| 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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| 04/01/2010 | WO2006049552A9 Outlet device for a jet engine and a craft comprising such an outlet device |
| 04/01/2010 | CA2734417A1 Nacelle with a variable nozzle section |
| 03/31/2010 | EP2169204A1 Actuator |
| 03/30/2010 | US7685825 Axially split nozzle liner for convergent nozzle |
| 03/30/2010 | CA2293076C Fan and compressor noise attenuation |
| 03/25/2010 | WO2010012874A3 Thrust reverser device |
| 03/24/2010 | CN101680395A Multiple-acting linear actuator |
| 03/24/2010 | CN101678897A Propulsion assembly for aircraft with sliding nacelle |
| 03/23/2010 | US7681400 Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft |
| 03/23/2010 | US7681399 Turbofan engine cowl assembly and method of operating the same |
| 03/23/2010 | CA2313260C Acoustic liner and method of making an acoustic liner |
| 03/18/2010 | US20100064659 Translating variable area fan nozzle with split beavertail fairings |
| 03/17/2010 | EP2163754A1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 03/17/2010 | CN101675239A Door with movable spoiler for door-type thrust reverser |
| 03/17/2010 | CN101675238A Exhaust system for gas turbine |
| 03/17/2010 | CN101675226A Acoustic panel having a variable acoustic characteristic |
| 03/16/2010 | US7677026 Mixer for separate-flow nozzle |
| 03/11/2010 | WO2010026354A2 Flexible abutment links for attaching a part made of cmc |
| 03/11/2010 | US20100058769 Fan variable area nozzle for a gas turbine engine fan nacelle with drive ring actuation system |
| 03/11/2010 | US20100058735 Operational line management of low pressure compressor in a turbofan engine |
| 03/11/2010 | DE102008045851A1 Vorrichtung zum Öffnen und Schließen einer Schubumkehrertür eines Strahltriebwerks A device for opening and closing a Schubumkehrertür a jet engine |
| 03/11/2010 | CA2733572A1 Flexible abutment links for attaching a part made of cmc |
| 03/10/2010 | EP2161437A2 Device for opening and closing a thrust reverser door of a turbojet engine |
| 03/09/2010 | US7673458 Turbofan engine nozzle assembly and method for operating the same |
| 03/09/2010 | US7673442 Turbofan engine cowl assembly |
| 03/04/2010 | US20100050651 Variable Slope Exhaust Nozzle |
| 03/04/2010 | US20100050596 Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle |
| 03/04/2010 | US20100050595 Gas turbine engine with axial movable fan variable area nozzle |
| 03/03/2010 | EP2159403A2 Variable slope exhaust nozzle |
| 03/02/2010 | US7669404 Localized arc filament plasma actuators for noise mitigation and mixing enhancement |
| 02/27/2010 | CA2675907A1 Variable slope exhaust nozzle |
| 02/25/2010 | US20100044504 Rear propulsion system with lateral air inlets for an aircraft with such system |
| 02/25/2010 | US20100044466 Grid thrust reverser cover comprising a seal support and associated seal |
| 02/24/2010 | EP2157305A2 Gas turbine engine with variable area fan nozzle |
| 02/24/2010 | EP2156042A1 Multiple-acting linear actuator |
| 02/24/2010 | EP1999022B1 Air inlet shroud structure |
| 02/24/2010 | EP1846294B1 Procedure for replacement of acoustic liner in integrated exhaust duct muffler for use with airborne auxiliary power units |
| 02/24/2010 | CN101657629A Nacelle for turbojet jet fitted with a single door thrust reverser system |
| 02/24/2010 | CN101657628A Grid thrust reverser cover comprising a seal support and associated seal |
| 02/23/2010 | US7665294 Exhaust nozzle assembly |
| 02/23/2010 | CA2365100C Method for making a sound reducing panel with resistive layer having structural property and resulting panel |
| 02/18/2010 | WO2010019131A1 Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods |
| 02/18/2010 | WO2009056713A3 Double-acting telescopic linear actuator with single-motor drive system |
| 02/18/2010 | US20100037623 High Efficiency Turbine Engine |
| 02/17/2010 | EP2153051A1 A masking arrangement for a gas turbine engine |
| 02/17/2010 | EP2153050A1 Door with movable spoiler for door-type thrust reverser |
| 02/17/2010 | EP2153049A1 A system for mixing gas flows in a gas turbine engine, gas turbine engine and an aircraft engine |
