| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 03/05/2015 | WO2015031143A1 Three spool geared turbofan with low pressure compressor drive gear system and mechanical controller |
| 03/05/2015 | WO2015031083A1 Support assembly for a turbomachine |
| 03/05/2015 | WO2015030946A1 Gas turbine engine with fan clearance control |
| 03/05/2015 | WO2015028747A1 Isostatic suspension of a turbojet by rear double support |
| 03/05/2015 | US20150059315 Apparatus and method for bleeding off compressor air in a jet engine |
| 03/04/2015 | EP2841753A1 Thermal management system for a gas turbine engine |
| 03/04/2015 | EP2841739A2 Geared turbofan with three turbines all counter-rotating |
| 03/04/2015 | EP2841712A2 Aircraft engine driveshaft vessel assembly and method of assembling the same |
| 03/04/2015 | EP2841710A1 Gas turbine engine core providing exterior airfoil portion |
| 03/04/2015 | EP2841709A1 Airfoil with break-way, free-floating damper member |
| 03/04/2015 | EP2841708A1 Airfoil cooling enhancement and method of making the same |
| 03/04/2015 | EP2841705A1 Airfoil including loose damper |
| 03/04/2015 | EP2841704A1 Airfoil with powder damper |
| 03/04/2015 | EP2841702A1 Airfoil having tapered buttress |
| 03/04/2015 | EP2841700A1 Airfoil support method and apparatus |
| 03/04/2015 | EP2841699A1 Airfoil including damper member |
| 03/04/2015 | EP2841696A1 Blade having porous, abradable element |
| 03/03/2015 | USRE45397 Open-cycle internal combustion engine |
| 03/03/2015 | US8967967 Propfan engine |
| 03/03/2015 | US8967964 Boundary layer energiser |
| 03/03/2015 | US8967958 Integration of an air-liquid heat exchanger on an engine |
| 03/03/2015 | US8967950 Drive mechanism for a pair of contra-rotating propellers through an epicyclic gear train |
| 03/03/2015 | US8967944 Accessory gearbox buffer cooling air pump system |
| 03/03/2015 | US8966911 Turbofan engine with HP and LP power off-takes |
| 02/26/2015 | WO2015027131A1 High performance convergent divergent nozzle |
| 02/26/2015 | WO2015026444A1 Three spool turbofan engine with low noise intermediate turbine rotor |
| 02/26/2015 | US20150052908 Bleed duct assembly for a gas turbine engine |
| 02/25/2015 | EP2840236A1 Bleed duct assembly for a gas turbine engine |
| 02/24/2015 | US8961114 Integrated variable geometry flow restrictor and heat exchanger |
| 02/24/2015 | US8960597 Propulsion unit for an aircraft and air intake structure for such a unit |
| 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 |
| 02/19/2015 | WO2015021522A1 Axial turbomachines with rotary housing and fixed central element |
| 02/19/2015 | US20150047315 Gas turbine engine flow duct having integrated heat exchanger |
| 02/18/2015 | EP2836683A2 Tie shaft arrangement for turbomachine |
| 02/17/2015 | US8955304 Gas turbine engine with modular cores and propulsion unit |
| 02/12/2015 | WO2015019007A1 Integrated thrust reverser device and aircraft engine nacelle equipped therewith |
| 02/11/2015 | EP2835522A1 Device and method for letting off compressor air in an engine |
| 02/11/2015 | EP2834509A1 Combustor having a beveled grommet |
| 02/11/2015 | EP2834505A1 Geared architecture with inducer for gas turbine engine |
| 02/11/2015 | EP2834497A1 Turbomachine thermal management |
| 02/11/2015 | EP2834496A1 Differential geared architecture for gas turbine engine |
| 02/11/2015 | CN104350237A 飞机发动机传动轴容器组件和组装所述组件的方法 Aircraft engine drive shaft components and assembly of the container components |
| 02/11/2015 | CN103195612B 一种多功能涡轮风扇喷气发动机 A multifunctional turbofan jet engine |
| 02/10/2015 | US8950171 Counter-rotating gearbox for tip turbine engine |
| 02/05/2015 | WO2015017405A1 Method to immobilize an entrapped contaminant within a honeycomb structure |
| 02/05/2015 | WO2015017041A1 Gas turbine engine shaft bearing configuration |
| 02/05/2015 | DE102013219818B3 Axialverdichter Axial compressor |
| 02/05/2015 | DE102013215371A1 Vorrichtung und Verfahren zum Abblasen von Verdichterluft in einem Triebwerk Apparatus and method for blowing off compressor air in a jet engine |
| 02/04/2015 | EP2831403A1 Gas turbine engine fan drive gear system damper |
| 02/04/2015 | EP2831402A2 Gas turbine engine thrust reverser system |
