| 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) |
|---|
| 07/02/2008 | EP1755867B1 Method for production of elements such as thrust-reverser cascade vanes by moulding of a composite material |
| 07/02/2008 | CN101213361A Aircraft pod and aircraft equipped with at least one such pod |
| 07/01/2008 | US7392651 Turbomachine nozzle cover for reducing jet noise |
| 06/26/2008 | WO2008076688A2 Two-piece aft closure for a rocket motor case |
| 06/26/2008 | WO2008075671A1 Jet flow discharge nozzle and jet engine |
| 06/26/2008 | US20080149742 System, method, and apparatus for control input prediction and state verification of fluidic vectoring exhaust in high performance aircraft |
| 06/25/2008 | EP1936173A2 Engine propulsion system having first and second exhaust ducts |
| 06/25/2008 | EP1936172A2 Systems and methods for passively directing aircraft engine nozzle flows |
| 06/25/2008 | EP1934547A2 Exhaust assembly for mass ejection drive system |
| 06/25/2008 | EP1934456A1 Method for attenuating the noise of a turbofan |
| 06/24/2008 | US7389635 Twisted mixer with open center body |
| 06/19/2008 | US20080143058 Two-piece aft closure for a rocket motor case |
| 06/19/2008 | US20080141656 Bypass turbomachine with artificial variation of its throat section |
| 06/19/2008 | US20080141655 Duct burning mixed flow turbofan and method of operation |
| 06/18/2008 | EP1931870A1 An arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine |
| 06/18/2008 | CA2613777A1 Duct burning mixed flow turbofan and method of operation |
| 06/17/2008 | CA2416251C Cooling device for the common nozzle of a turbo-jet engine nacelle |
| 06/13/2008 | CA2605518A1 Engine propulsion system and methods of assembling the same |
| 06/12/2008 | WO2008040869A3 Jet engine nacelle for an aircraft and aircraft comprising such a nacelle |
| 06/12/2008 | US20080134664 Thrust reverser pin lock |
| 06/11/2008 | EP1930580A2 Aircraft engine |
| 06/11/2008 | EP1930579A2 Thermally decoupled mixer |
| 06/11/2008 | CN101198785A Control system for the nacelle of a turboreactor |
| 06/11/2008 | CN100394011C Steam booster device and method for jet engine |
| 06/10/2008 | US7384609 Pre-converter device for cleaning exhaust gas for an internal combustion engine |
| 06/10/2008 | CA2501766C Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle |
| 06/10/2008 | CA2442859C Tortuous path exhaust eductor system |
| 06/05/2008 | WO2008067000A2 Pintle-controlled propulsion system with external dynamic seal |
| 06/05/2008 | US20080127629 Air Compression Type Engine For Aviation |
| 06/05/2008 | DE102006056643A1 Air craft engine e.g. bypass jet engine, has multiple guiding units that are attached to one of ambient air facing walls of exhaust gas nozzle modules, and causing turbulence for noise reduction of engine in ambient air |
| 06/04/2008 | EP1927745A1 Vectorable nozzle with pivotable triangular panels |
| 05/30/2008 | CA2603636A1 Methods and system for recuperated cooling of integral turbine nozzle and shroud assemblies |
| 05/30/2008 | CA2603312A1 Method and system to facilitate cooling turbine engines |
| 05/30/2008 | CA2603174A1 Methods and system for cooling integral turbine nozzle and shroud assemblies |
| 05/30/2008 | CA2601612A1 Method and system to facilitate preferentially distributed recuperated film cooling of turbine shroud assembly |
| 05/29/2008 | WO2008063154A2 Fan variable area nozzle with adaptive structure |
| 05/29/2008 | WO2008063153A2 Managing low pressure turbine maximum speed in a turbofan engine |
| 05/29/2008 | WO2008063152A2 Turbofan engine |
| 05/29/2008 | WO2008061336A1 Turbofan gas turbine engine and nacelle arrangement |
| 05/29/2008 | US20080120979 Morphing structure |
| 05/29/2008 | US20080120978 Propulsion system |
| 05/29/2008 | CA2569179A1 Vectorable nozzle with pivotable triangular panels |
| 05/28/2008 | EP1924498A1 Dynamically self-locking catching device |
| 05/28/2008 | CN100390397C Air compression aeroengine |
| 05/28/2008 | CA2611629A1 Turbine exhaust strut airfoil profile |
| 05/27/2008 | US7377109 Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flows |
| 05/27/2008 | US7377108 Apparatus and method for reduction jet noise from single jets |
| 05/22/2008 | US20080115484 Mixer For Separate-Stream Nozzle |
| 05/22/2008 | US20080115477 Localized arc filament plasma actuators for noise mitigation and mixing enhancement |
| 05/22/2008 | CA2610676A1 Turbine exhaust strut airfoil profile |
