| 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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| 10/27/2011 | WO2011131874A1 Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle |
| 10/27/2011 | WO2011131873A1 Nacelle for an aircraft engine with variable cross-section nozzle |
| 10/27/2011 | WO2011131872A1 Hydraulic control system for a thrust reversal device |
| 10/27/2011 | WO2011131651A1 Exhaust gas diffuser of a gas turbine |
| 10/27/2011 | CA2795691A1 Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle |
| 10/27/2011 | CA2792968A1 Nacelle for an aircraft engine with variable cross-section nozzle |
| 10/27/2011 | CA2792521A1 Hydraulic control system for a thrust reversal device |
| 10/26/2011 | EP2381071A1 Exhaust gas diffusor of a gas turbine |
| 10/26/2011 | EP2116714B1 Low noise aircraft |
| 10/25/2011 | US8043690 Exhaust washed structure and associated composite structure and method of fabrication |
| 10/20/2011 | WO2011128560A1 System for controlling an electrical device of a nacelle |
| 10/20/2011 | DE102010014910A1 Mixing device for turbofan engine for mixing cold air stream with hot-air stream, has engine pod and exhaust cone that defines cold air stream with hot-air stream |
| 10/20/2011 | DE102010014909A1 Variable mixer i.e. variable bloom mixer, for mixing cool and hot air streams of fan of turbofan engine of aircraft, has traction cable for obtaining original position by compensating traction force using resilient material properties |
| 10/20/2011 | CA2794249A1 System for controlling an electrical device of a nacelle |
| 10/19/2011 | EP2205847B1 A device and method for controlling vortex structures in a turbulent air jet |
| 10/13/2011 | WO2011125248A1 Jet flow nozzle and jet engine |
| 10/13/2011 | WO2011124793A1 Aircraft propulsion system provided with reverse thrust means |
| 10/13/2011 | CA2795710A1 Jet flow nozzle and jet engine |
| 10/13/2011 | CA2792288A1 Aircraft propulsion system provided with reverse thrust means |
| 10/12/2011 | EP2375045A1 Afterbody assembly provided with flexible links with abutments |
| 10/12/2011 | CN102216597A Thrust reverser for a turbofan engine nacelle |
| 10/11/2011 | US8033111 Damping of vibration of a combustion chamber by resonators |
| 10/05/2011 | EP2372697A1 Method of retrofitting an acoustic treatment into a fluid handling module |
| 10/04/2011 | US8028797 System for joining acoustic cellular panel sections in edge-to-edge relation |
| 09/29/2011 | WO2011117555A1 Reverse thrust device |
| 09/29/2011 | US20110233305 Structure for thrust inverter |
| 09/29/2011 | US20110232991 Method for bonding honeycomb cores |
| 09/29/2011 | US20110232291 System and method for an exhaust diffuser |
| 09/29/2011 | US20110232262 Radial and axial compliant sliding seal incorporating spring capturing features for improved bearing plane sealing in an articulating nozzle |
| 09/29/2011 | CA2792973A1 Reverse thrust device |
| 09/28/2011 | EP2369163A2 Nozzle with adjustable throat |
| 09/28/2011 | EP2368032A1 Thrust reverser for a turbofan engine nacelle |
| 09/27/2011 | US8025122 Acoustically treated exhaust centerbody for jet engines and associated methods |
| 09/21/2011 | CN101523041B Jet engine nacelle for an aircraft and aircraft comprising such a nacelle |
| 09/20/2011 | US8020386 Rollertrack pivoting axi-nozzle |
| 09/20/2011 | US8020368 Aircraft jet engine provided with a device for reducing propulsion jet noise |
| 09/20/2011 | US8020367 Nozzle with yaw vectoring vane |
| 09/15/2011 | US20110220433 Combustor and gas turbine having the same |
| 09/14/2011 | EP2364401A1 Radially translating fan nozzle nacelle |
| 09/13/2011 | US8015820 Gas turbine engine exhaust component and manufacturing method of same |
| 09/13/2011 | US8015819 Wet active chevron nozzle for controllable jet noise reduction |
| 09/13/2011 | US8015797 Thrust reverser nozzle for a turbofan gas turbine engine |
| 09/09/2011 | WO2011107320A1 Flow mixer and corresponding gas turbine engine |
| 09/08/2011 | US20110215204 System and method for generating thrust |
| 09/08/2011 | US20110215193 Hybrid torque box for a thrust reverser |
| 09/07/2011 | EP1931870B1 An arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine |
| 09/06/2011 | CA2485322C Soundproofing panels with beads and process for producing the said panels |
| 08/31/2011 | EP2361350A1 Magnetic advanced generation jet electric turbine |
| 08/31/2011 | EP2142779B1 Acoustic panel having a variable acoustic characteristic |
