| 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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| 09/26/2013 | WO2013140055A1 Aircraft turbojet engine exhaust cone |
| 09/25/2013 | EP2640952A2 Nacelle for an aircraft turbofan engine |
| 09/25/2013 | EP2640946A1 Thermal integration of thermoelectric device |
| 09/25/2013 | EP2640639A1 Turbojet engine nacelle reinforcing structure |
| 09/25/2013 | CN203214191U Tail shaft rear shaft aluminum tube device |
| 09/25/2013 | CN203214190U Novel tail shaft front shaft aluminum tube |
| 09/25/2013 | CN203214189U Plug type axial symmetry spray pipe central cone circulation adjustable cooling structure |
| 09/25/2013 | CN203214188U Adjustable center body structure of two-dimensional plug nozzle |
| 09/25/2013 | CN103328801A Door for thrust reverser of an aircraft nacelle |
| 09/25/2013 | CN103328800A Nacelle for an aircraft bypass turbojet engine |
| 09/25/2013 | CN103321779A Supersonic non-uniform inflow maximum-thrust nozzle and wall determination method therefor |
| 09/24/2013 | CA2540259C Gas stream deflection system in a nozzle |
| 09/19/2013 | WO2013137951A2 Flexible leaf spring seal for sealing an air gap between moving plates |
| 09/19/2013 | WO2013135481A1 Fluid-pulsing device |
| 09/18/2013 | CN103314207A Aircraft turbojet engine thrust reverser with a reduced number of latches |
| 09/18/2013 | CN103314206A Nacelle for an aircraft bypass turbojet engine |
| 09/18/2013 | CN103306853A Sandwich structure with shear stiffness between skins and compliance in the thickness direction |
| 09/17/2013 | CA2761761C Aircraft engine nacelle comprising a mobile cowl moved by electric motors |
| 09/12/2013 | US20130232981 Jet noise reduction using eduction effect |
| 09/12/2013 | US20130232949 Pressure balanced area control of high aspect ratio nozzle |
| 09/12/2013 | US20130232948 Noise-Reducing Engine Nozzle System |
| 09/11/2013 | EP2636878A1 Noise-reducing engine nozzle system |
| 09/11/2013 | EP2635789A2 Aircraft turbojet engine thrust reverser with a lower number of actuators |
| 09/11/2013 | EP2635788A1 Thrust reverser device without a control rod in the stream |
| 09/11/2013 | CN103299035A Device for linking a front frame to a fan casing |
| 09/11/2013 | CN103291495A Supersonic/hypersonic aerocraft engine overexpansion nozzle bypass type device |
| 09/11/2013 | CN103291494A Exercise-decoupling axial-symmetry thrust vectoring nozzle adjusting mechanism with sliding pairs |
| 09/11/2013 | CN103291493A Exercise-decoupling axial-symmetry thrust vectoring nozzle adjusting mechanism |
| 09/11/2013 | CN101977814B Device for reducing turboprop infrared emissions |
| 09/10/2013 | US8528857 Translatable jet engine thrust reverser configuration providing improved maintenance access |
| 09/09/2013 | CA2805833A1 Jet noise reduction using eduction effect |
| 09/05/2013 | US20130228635 Turbojet engine nacelle |
| 09/05/2013 | US20130227952 Sandwich structure with shear stiffness between skins and compliance in the thickness direction |
| 09/05/2013 | CA2800433A1 Sandwich structure with shear stiffness between skins and compliance in the thickness direction |
| 09/04/2013 | CN203175702U Central cone cooling structure of plug type axially-symmetrical spay tube |
| 09/04/2013 | CN101922379B Translating variable area fan nozzle providing an upstream bypass flow exit |
| 09/04/2013 | CN101809272B Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron |
| 09/03/2013 | US8522528 System for diffusing bleed air flow |
| 08/29/2013 | US20130219858 Turbine engine with thrust vectoring exhaust nozzle |
| 08/28/2013 | EP2631450A1 Element for sound absorption in aircrafts nacelles |
| 08/28/2013 | EP2630357A1 Actuation system for a propulsive unit of an airplane |
| 08/28/2013 | CN203161375U Centripetal jet pipe |
| 08/28/2013 | CA2807676A1 Gas turbine exhaust having reduced jet noise |
| 08/27/2013 | US8516824 Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise |
| 08/27/2013 | US8516790 Spring for a cascade-type thrust reverser shutter for an aircraft jet engine |
| 08/22/2013 | US20130213006 Actuator assembly |
| 08/21/2013 | EP2628936A2 Aviation gas turbine thrust reversing device |
| 08/21/2013 | EP2628935A2 Actuator assembly |
| 08/21/2013 | EP2628934A2 Thermoelectric generator in turbine engine nozzles |