| 02/04/2015 | EP2831396A2 Reverse core gear turbofan |
| 02/04/2015 | EP2831391A1 Torque frame bushing arrangement for gas turbine engine fan drive gear system |
| 02/04/2015 | CN104334863A 叶片的连结部结构及使用该连结部结构的喷气式发动机 The blade connecting portion structure and use of the structure of the jet engine connecting portion |
| 02/04/2015 | CN104334855A 航空器用发动机的风扇罩 Aircraft engine fan cover |
| 02/03/2015 | US8944765 Bellows type sealing device for partition penetration by a connecting rod of a turboprop fan blade orientation control system |
| 02/03/2015 | US8943793 Rear section of aircraft nacelle and nacelle equipped with such rear section |
| 02/03/2015 | US8943792 Gas-driven propulsor with tip turbine fan |
| 01/29/2015 | WO2015012923A2 Turbofan engine front section |
| 01/29/2015 | WO2015012920A2 Secondary nozzle for jet engine |
| 01/29/2015 | WO2015012919A2 Multi-nozzle flow diverter for jet engine |
| 01/29/2015 | WO2015011413A1 Hub of an intermediate casing for an aircraft turbojet engine comprising doors with contoured geometry |
| 01/29/2015 | WO2015011392A1 Intermediate housing hub for an aircraft turbofan, including air guide deflectors |
| 01/29/2015 | US20150027101 Geared gas turbine engine architecture for enhanced efficiency |
| 01/28/2015 | EP2828514A1 Trailing edge cooling |
| 01/28/2015 | EP2828508A1 Ignition unit for turbojet engine |
| 01/28/2015 | CN104314705A 船用涡轮喷气发动机防护设备 Marine turbojet protective equipment |
| 01/27/2015 | US8938944 Aircraft gas-turbine engine with oil cooler in the engine cowling |
| 01/27/2015 | US8938943 Gas turbine engine with bypass mixer |
| 01/21/2015 | EP2825824A1 Fuel air premixer for gas turbine engine |
| 01/21/2015 | EP2825760A1 Aerospace engine with augmenting turbojet |
| 01/21/2015 | EP2825759A1 Gas turbine engine variable stator vane assembly |
| 01/21/2015 | EP2825758A1 Pump system for tms aoc reduction |
| 01/21/2015 | EP2825757A1 Constant-speed pump system for engine thermal management system aoc reduction and environmental control system loss elimination |
| 01/21/2015 | EP2825733A2 Shark-bite tip shelf cooling configuration |
| 01/21/2015 | CN104295405A 一种降低小涵道比航空涡扇发动机外涵道气体流阻的方法 An aviation Xiaohan Road than outer bypass turbofan engine method of reducing gas flow resistance |
| 01/20/2015 | US8935923 Gas turbine engine with intercooling turbine section and intercooling turbine section bypass |
| 01/20/2015 | US8935913 Geared turbofan gas turbine engine architecture |
| 01/20/2015 | US8935912 Gas turbine engine with variable overall pressure ratio |
| 01/15/2015 | WO2015006538A1 Plastic variable inlet guide vane |
| 01/15/2015 | WO2015006445A1 Plated polymer nacelle |
| 01/15/2015 | US20150013301 Turbine engine including balanced low pressure stage count |
| 01/15/2015 | DE102013213520A1 Vorrichtung und Verfahren zum Ableiten von Sperrluft in einem Turbofan-Triebwerk Apparatus and method for deriving blocking air in a turbofan engine |
| 01/15/2015 | DE102013213518A1 Turbofan-Triebwerk Turbofan engine |
| 01/14/2015 | EP2823174A1 Erosion resistant and hydrophobic article |
| 01/14/2015 | EP2823170A1 Gas turbine engine fuel heating system |
| 01/14/2015 | CN104285054A 具有被吹扫的隔离空气腔的燃料喷射器 Was purged with isolated air chamber of the fuel injector |
| 01/13/2015 | US8932091 Propulsion system |
| 01/13/2015 | US8931588 Acoustic panel |
| 01/13/2015 | US8931285 Planetary gear system arrangement with auxiliary oil system |
| 01/13/2015 | US8931284 Flow discharge device |
| 01/13/2015 | CA2582624C Flame-retention arm of a post-combustion chamber |
| 01/08/2015 | WO2015001827A1 Stator vane structure and turbofan jet engine using same |
| 01/08/2015 | US20150007549 Rotary Turbo Rocket |
| 01/08/2015 | DE112013002188T5 Brennstoffeinspritzvorrichtung mit gespültem Isolierlufthohlraum Fuel injector with washed Isolierlufthohlraum |
| 01/07/2015 | EP2821657A1 Bearing arrangement |
| 01/07/2015 | EP2821627A1 Afterburner and aircraft engine |
| 01/07/2015 | EP2820282A2 Counter-rotating low pressure turbine with gear system mounted to mid turbine frame |
| 01/07/2015 | EP2820281A2 Counter-rotating low pressure turbine without turbine exhaust case |
| 01/07/2015 | EP2820280A2 Counter-rotating low pressure turbine with gear system mounted to turbine exhaust case |