| 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) |
|---|
| 07/16/2009 | WO2009087282A2 Door-type thrust reverser for a jet engine |
| 07/16/2009 | US20090178416 Bifurcation and aft vent used to vary fan nozzle exit area |
| 07/16/2009 | US20090178415 Extendible exhaust nozzle bell for a rocket engine |
| 07/16/2009 | CA2705361A1 Door-type thrust reverser for a jet engine |
| 07/15/2009 | EP2078152A1 Cascade-type thrust reverser for jet engine |
| 07/15/2009 | EP1797310B1 Mixer for separate-flow nozzle |
| 07/14/2009 | US7559507 Thrust reversers including locking assemblies for inhibiting deflection |
| 07/09/2009 | US20090173077 Nozzle with Temperature-Responsive Throat Diameter |
| 07/09/2009 | DE102007036527B4 Düsenanordnung für ein Gasturbinentriebwerk Nozzle arrangement for a gas turbine engine |
| 07/09/2009 | CA2690287A1 Device for mechanically decoupled fastening of an aircraft component perfused by hot gas |
| 07/08/2009 | CN101479461A Guiding carrier for jet engine linings |
| 07/08/2009 | CN100510369C Methods and apparatus for operating gas turbine engines |
| 07/07/2009 | US7555904 Thermally compliant rivet connection for connecting turbine engine liner to convergent flap and seal for turbine nozzle |
| 07/07/2009 | US7555894 Swivelling exhaust nozzle for an aircraft engine |
| 07/07/2009 | US7555893 Aircraft propulsion system |
| 07/07/2009 | CA2372631C Mobile cowling actuating system of a thrust reverser in a turbojet |
| 07/02/2009 | WO2009060133A3 Dual action telescopic linear actuator |
| 07/01/2009 | EP2074323A1 Turbofan engine with variable bypass nozzle exit area and method of operation |
| 07/01/2009 | EP2074320A1 Variable area fan nozzle thrust reverser |
| 07/01/2009 | EP2074319A1 Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method |
| 07/01/2009 | EP2074318A1 Bifurcation and aft vent used to vary fan nozzle exit area |
| 07/01/2009 | EP2074317A1 Gas turbine engine bifurcation located in a fan variable area nozzle |
| 07/01/2009 | EP2074316A2 Managing low pressure turbine maximum speed in a turbofan engine |
| 07/01/2009 | EP2074314A1 Turbofan engine operation control |
| 07/01/2009 | EP2074313A1 Fan variable area nozzle with electromechanical actuator |
| 07/01/2009 | EP2074312A1 Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system |
| 07/01/2009 | EP2074311A1 Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle |
| 07/01/2009 | EP2074310A1 Controlling the aerodynamic drag of a gas turbine engine during a shutdown state |
| 07/01/2009 | EP2074309A1 Fan variable area nozzle with cable actuator system |
| 07/01/2009 | EP2074308A1 Integrated variable area nozzle and thrust reversing mechanism |
| 07/01/2009 | EP2074307A1 Translating core cowl having aerodynamic flap sections |
| 07/01/2009 | EP2074306A1 Dual function cascade integrated variable area fan nozzle and thrust reverser |
| 07/01/2009 | EP2074305A1 Translating core cowl for a gas turbine engine |
| 07/01/2009 | EP2074304A1 Tri-body variable area fan nozzle and thrust reverser |
| 07/01/2009 | EP2074303A1 Core cowl airfoil for a gas turbine engine |
| 07/01/2009 | EP2074302A1 Corrugated core cowl for a gas turbine engine |
| 07/01/2009 | EP2074301A1 Reduced take-off field length using variable nozzle |
| 07/01/2009 | EP2074298A1 Variable area nozzle assisted gas turbine engine restarting |
| 07/01/2009 | CN101473130A Thrust reverser forming an adaptive nozzle |
| 07/01/2009 | CN100507252C Fluidic chevrons and configurable thermal shield for jet noise reduction |
| 06/30/2009 | CA2535327C Thrust reverser lock comprising locking device |
| 06/25/2009 | WO2009004143A3 Dual flow turboshaft engine and improved hot flow nozzle |
| 06/25/2009 | US20090162213 Pumping Ejector |
| 06/25/2009 | US20090158704 Gas Turbine Engine |
| 06/25/2009 | US20090158703 Sliding ramp nozzle system for a gas turbine engine |
| 06/25/2009 | DE102007063018A1 Düse mit Leitelementen Nozzle with baffles |
| 06/24/2009 | EP2072793A2 Nozzle with guiding elements |