| 08/21/2013 | EP2627872A1 Device for connecting a thrust reverser front frame to a fan casing and nacelle incorporating such a device |
| 08/21/2013 | CN103261026A Inner structure for an aircraft nacelle |
| 08/21/2013 | CN103261025A Nacelle for a bypass turbojet engine |
| 08/21/2013 | CN103256147A Thermoelectric generator in turbine engine nozzles |
| 08/20/2013 | US8511090 Jet engine nozzle exit configurations and associated systems and methods |
| 08/20/2013 | US8511062 Actuation system for a translating variable area fan nozzle |
| 08/15/2013 | US20130206902 Power supply circuit for an aircraft de-icing system |
| 08/15/2013 | US20130206865 Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle |
| 08/15/2013 | CA2795647A1 Thermoelectric generator in turbine engine nozzles |
| 08/14/2013 | EP2626541A2 Variable area mechanism with angular trailing edges |
| 08/14/2013 | EP2625413A1 Aircraft propulsion assembly |
| 08/14/2013 | EP2625388A1 Thrust reverser |
| 08/14/2013 | DE102012002885A1 Fluggasturbinenschubumkehrvorrichtung Aircraft gas turbine thrust reverser |
| 08/13/2013 | US8505307 Translating variable area fan nozzle with split beavertail fairings |
| 08/08/2013 | US20130200178 Cascade-style variable area fan duct nozzle |
| 08/07/2013 | CN101946081B System for controlling the cowl of a turbojet engine nacelle thrust reverser |
| 08/07/2013 | CN101529073B Thrust reverser with grids for jet engine |
| 08/06/2013 | US8499544 Turbogenerator with cooling system |
| 08/01/2013 | US20130192215 Thermal insulation of rocket engines |
| 08/01/2013 | DE102012001571A1 Triebwerksgehäuse einer Fluggasturbine mit Schalldämpfungselementen im Fan-Einströmbereich Engine casing of an aircraft gas turbine with sound damping elements in the fan inflow |
| 07/31/2013 | EP2620628A2 Gas turbine engine nacelle with sound damping means in the fan intake area |
| 07/31/2013 | EP2620627A2 Nacelle cowling for a turbofan thrust reverse |
| 07/31/2013 | CN101946079B Control system for turbojet engine nacelle |
| 07/31/2013 | CN101410300B Air inlet shroud structure |
| 07/27/2013 | CA2800590A1 Nacelle |
| 07/25/2013 | WO2013107987A1 Twin-door thrust reverser |
| 07/24/2013 | EP2617978A2 Integrated thrust reverser actuator and variable area fan nozzle actuator |
| 07/24/2013 | EP2616656A1 Locking/unlocking device for a thrust reverser with sliding cover and adaptive nozzle for aircraft engine nacelle |
| 07/24/2013 | CN101939528B Variable area fan nozzle with bypass flow |
| 07/23/2013 | US8490744 Combustor and gas turbine having the same |
| 07/18/2013 | WO2012044822A3 Cowl assembly |
| 07/17/2013 | EP2615400A2 Multi-channel cooling bond pad and corresponding cooling method |
| 07/17/2013 | CN103210200A Nacelle for an aircraft bypass turbojet engine |
| 07/17/2013 | CN103210195A Thermal integration of thermoelectric device |
| 07/17/2013 | CN103209893A Turbojet engine nacelle reinforcing structure |
| 07/16/2013 | US8484944 Aerodynamic device for thrust reverser cascades |
| 07/11/2013 | WO2013103427A2 Linear detonation wave diverter |
| 07/11/2013 | WO2013102739A1 Seal for a turbojet engine pylon and nacelle, and turbojet engine pylon-nacelle assembly incorporating such a seal |
| 07/11/2013 | WO2013102724A1 Cellular acoustic structure for a turbojet engine and turbojet engine incorporating at least one such structure |
| 07/11/2013 | US20130175353 High-speed jet noise reduction via fluidic injection |
| 07/11/2013 | CA2857171A1 Cellular acoustic structure for a turbojet engine and turbojet engine incorporating at least one such structure |
| 07/10/2013 | CN103201491A Aircraft turbojet engine thrust reverser with a lower number of actuators |
| 07/10/2013 | CN103201490A Thrust reverser device without a control rod in the stream |
| 07/10/2013 | CN103201489A Actuation system for a propulsive unit of an airplane |
| 07/10/2013 | CN103195611A Turbofan engine and use method thereof |
| 07/10/2013 | CN101842571B Control and monitoring system and method |
| 07/09/2013 | US8479877 Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall element |
| 07/09/2013 | US8479491 Clamping system and method for thrust reverser attachment |
| 07/04/2013 | US20130167505 Seal for a variable area fan nozzle |
| 07/03/2013 | EP2610471A2 Seal for a variable area fan nozzle |
| 07/03/2013 | EP2610462A2 Gas turbine engine with low stage count low pressure turbine |