| 05/21/2008 | EP1923310A2 Nacelle drag reduction device for a turbofan gas turbine engine |
| 05/20/2008 | CA2281172C Nacelle for grounded moving component turbofan |
| 05/14/2008 | EP1921291A2 Gas turbine engine providing simulated boundary layer thickness increase |
| 05/14/2008 | EP1352167B1 Method for manufacturing outlet nozzles for rocket engines |
| 05/14/2008 | CA2609294A1 Turbofan engine nozzle assembly and method for operating the same |
| 05/14/2008 | CA2609291A1 Turbofan engine cowl assembly and method of operating the same |
| 05/14/2008 | CA2609282A1 Turbofan engine cowl assembly and method of operating the same |
| 05/14/2008 | CA2609281A1 Turbofan engine cowl assembly and method of operating the same |
| 05/14/2008 | CA2609228A1 Turbofan engine nozzle assembly and method for operating the same |
| 05/13/2008 | US7370468 Turbojet electromechanical thrust reverser with servo-controlled door displacement |
| 05/08/2008 | WO2008054436A2 Damped coil pin for attachment hanger hinge |
| 05/08/2008 | WO2008053088A1 Jet engine nacelle member |
| 05/08/2008 | WO2008053087A1 Side-opening jet engine nacelle |
| 05/08/2008 | US20080105488 rotary motion mixer for a converging-stream nozzle of a turbomachine |
| 05/08/2008 | US20080105487 Curved lobe mixer for a converging-stream nozzle for a turbomachine |
| 05/08/2008 | US20080105074 Bi-directional locking ring assembly for aircraft thrust reverser manual drive unit |
| 05/08/2008 | US20080104941 Exhaust cone for channeling a stream of gas downstream from a turbine |
| 05/08/2008 | US20080104940 Device for Controlling a Gas Flow, a Jet Engine Comprising the Device and an Aircraft Comprising the Device |
| 05/08/2008 | CA2666747A1 Jet engine nacelle member |
| 05/08/2008 | CA2666614A1 Side-opening jet engine nacelle |
| 05/07/2008 | EP1918563A2 Exhaust liner suspension system |
| 05/07/2008 | EP1918562A2 Bi-directional locking ring assembly for aircraft thrust reverser manual drive unit |
| 05/07/2008 | EP1918561A2 Combustion nozzle fluidic injection assembly |
| 05/07/2008 | EP1918560A2 Combined control for supplying cooling air and support air in a turbine engine nozzle |
| 05/07/2008 | EP1485600A4 Duplex mixer exhaust nozzle |
| 05/07/2008 | CN101175913A Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved |
| 05/02/2008 | WO2008049986A1 Thrust reverser with grids for jet engine |
| 05/02/2008 | CA2666496A1 Thrust reverser with grids for jet engine |
| 05/01/2008 | US20080098742 Combined control for supplying cooling air and support air in a turbine engine nozzle |
| 05/01/2008 | US20080098720 Securing assembly |
| 04/30/2008 | EP1916405A2 Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle |
| 04/30/2008 | EP1352169B1 Rocket engine member and a method for manufacturing a rocket engine member |
| 04/30/2008 | DE102006051375A1 Aerodynamic covering for installations in engine mountings and supply lines, has compressed air stream blown into outer air stream in separation area with high energy and oscillates or pulsates depending on streaming behaviors |
| 04/29/2008 | US7364117 Passive cooling system for auxiliary power unit installation |
| 04/24/2008 | US20080093174 Tip Turbine Engine with a Heat Exchanger |
| 04/24/2008 | US20080092548 Gas turbine engine having slim-line nacelle |
| 04/24/2008 | US20080092514 Tip Turbine Engine Composite Tailcone |
| 04/24/2008 | US20080092362 Zero acoustic splice fan case liner |
| 04/23/2008 | EP1913237A1 Radially expanding turbine engine exhaust cylinder interface |
| 04/17/2008 | WO2008045094A1 Bifurcation and aft vent used to vary fan nozzle exit area |
| 04/17/2008 | WO2008045093A1 Gas turbine engine bifurcation located in a fan variable area nozzle |
| 04/17/2008 | WO2008045092A1 Fan variable area nozzle positional measurement system |
| 04/17/2008 | WO2008045091A1 Gas turbine engine fan variable area nozzle with swivalable insert system |
| 04/17/2008 | WO2008045090A1 Gas turbine engine with rotationally overlapped fan variable area nozzle |
| 04/17/2008 | WO2008045089A1 Core cowl airfoil for a gas turbine engine |
| 04/17/2008 | WO2008045082A1 Reduced take-off field length using variable nozzle |
| 04/17/2008 | WO2008045081A1 Variable fan nozzle using shape memory material |
| 04/17/2008 | WO2008045080A1 Variable area fan nozzle for accommodating a foreign object strike event |
| 04/17/2008 | WO2008045079A1 Turbofan engine operation control |
| 04/17/2008 | WO2008045074A1 Turbofan engine with variable bypass nozzle exit area and method of operation |