| 02/17/2010 | EP2152937A1 Coating |
| 02/17/2010 | EP2152582A1 Propulsion assembly for aircraft with sliding nacelle |
| 02/17/2010 | CN101652556A Thrust reverser for a jet engine |
| 02/16/2010 | US7661510 Method for the manufacture of a light-weight sheet |
| 02/11/2010 | WO2010015751A1 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle |
| 02/11/2010 | US20100032497 Nozzle with guiding elements |
| 02/11/2010 | US20100031631 Gas turbine comprising a guide ring and a mixer |
| 02/11/2010 | US20100031628 Jet flow discharge nozzle and jet engine |
| 02/11/2010 | CA2732127A1 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle |
| 02/10/2010 | EP1937954B1 Turbojet engine with attenuated jet noise |
| 02/10/2010 | CN101646857A Aircraft nacelle incorporating a thrust-reversing device |
| 02/09/2010 | US7658063 Gas turbine having a single shaft bypass configuration |
| 02/04/2010 | WO2010013499A1 Method of preventing jet noise and jet nozzle |
| 02/04/2010 | WO2010012900A2 Acoustic attenuation panel for aircraft engine nacelle |
| 02/04/2010 | WO2010012899A2 Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
| 02/04/2010 | WO2010012878A1 Thrust reverser device |
| 02/04/2010 | WO2010012874A2 Thrust reverser device |
| 02/04/2010 | US20100025493 Actuator arrangement |
| 02/04/2010 | US20100024428 Rocket Apparatus and/or Method |
| 02/04/2010 | CA2732351A1 Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
| 02/04/2010 | CA2731974A1 Acoustic attenuation panel for aircraft engine nacelle |
| 02/02/2010 | US7654363 Turboshaft engine that reduces rear noise emissions |
| 01/28/2010 | WO2010011381A1 Duplex tab exhaust nozzle |
| 01/28/2010 | US20100018213 Gas turbine engine with rotationally overlapped fan variable area nozzle |
| 01/28/2010 | US20100018212 Dilating fan duct nozzle |
| 01/28/2010 | CA2728527A1 Duplex tab exhaust nozzle |
| 01/27/2010 | EP2148139A2 Flow sleeve impingement cooling using a plenum ring |
| 01/27/2010 | EP2148055A1 Exhaust gas system |
| 01/27/2010 | CN101634257A Secondary-duct combination spray pipe of engine |
| 01/27/2010 | CN100585157C Aircraft pod and aircraft equipped with at least one such pod |
| 01/26/2010 | CA2466222C Streamlined body and combustion apparatus having such a streamlined body |
| 01/26/2010 | CA2452972C Methods and apparatus for generating gas turbine engine thrust |
| 01/21/2010 | US20100012423 Acoustic treatment device for turbine and combustion noises |
| 01/21/2010 | US20100011777 Morphing structure and method |
| 01/21/2010 | US20100011740 Turbofan engine operation control |
| 01/19/2010 | US7647776 Fluid flow control system |
| 01/14/2010 | WO2009122037A3 Device for reducing turboprop infrared emissions |
| 01/14/2010 | US20100006697 Low noise aircraft |
| 01/14/2010 | US20100006368 Localized Decisions and Actions Determined from Communal Network of Observations in Order to Achieve Global Solution |
| 01/14/2010 | US20100005807 Liquid propellant rocket engine with a propulsion chamber shutter |
| 01/14/2010 | US20100005806 Eductor system for a gas turbine engine |
| 01/14/2010 | US20100005780 Method of manufacturing a cmc flow mixer lobed structure for a gas turbine aeroengine |
| 01/14/2010 | US20100005777 Dual function cascade integrated variable area fan nozzle and thrust reverser |
| 01/13/2010 | EP2143927A1 Liquid-propellant rocket engine with propulsion chamber blanking plug |
| 01/13/2010 | EP2142787A2 Exhaust system for gas turbine |
| 01/13/2010 | EP2142779A2 Acoustic panel having a variable acoustic characteristic |
| 01/13/2010 | CN101627202A Self-calibration method for the electric jacks of a turbojet nacelle |
| 01/12/2010 | US7644575 Morphing structure |
| 01/07/2010 | WO2010001147A1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 01/07/2010 | WO2009138598A3 Method and device for implementing the thrust reversers of an aircraft |
| 01/07/2010 | WO2009136096A3 Bypass turbojet engine nacelle |
| 01/07/2010 | US20100003121 Variable area fan nozzle for accommodating a foreign object strike event |
| 01/07/2010 | US20100001123 Translatable thrust inverter for jet engine |