| 08/31/2011 | CN101426681B Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 08/25/2011 | WO2011101581A1 Circuit for detecting the positions of contactors in a turbine engine |
| 08/25/2011 | US20110204161 Door with movable spoiler for door-type thrust reverser |
| 08/25/2011 | US20110203288 Jet Engine Exhaust Nozzle Flow Effector |
| 08/25/2011 | US20110203255 Flexible abutment links for attaching a part made of cmc |
| 08/25/2011 | US20110203254 Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise |
| 08/25/2011 | CA2786543A1 Circuit for detecting the positions of contactors in a turbine engine |
| 08/24/2011 | EP2360367A2 Actuator control system for an aircraft thrust reverser |
| 08/24/2011 | CN201943841U 一种涡喷消防车多级、复合降噪装置 A scroll jet engines multi-level, complex noise reduction device |
| 08/23/2011 | US8002217 System for adjustment of thrust reverser pivot door |
| 08/23/2011 | CA2495624C Turbojet having a large bypass ratio |
| 08/18/2011 | WO2011098737A1 Gas-guiding pipe comprising a noise-attenuating covering with variable porosity |
| 08/18/2011 | WO2011098729A1 Device for ejecting gas from a gas turbine engine and gas turbine engine |
| 08/18/2011 | WO2011098711A1 Aircraft control system |
| 08/18/2011 | DE102009031061A1 Jet drive i.e. gas turbine, for airplane, has thrust nozzle with two parts, where one of parts has cylindrical outer part and inner part tapering in flow direction of turbine shaft, and another part has outer part tapering in flow direction |
| 08/18/2011 | CA2789555A1 Gas-guiding pipe comprising a noise-attenuating covering with variable porosity |
| 08/18/2011 | CA2789258A1 Device for ejecting gas from a gas turbine engine and gas turbine engine |
| 08/18/2011 | CA2785918A1 Aircraft control system |
| 08/11/2011 | WO2011095747A1 Secondary-air nozzle of a two-flow jet engine having separated flows including a grid thrust reverser |
| 08/11/2011 | US20110192167 Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron |
| 08/11/2011 | US20110192135 Control System |
| 08/11/2011 | DE102010007665A1 Exhaust nozzle for jet engine, has centrally arranged sliding cone to change nozzle cross-section, where extension tube is provided to guide sliding cone |
| 08/11/2011 | CA2788903A1 Secondary-air nozzle of a two-flow jet engine having separated flows including a grid thrust reverser |
| 08/10/2011 | EP2354516A2 Translatable cascade thrust reverser |
| 08/10/2011 | EP2354493A2 Ejector/mixer nozzle for noise reduction |
| 08/09/2011 | CA2478202C Methods and apparatus to reduce turbine engine nozzle basesheet stresses |
| 08/03/2011 | EP2350445A2 Method and system for altering engine air intake geometry |
| 08/03/2011 | CN201916074U 喷气轮发动机 Jet turbine engine |
| 08/03/2011 | CN102144084A Flexible abutment links for attaching a part made of CMC |
| 08/02/2011 | US7988087 VTOL aircraft nozzle |
| 07/28/2011 | US20110180620 Elimination of unfavorable outflow margin |
| 07/28/2011 | US20110179768 Rocket thruster assembly comprising load-balanced pintle valve |
| 07/26/2011 | US7984787 Fluid-carrying conduit and method with noise attenuation |
| 07/21/2011 | WO2011085835A2 Laval nozzle |
| 07/21/2011 | WO2011016973A3 High stiffness shape memory alloy actuated aerostructure |
| 07/21/2011 | US20110174899 Nacelle with a variable nozzle section |
| 07/21/2011 | US20110173949 Jet engine nacelle having dampers for half-shells |
| 07/21/2011 | DE102010001059A1 Zwischengehäuse für ein Gasturbinentriebwerk Between the housing for a gas turbine engine |
| 07/20/2011 | CN102131705A Nacelle with a variable nozzle section |
| 07/19/2011 | US7980508 Jet propulsion efflux outlets |
| 07/19/2011 | US7980058 Air compression type engine for aviation |
| 07/14/2011 | WO2011083256A1 Thrust reverser for an aircraft having semi-recessed turbofan engines |
| 07/14/2011 | US20110168833 Aircraft having a rotating turbine engine |
| 07/14/2011 | US20110168809 Thrust vector system |
| 07/14/2011 | US20110167788 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 07/14/2011 | US20110167786 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines |
| 07/14/2011 | US20110167785 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines |
| 07/13/2011 | CN102121402A Steam engine |
| 07/12/2011 | US7975488 Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct |
| 07/12/2011 | US7975466 Exhaust nozzle for thrust vectoring |
| 07/12/2011 | CA2469847C Noise-reducing turbomachine nozzle |