| 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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| 03/05/2015 | WO2015028755A1 Nacelle comprising a thrust reverser device with maintained mobile grids |
| 03/05/2015 | WO2015028735A1 Thrust reverser of a turbojet nacelle, comprising grids and cylinders fixed upstream of mobile hoods |
| 03/05/2015 | US20150060194 Sound absorber, sound absorber assembly and an engine with a sound absorber assembly |
| 03/04/2015 | EP2843195A1 Gas turbine engine guide wheel |
| 03/04/2015 | EP2841752A1 Actuating device for moving a mobile cap of a thrust reverser |
| 03/04/2015 | EP2841751A1 Actuating device for moving a thrust reverser |
| 03/04/2015 | EP2841750A2 Variable immersion lobe mixer for turbofan jet engine exhauts and method of fabricating the same |
| 03/04/2015 | EP2841749A1 Connecting gas turbine engine annular members |
| 03/04/2015 | EP2841340A1 Turbofan engine nacelle with downstream section |
| 03/03/2015 | US8967964 Boundary layer energiser |
| 03/03/2015 | US8967570 Blind retention mount |
| 02/26/2015 | WO2015027131A1 High performance convergent divergent nozzle |
| 02/26/2015 | WO2015026417A2 Dual-mode plug nozzle |
| 02/26/2015 | US20150056070 Multi surface blocker door system and apparatus |
| 02/26/2015 | US20150053789 Linkage to control and restrain flap movement |
| 02/26/2015 | US20150052875 Blocker door actuation system and apparatus |
| 02/24/2015 | US8962968 Thermoelectric generation for a gas turbine |
| 02/24/2015 | US8961114 Integrated variable geometry flow restrictor and heat exchanger |
| 02/24/2015 | US8959924 Aircraft turbofan engine |
| 02/24/2015 | US8959889 Method of varying a fan duct nozzle throat area of a gas turbine engine |
| 02/24/2015 | CA2693352C Device and control process for supplying power to at least one maintenance actuator in an aircraft |
| 02/19/2015 | WO2015023412A1 Noise absorbing structure comprising a honeycomb with an internal septum |
| 02/19/2015 | US20150048177 Exhaust nozzle and method for changing exhaust flow path |
| 02/19/2015 | DE102008020198B4 Düsenerweiterung für ein Triebwerk und Verfahren zur Herstellung und Kühlung einer Düsenerweiterung Nozzle extension for a jet engine and process for producing and cooling a nozzle extension |
| 02/18/2015 | EP2837811A1 A panel attachment system |
| 02/18/2015 | EP2837810A1 Thrust reverser unit |
| 02/18/2015 | EP2837776A1 A panel attachment system |
| 02/17/2015 | US8955306 Method for synchronizing the actuators of a movable thrust reverser cowl |
| 02/17/2015 | US8955305 Self-calibration method for the electric jacks of a turbojet nacelle |
| 02/17/2015 | CA2694923C System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 02/12/2015 | WO2015019007A1 Integrated thrust reverser device and aircraft engine nacelle equipped therewith |
| 02/12/2015 | US20150041059 Inner fixed structure with attached corner fitting |
| 02/12/2015 | DE102004018725B4 Dämpfung von Schwingungen einer Brennkammer durch Resonatoren Damping of oscillations of a combustion chamber through resonators |
| 02/10/2015 | US8951006 Nacelle for the jet engine of an aircraft |
| 02/10/2015 | CA2696223C Spring for a cascade-type thrust reverser shutter for an aircraft jet engine |
| 02/10/2015 | CA2674260C Nacelle for aircraft jet engine and aircraft including such nacelle |
| 02/05/2015 | WO2015017492A1 Thrust reverser system with translating-rotating hinge assembly |
| 02/05/2015 | WO2015015111A1 Propulsion assembly for aircraft |
| 02/05/2015 | US20150037135 Acoustic liner |
| 02/05/2015 | US20150033747 Convergent-divergent nozzle for a turbine engine |
| 02/04/2015 | EP2833356A2 Acoustic panel |
| 02/04/2015 | EP2832973A1 Acoustic liner |
| 02/04/2015 | EP2831402A2 Gas turbine engine thrust reverser system |
| 02/04/2015 | EP2831382A1 Integration of parts of an afterbody of an aircraft engine |
| 02/04/2015 | CN104334451A 用于涡轮喷气发动机机舱的推力反向器的单件罩的锁定/解锁装置 For turbojet engine thrust reverser nacelle of a single piece cap locking / unlocking device |
| 02/03/2015 | US8943794 Linear telescopic actuator for moving a first and a second element relative to a stationary element |
| 01/29/2015 | WO2015011198A1 Combustion gas discharge nozzle for a rocket engine provided with a sealing device between a stationary part and a moving part of the nozzle |
| 01/29/2015 | US20150028129 Biconical exhaust cone for a civil aviation jet engine |
