| 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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| 04/17/2008 | WO2008045072A1 Dual function cascade integrated variable area fan nozzle and thrust reverser |
| 04/17/2008 | WO2008045071A1 Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method |
| 04/17/2008 | WO2008045070A1 Variable area fan nozzle thrust reverser |
| 04/17/2008 | WO2008045069A1 Fan variable area nozzle with electromechanical actuator |
| 04/17/2008 | WO2008045067A1 Translating core cowl having aerodynamic flap sections |
| 04/17/2008 | WO2008045066A1 Controlling the aerodynamic drag of a gas turbine engine during a shutdown state |
| 04/17/2008 | WO2008045065A1 Controlling ice buildup on aircraft engine and nacelle static and rotating components |
| 04/17/2008 | WO2008045064A1 Turbofan engine sound control system and method |
| 04/17/2008 | WO2008045063A1 Variable area nozzle assisted gas turbine engine restarting |
| 04/17/2008 | WO2008045062A1 Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system |
| 04/17/2008 | WO2008045061A1 Translating core cowl for a gas turbine engine |
| 04/17/2008 | WO2008045058A1 Operational line management of low pressure compressor in a turbofan engine |
| 04/17/2008 | WO2008045057A1 Bladder type variable area fan nozzle |
| 04/17/2008 | WO2008045056A1 Tri-body variable area fan nozzle and thrust reverser |
| 04/17/2008 | WO2008045055A1 Turbofan engine having inner fixed structure including ducted passages |
| 04/17/2008 | WO2008045054A1 Modulating flow through gas turbine engine cooling system |
| 04/17/2008 | WO2008045052A1 Method and device to avoid turbofan instability in a gas turbine engine |
| 04/17/2008 | WO2008045050A1 Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle |
| 04/17/2008 | WO2008045049A1 Gas turbine engine with axial movable fan variable area nozzle |
| 04/17/2008 | WO2008045048A1 Integrated variable area nozzle and thrust reversing mechanism |
| 04/17/2008 | WO2008045035A1 Corrugated core cowl for a gas turbine engine |
| 04/17/2008 | WO2008045034A1 Fan variable area nozzle with cable actuator system |
| 04/17/2008 | WO2008043890A1 Cascade-type thrust reverser for jet engine |
| 04/17/2008 | CA2663231A1 Cascade-type thrust reverser for jet engine |
| 04/16/2008 | CN101162005A Nuclear reactor and flying saucer manufactured thereby |
| 04/10/2008 | US20080083210 Monolithic thrust reverser components |
| 04/10/2008 | CA2664244A1 Aircraft engine nacelle and aircraft equipped with such a nacelle |
| 04/09/2008 | EP1908950A2 Pressure balance control for gas turbine engine nozzle |
| 04/09/2008 | EP1908949A1 Rocket engine |
| 04/09/2008 | CN100379945C Method and device for support high temperature pipeline |
| 04/08/2008 | CA2321357C Turbojet thrust reverser with centre-pivot doors |
| 04/02/2008 | EP1905998A2 Asymmetric Serrated Nozzle For Exhaust Noise Reduction |
| 04/02/2008 | EP1905997A1 Rocket enginge |
| 04/02/2008 | EP1905689A1 Integrated propulsion system comprising a turbofan engine |
| 04/01/2008 | CA2284363C Thermal barrier coating systems and materials |
| 03/28/2008 | CA2601288A1 Turbine exhaust case cowling for a gas turbine engine |
| 03/27/2008 | WO2008034214A1 Thrust reverser nozzle for a turbofan gas turbine engine |
| 03/27/2008 | US20080072604 Pressure balance control for gas turbine engine nozzle |
| 03/27/2008 | US20080072571 Aeroengine thrust reverser |
| 03/26/2008 | EP1903205A2 Thrust reverser nozzle for a turbofan gas turbine engine |
| 03/26/2008 | EP1902948A1 Gas turbine helicopter engine with reduced sound emissions due to acoustic treatment of a jet pump |
| 03/26/2008 | CN101149296A Broad-band noise-reducing acoustic liner and its manufacture method |
| 03/26/2008 | CN101149025A Gas turbine helicopter engine with noise emission reduced through acoustical treatment of an eductor |
| 03/19/2008 | EP1900924A2 Bleed valve outlet flow deflector |
| 03/19/2008 | EP1900909A2 Variable area nozzle in a gas turbine engine |
| 03/19/2008 | CN101144440A Nuclear reactor and flying saucer prepared from the same |
| 03/18/2008 | CA2292821C Acoustically adjusted multi-channel turbine engine exhaust device |
| 03/13/2008 | US20080060344 Exhaust duct and tail cone attachment of aircraft engines |
| 03/13/2008 | US20080060343 Asymmetric serrated nozzle for exhaust noise reduction |
| 03/13/2008 | US20080060342 Flow reverser |
| 03/12/2008 | EP1896717A1 Aircraft pod and aircraft equipped with at least one such pod |