| 06/24/2009 | EP2071930A2 Actuation of a turbofan engine bifurcation to change an effective nozzle exit area |
| 06/24/2009 | CN101466940A Engine exhaust system |
| 06/21/2009 | CA2647052A1 Nozzle with guiding elements |
| 06/18/2009 | US20090151320 Partial cascade thrust reverser |
| 06/17/2009 | EP2069632A1 Turbofan engine sound control system and method |
| 06/17/2009 | EP2069631A1 Fan variable area nozzle positional measurement system |
| 06/17/2009 | EP2069630A1 Gas turbine engine with axial movable fan variable area nozzle |
| 06/17/2009 | EP2069629A1 Gas turbine engine fan variable area nozzle with swivalable insert system |
| 06/16/2009 | US7546738 Turbine engine nozzle |
| 06/16/2009 | US7546727 Reduced noise jet engine |
| 06/11/2009 | US20090145134 Rocket engine nozzle system |
| 06/11/2009 | US20090145133 Exhaust liner attachment arrangement |
| 06/11/2009 | US20090145107 Propulsion system |
| 06/10/2009 | EP2067974A1 Laminate air seal for a gas turbine engine |
| 06/10/2009 | EP2066895A2 Jet engine nacelle for an aircraft and aircraft comprising such a nacelle |
| 06/10/2009 | EP2066890A1 Modulating flow through gas turbine engine cooling system |
| 06/10/2009 | EP2066872A1 Method and device to avoid turbofan instability in a gas turbine engine |
| 06/10/2009 | CN100497923C Methods and apparatus to reduce turbine engine nozzle base sheet stresses |
| 06/09/2009 | US7543452 Serrated nozzle trailing edge for exhaust noise suppression |
| 06/09/2009 | US7543451 Aircraft engine exhaust shroud |
| 06/03/2009 | EP2064434A1 Operational line management of low pressure compressor in a turbofan engine |
| 06/03/2009 | EP2064433A1 Bladder type variable area fan nozzle |
| 06/03/2009 | EP2064432A2 Pintle-controlled propulsion system with external dynamic seal |
| 06/03/2009 | CN101446244A Single-valve core and double-channel solenoid valve |
| 06/02/2009 | CA2379193C Synchronized locking system for thrust-reverser doors |
| 05/28/2009 | WO2009066037A1 Grid-type thrust reverser |
| 05/28/2009 | US20090133406 Fan nozzle of adjustable section |
| 05/28/2009 | CA2702010A1 Grid-type thrust reverser |
| 05/27/2009 | EP2063095A2 Fan nozzle with adjustable cross-section |
| 05/27/2009 | EP2061964A1 Turbofan engine having inner fixed structure including ducted passages |
| 05/27/2009 | CN101443543A Turbojet nacelle equipped with means for reducing the noise produced by said turbojet |
| 05/23/2009 | CA2645240A1 Adjustable section turbofan exhaust nozzle |
| 05/21/2009 | US20090127391 Pivoting Fairings for a Thrust Reverser |
| 05/21/2009 | US20090127390 Thrust Reverser for a Turbofan Gas Turbine Engine |
| 05/21/2009 | US20090126342 Thrust Reverser Door |
| 05/21/2009 | US20090126341 Thrust Reverser |
| 05/21/2009 | US20090126340 Pivoting Door Thrust Reverser for a Turbofan Gas Turbine Engine |
| 05/20/2009 | EP2060770A2 Thrust reverser door |
| 05/20/2009 | EP2060769A2 Thrust reverser |
| 05/20/2009 | EP2060768A2 Thrust reverser for a turbofan gas turbine engine |
| 05/20/2009 | EP2060767A2 Pivoting door thrust reverser for a turbofan gas turbine engine |
| 05/20/2009 | EP2060766A2 Thrust reverser and method of redirecting jet engine thrust |
| 05/20/2009 | EP2060765A2 Pivoting fairings for a thrust reverser |
| 05/20/2009 | CN101438048A Nacell for bypass engine with high bypass ratio |
| 05/20/2009 | CN100489289C Jet engine cabin air bleed cavity sealing device |
| 05/20/2009 | CN100489288C Device for using seal member for releasing air of cabin and sealing cavity |
| 05/19/2009 | US7533760 Noise reduction tubes |
| 05/19/2009 | US7533533 Jet engine with a variable section nozzle of which at least one flap pivots about a pin, pins for flaps |
| 05/19/2009 | US7533517 Exhaust nozzle for an engine of a flying craft |
| 05/16/2009 | CA2639079A1 Thrust reverser |
| 05/16/2009 | CA2639078A1 Pivoting fairings for a thrust reverser |
| 05/16/2009 | CA2638860A1 Thrust reverser door |
| 05/16/2009 | CA2638842A1 Pivoting door thrust reverser for a turbofan gas turbine engine |