| 01/28/2015 | EP2828513A1 Aircraft turbojet engine exhaust cone |
| 01/28/2015 | EP2828490A1 Variable-section jet pipe and aircraft turbojet engine nacelle equipped with such a jet pipe |
| 01/27/2015 | US8939401 System for controlling the cowl of a turbojet engine nacelle thrust reverser |
| 01/27/2015 | US8939397 Aircraft capable of hovering having an exhaust duct with thermoelectric conversion circuit |
| 01/27/2015 | US8938972 Engine apparatus and method for reducing a side load on a flying object |
| 01/27/2015 | US8938971 Flow straightener and mixer |
| 01/27/2015 | US8938944 Aircraft gas-turbine engine with oil cooler in the engine cowling |
| 01/22/2015 | WO2015008037A1 A thrust flow powered vehicle |
| 01/22/2015 | WO2015007987A1 Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face |
| 01/22/2015 | US20150021117 Duct and method for damping pressure waves caused by thermoacoustic instability |
| 01/21/2015 | CN204113490U 一种球面矢量喷管球面密封结构 A Spherical vectoring nozzle spherical sealing structure |
| 01/21/2015 | CN204113489U 一种防止球面收敛喷管球面调节片卡滞的结构 A spherical spherical convergent nozzle flaps prevent catching structure |
| 01/21/2015 | CN204113488U 一种球面收敛喷管冷却流量控制结构 A Spherical convergent nozzle cooling flow control structure |
| 01/21/2015 | CN104295404A 二元流体式推力矢量动力装置 Binary fluid type thrust vector power plant |
| 01/21/2015 | CN102953865B 一种塞式轴对称喷管塞锥的冷却结构 An axisymmetric plug plug cone nozzle cooling structure |
| 01/21/2015 | CN102799739B 一种考虑安装性能的发动机喷管喉道面积调节设计方法 Consider installing one kind of performance engine nozzle throat area regulating the design method |
| 01/15/2015 | WO2015006445A1 Plated polymer nacelle |
| 01/15/2015 | WO2015004059A1 Turbine engine casing having a cut-out flange |
| 01/15/2015 | US20150016965 Link arm drag reducing device |
| 01/14/2015 | EP2824308A1 Exhaust mixer with offset lobes |
| 01/14/2015 | EP2823173A2 Seal assembly |
| 01/14/2015 | CN104285055A 推力反向控制系统 Thrust reverser control system |
| 01/13/2015 | US8932176 Linear actuator and method of operation thereof |
| 01/13/2015 | US8932091 Propulsion system |
| 01/13/2015 | US8931736 Nacelle |
| 01/13/2015 | US8931281 External flap retaining mechanism |
| 01/13/2015 | US8931269 Temperature activatable actuator |
| 01/13/2015 | US8931253 Double-acting telescopic linear actuator with single-motor drive system |
| 01/09/2015 | CA2851073A1 Exhaust mixer with offset lobes |
| 01/08/2015 | WO2015002805A1 Gas turbine engine system for modulating flow of fan by-pass air and core engine air |
| 01/08/2015 | WO2015002637A1 Engine and band clamp |
| 01/08/2015 | US20150008268 Pivot thrust reverser with multi-point actuation |
| 01/07/2015 | EP2821621A1 Acoustic structure for a gas turbine engine |
| 01/07/2015 | EP2819920A1 Flattened nacelle of a turbojet engine |
| 01/07/2015 | CN104271894A 航空器发动机艉部的部件集成 Aircraft engine components, integrated stern |
| 01/07/2015 | CN104271890A 具有展开控制的阻断襟翼的推力反向器 Having a blocking flap deployment control thrust reverser |
| 01/07/2015 | CN102900564B 用于轴流压缩系统叶顶喷气稳定性控制的控制器 Axial compression system for tip stability control jet controller |
| 01/06/2015 | US8925332 Anti-fire seal assembly and nacelle comprising such a seal |
| 01/06/2015 | US8925295 Air discharging device for an aircraft double-flow turbine engine |
| 01/06/2015 | CA2603312C Method and system to facilitate cooling turbine engines |
| 01/01/2015 | US20150000289 Gas ejection cone for aircraft turbojet engines |
| 01/01/2015 | US20150000252 Rotational annular airscrew with integrated acoustic arrester |
| 12/31/2014 | CN104254481A 有下游段的涡轮喷气发动机机舱 There turbojet engine nacelle downstream segment |
| 12/31/2014 | CN104251167A 用于可变面积风扇喷嘴的枢转环形瓣片致动 Pivoting annular flap for a variable area fan nozzle actuator |
| 12/30/2014 | US8919668 Thrust reverser having a lockable variable nozzle section |
| 12/30/2014 | US8919667 Nacelle with a variable nozzle section |
| 12/30/2014 | US8919136 Flexible abutment links for attaching a part made of CMC |
| 12/30/2014 | US8919096 System for controlling a plurality of functions of a turbojet engine |
| 12/30/2014 | CA2666614C Side-opening jet engine nacelle |
| 12/30/2014 | CA2609228C Turbofan engine nozzle assembly and method for operating the same |
| 12/25/2014 | US20140373927 Low shock strength propulsion system |
| 12/25/2014 | US20140373550 Tail cone for a microjet rotary turbine engine |