| 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) |
|---|
| 07/03/2013 | EP2609296A2 Method for mounting shielding on a turbine casing, and mounting assembly for implementing same |
| 07/02/2013 | CA2766010C Passive cooling system for auxiliary power unit installation |
| 06/30/2013 | CA2800464A1 Gas turbine engine with low stage count low pressure turbine |
| 06/30/2013 | CA2800001A1 Gas turbine engine compressor arrangement |
| 06/29/2013 | CA2800049A1 Seal for a variable area fan nozzle |
| 06/27/2013 | WO2013095765A1 Gas turbine duct blocker with rotatable vane segments |
| 06/27/2013 | WO2013095764A1 Gas turbine duct blocker that includes a duct blocker rotor with a plurality of roller elements |
| 06/27/2013 | WO2013093283A1 Door for a thrust reverser with doors |
| 06/27/2013 | US20130161414 Actuation system for a translating variable area fan nozzle |
| 06/27/2013 | DE102011113784A1 Disc shaped vertical lifting turbocompressor for turbojet engine of aircraft, has combustion chamber which is arranged on the tangent line of rotary compressor for adjusting the time required for flow of gas through combustion chamber |
| 06/27/2013 | CA2858504A1 Door for a thrust reverser with doors |
| 06/26/2013 | EP2607676A2 Dual function cascade integrated variable area fan nozzle and thrust reverser |
| 06/26/2013 | EP2607631A2 Variable area fan nozzle with drive system monitoring |
| 06/26/2013 | EP2606217A1 Beam for a cascade thrust reverser |
| 06/26/2013 | CN103174547A Mixer suitable for binary spray tube |
| 06/26/2013 | CN101952580B System for controlling a plurality of functions of a turbojet engine |
| 06/25/2013 | US8469141 Acoustic damping device for use in gas turbine engine |
| 06/21/2013 | CA2798660A1 Dual function cascade integrated variable area fan nozzle and thrust reverser |
| 06/20/2013 | WO2012071166A3 Integrated variable geometry flow restrictor and heat exchanger |
| 06/19/2013 | EP2604811A2 Energy-absorbing fan case for a gas turbine engine |
| 06/19/2013 | CN102050228B Method for diagnosing spraying tube blocking fault by using combination of spinning top and air spraying time |
| 06/18/2013 | US8464512 Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator |
| 06/13/2013 | WO2013084135A1 Element for sound absorption mounted on aircraft components |
| 06/13/2013 | WO2013083937A1 Method for creating a connecting element positioned between two components of a structure, connecting element and bypass turbojet engine comprising such a connecting element |
| 06/13/2013 | WO2013083908A1 A convergent-divergent turbo-machine nozzle |
| 06/13/2013 | US20130146708 Case assemblies with common controls |
| 06/13/2013 | US20130146393 Method for producing an acoustic treatment panel |
| 06/13/2013 | US20130145768 Case assembly with fuel or hydraulic driven vafn actuation systems |
| 06/13/2013 | US20130145743 Case assembly with fuel driven actuation systems |
| 06/13/2013 | DE102011120855A1 Schubvektorsteuerung Thrust vector control |
| 06/13/2013 | CA2857927A1 A convergent-divergent turbo-machine nozzle |
| 06/13/2013 | CA2856105A1 Element for sound absorption mounted on aircraft components |
| 06/12/2013 | EP2602464A2 Common control for thrust reverser and variable area fan nozzle |
| 06/12/2013 | EP2602457A2 Fuel driven actuation systems for thrust reverser |
| 06/12/2013 | EP2602456A2 Fuel or hydraulic fluid driven actuation systems for variable area fan nozzles |
| 06/12/2013 | CN202991267U Device for increasing reverse thrust efficiency of aeroengine by directional expansion boosting |
| 06/12/2013 | CN103154489A Aircraft propulsion assembly |
| 06/12/2013 | CN103154441A Device for connecting a thrust reverser front frame to a fan casing and nacelle incorporating such a device |
| 06/12/2013 | CN103154435A 推力反向器 Thrust reverser |
| 06/12/2013 | CN101675226B Acoustic panel having a variable acoustic characteristic |
| 06/11/2013 | US8459036 Aircraft nozzle having actuators capable of changing a flow area of the aircraft nozzle |
| 06/11/2013 | US8459035 Gas turbine engine with low fan pressure ratio |
| 06/06/2013 | WO2013001185A3 Tertiary locking assembly for a thrust reverser |
| 06/06/2013 | US20130142650 Turbine device |
| 06/05/2013 | EP2599970A2 Reduction of heating effects of an impinging exhaust plume |
| 06/05/2013 | EP2599960A1 Turbomachine component machining method |
