engine with curve ducts |
| 04/27/2011 | CN102037231A Device with secondary jets reducing the noise generated by an aircraft jet engine |
| 04/27/2011 | CN102032072A Exhaust system for gaseous film cooling central cone of turbofan aircraft engine |
| 04/21/2011 | US20110088403 Nozzle-area ratio float bias |
| 04/21/2011 | US20110088369 Method for synchronizing the actuators of a movable thrust reverser cowl |
| 04/20/2011 | EP2311731A1 Thurst reverser actuation |