| 03/12/2008 | EP1896716A2 Jet nozzle mixer |
| 03/11/2008 | US7341225 Aircraft wing and aeroengine arrangement for attenuating engine noise |
| 03/11/2008 | US7340883 Morphing structure |
| 03/11/2008 | CA2600818A1 Exhaust duct and tail cone attachment of aircraft engines |
| 03/05/2008 | EP1895140A2 Fan exhaust nozzle for turbofan engine |
| 03/05/2008 | EP1893863A2 Turbofan core thrust spoiler |
| 03/05/2008 | EP1633935A4 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 03/05/2008 | EP1340736B1 Porous sound absorbing material and method of manufacturing the material |
| 03/05/2008 | CA2599095A1 Turbine exhaust strut airfoil and gas path profile |
| 03/04/2008 | US7337875 High admittance acoustic liner |
| 02/29/2008 | CA2598304A1 Fan exhaust nozzle for turbofan engine |
| 02/28/2008 | WO2008023168A1 Aircraft engine thrust reverser |
| 02/28/2008 | WO2008003889A3 Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with said device |
| 02/28/2008 | US20080047273 Turbomachine nozzle cover provided with triangular patterns having pairs of vertices for reducing jet noise |
| 02/28/2008 | CA2661540A1 Aircraft engine thrust reverser |
| 02/27/2008 | EP1892405A2 Gas turbine engine exhaust duct ventilation |
| 02/27/2008 | EP1891318A1 Control system for the nacelle of a turboreactor |
| 02/27/2008 | CN100371580C Long service life jet deflection plate for turbine jet motor of aircraft |
| 02/26/2008 | US7334395 Aircraft structure that includes a duct for guiding fluid flow therethrough |
| 02/26/2008 | US7334394 Localized arc filament plasma actuators for noise mitigation and mixing enhancement |
| 02/26/2008 | US7334393 Aircraft engine in which there is a small clearance separating the fan cowls and the thrust inverter cowls |
| 02/21/2008 | WO2008019493A1 Gas turbine engine exhaust duct ventilation |
| 02/21/2008 | US20080041062 Turbomachine nozzle cover provided with triangular patterns having a point of inflexion for reducing jet noise |
| 02/21/2008 | US20080041061 Multiple vane variable geometry nozzle |
| 02/13/2008 | EP1887209A2 Hanger system for a cooling liner within a gas turbine engine exhaust duct |
| 02/13/2008 | EP1887208A2 Attachment hanger system for a cooling liner within a gas turbine engine exhaust duct |
| 02/13/2008 | EP1171705B1 Rocket engine |
| 02/12/2008 | US7328771 Zero acoustic splice fan case liner |
| 02/09/2008 | CA2839333A1 Jet engine nozzle exit configurations and associated systems and methods |
| 02/09/2008 | CA2813533A1 Jet engine nozzle exit configurations and associated systems and methods |
| 02/09/2008 | CA2756214A1 Jet engine nozzle exit configurations and associated systems and methods |
| 02/07/2008 | US20080028763 Thermal management system with thrust recovery for a gas turbine engine fan nacelle assembly |
| 02/06/2008 | EP1884650A1 Gas exhaust nozzle for a bypass flow turbomachine |
| 02/06/2008 | EP1884649A1 By-pass engine with variation of its throat section by means of air injection |
| 02/06/2008 | EP1766218B1 Aircraft jet engine provided with a device for reducing propulsion jet noise |
| 02/06/2008 | CN101117927A Nuclear reactor and flying saucer made by it |
| 01/31/2008 | US20080022690 Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl |
| 01/31/2008 | US20080022689 Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct |
| 01/31/2008 | US20080022651 Jet engine noise suppressor |
| 01/31/2008 | DE10242393B4 Abschirmung für die aus einem Flugzeug-Strahltriebwerk emittierten Abgasschwaden Shielding of light emitted from an aircraft jet engine exhaust fumes |
| 01/30/2008 | EP1882822A2 Cooled exhaust liner assembly for a gas turbine |
| 01/30/2008 | EP1882096A1 Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved |
| 01/26/2008 | CA2594753A1 Dual flow turbine engine exhaust nozzle having a variable exhaust or collar section by displacement of the secondary cowling |
| 01/24/2008 | US20080017442 System for joining acoustic cellular panel sections in edge-to-edge relation |
| 01/24/2008 | US20080016873 Outlet Device for a Jet Engine and a Jet Engine Comprising Such an Outlet Device |
| 01/24/2008 | US20080016872 Vectorable nozzle with pivotable triangular panels |
| 01/23/2008 | EP1880941A2 System for joining acoustic cellular panel sections in edge-to-edge relation |
| 01/17/2008 | US20080010969 Gas turbine engine and method of operating same |
| 01/16/2008 | EP1878904A2 Thrust reverser assembly for a gas turbine engine and method of operating same |