| 06/05/2013 | EP2599078A2 Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 06/05/2013 | CN103133180A Low jet flow noise spray pipe and turbofan engine including the same |
| 06/05/2013 | CN101737194B Adjustable front duct ejector in variable cycle engine mode switching mechanism |
| 06/05/2013 | CN101709679B Adjustable rear culvert channel injector in mode switching mechanism of variable cycle engine |
| 06/04/2013 | US8453458 Gas turbine engine variable exhaust nozzle |
| 06/04/2013 | US8453457 Nozzle plasma flow control utilizing dielectric barrier discharge plasma actuators |
| 06/04/2013 | US8453429 System and method for assembling a thrust reverser for a gas turbine propulsion system |
| 05/30/2013 | WO2013076417A1 Mechanical system for a turbine engine, turbine engine, and method for attaching a mechanical system within a turbine engine |
| 05/29/2013 | CN103124833A Method for mounting shielding on a turbine casing, and mounting assembly for implementing same |
| 05/29/2013 | CN102022222B Silencer |
| 05/29/2013 | CN101372926B Dual-flow turbomachine with jet noise reduction |
| 05/28/2013 | US8448420 Aircraft nacelle that incorporates a device for reversing thrust |
| 05/23/2013 | US20130126638 Thrust reverser having an aerodynamic coupling for a front frame |
| 05/22/2013 | EP2594752A2 Retractable exhaust liner segment for gas turbine engines |
| 05/21/2013 | US8443931 Noise reduction of supersonic jet engines |
| 05/21/2013 | US8443586 Variable area fan nozzle bearing track |
| 05/21/2013 | CA2612117C Aircraft pod and aircraft equipped with at least one such pod |
| 05/21/2013 | CA2582028C Mixer for separate-stream nozzle |
| 05/16/2013 | WO2013068664A1 Thrust reverser having twin doors |
| 05/16/2013 | WO2013068663A1 Thrust reverser device |
| 05/16/2013 | CA2851891A1 Thrust reverser having twin doors |
| 05/16/2013 | CA2851671A1 Thrust reverser device |
| 05/15/2013 | EP2591224A1 Thrust reverser having an aerodynamic coupling for a front frame |
| 05/15/2013 | CN101657628B Grid thrust reverser cover comprising a seal support and associated seal |
| 05/14/2013 | US8439305 Non-handed thrust reverser for installation on handed aircraft gas turbine propulsion engines |
| 05/14/2013 | US8438835 Methods and apparatus for mixing fluid in turbine engines |
| 05/14/2013 | CA2572698C Aircraft jet engine provided with a device for reducing propulsion jet noise |
| 05/10/2013 | WO2013064762A1 Cascade-type thrust reverser with one-piece mobile cowl |
| 05/10/2013 | CA2850704A1 Cascade-type thrust reverser with one-piece mobile cowl |
| 05/09/2013 | US20130112776 Nozzle arrangement and method of making the same |
| 05/09/2013 | US20130112497 Turbojet engine nacelle |
| 05/08/2013 | CN103097706A Locking/unlocking device for a thrust reverser with sliding cover and adaptive nozzle for aircraft engine nacelle |
| 05/08/2013 | CN101772635B Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise, and turbojet and motor assembly associated therewith |
| 05/07/2013 | US8434715 Nested fairing thrust reverser |
| 05/07/2013 | US8434309 Translating core cowl having aerodynamic flap sections |
| 05/07/2013 | US8434293 High stiffness shape memory alloy actuated aerostructure |
| 05/02/2013 | WO2013063362A1 Telescoping fluid porting tube |
| 05/02/2013 | WO2013062664A2 Nozzle arrangement and method of making the same |
| 05/02/2013 | WO2013060956A1 Device for attaching a hollow part |
| 05/02/2013 | CA2852996A1 A device for fastening a hollow part |
| 05/02/2013 | CA2851228A1 Nozzle arrangement and method of making the same |
| 05/01/2013 | EP2587038A1 Variable width gap seal |
| 05/01/2013 | EP2587037A2 Turbofan engine mixer assembly |
| 05/01/2013 | EP2587001A2 Blind retention mount |
| 05/01/2013 | CN101809273B Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator |
| 04/30/2013 | US8430203 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle |
| 04/30/2013 | CA2793462A1 Turbofan engine mixer assembly |
| 04/30/2013 | CA2793232A1 Component and method of fabricating the same |
| 04/30/2013 | CA2619292C Method for attenuating the noise of a turbofan |
| 04/25/2013 | US20130097998 Thrust reverser for an aircraft having semi-recessed turbofan engines |
| 04/25/2013 | US20130097997 Ram air fan diffuser |
| 04/24/2013 | EP2584184A2 Variable area nozzle for gas turbine engine |
| 04/24/2013 | CN202900416U Jet-flow high-efficiency thermal power system |
| 04/24/2013 | CN103069141A Beam for a cascade thrust reverser |