| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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| 03/05/2015 | WO2015031823A1 Fuel manifold for a gas turbine engine |
| 03/05/2015 | WO2015031816A1 Gas turbine engine wall assembly with support shell contour regions |
| 03/05/2015 | WO2015031796A1 Hybrid diffuser case for a gas turbine engine combustor |
| 03/05/2015 | WO2015031763A1 Seal for gas turbine engine |
| 03/05/2015 | WO2015031384A1 Bifurcated sliding seal |
| 03/05/2015 | WO2015031185A1 Geared architecture gas turbine engine with oil scavenge |
| 03/05/2015 | WO2015031178A1 Torque connector lubrication scuppers |
| 03/05/2015 | WO2015031083A1 Support assembly for a turbomachine |
| 03/05/2015 | WO2015031058A1 Variable vane bushing |
| 03/05/2015 | WO2015031057A1 Gas turbine engine airfoil crossover and pedestal rib cooling arrangement |
| 03/05/2015 | WO2015030948A1 Gas turbine engine diffuser cooling and mixing arrangement |
| 03/05/2015 | WO2015030946A1 Gas turbine engine with fan clearance control |
| 03/05/2015 | WO2015030928A1 Swirler mount interface for a gas turbine engine combustor |
| 03/05/2015 | WO2015030927A1 Contoured dilution passages for a gas turbine engine combustor |
| 03/05/2015 | WO2015030926A1 Baffle for gas turbine engine vane |
| 03/05/2015 | WO2015030858A2 Geared annular airflow actuation system for variable cycle gas turbine engines |
| 03/05/2015 | WO2015030857A2 Annular airflow actuation system for variable cycle gas turbine engines |
| 03/05/2015 | WO2015029444A1 Erosion resistant material and turbine blade |
| 03/05/2015 | WO2015028756A1 Two-part auxiliary arm for a turbofan nacelle |
| 03/05/2015 | WO2015028747A1 Isostatic suspension of a turbojet by rear double support |
| 03/05/2015 | WO2015028052A1 Recuperator, micro gas turbine and use of the recuperator |
| 03/05/2015 | WO2015028051A1 Axial air bearing and micro gas turbine |
| 03/05/2015 | US20150065025 Environmental control system including a compressing device |
| 03/05/2015 | US20150065023 Intercompressor bleed turbo compressor |
| 03/05/2015 | US20150064001 Case structure interposed between the engine and the nacelle with jointed ferrule segments |
| 03/05/2015 | US20150064000 Coupling part structure for vane and jet engine including the same |
| 03/05/2015 | US20150063411 Non-intrusive measurment of hot gas temperature in a gas turbine engine |
| 03/05/2015 | US20150060403 Methods for manufacturing an additively manufactured fuel contacting component to facilitate reducing coke formation |
| 03/05/2015 | US20150059355 Method and System for Controlling Gas Turbine Performance With a Variable Backflow Margin |
| 03/05/2015 | US20150059353 Gas Turbine Combustion System |
| 03/05/2015 | US20150059352 Dual fuel combustor for a gas turbine engine |
| 03/05/2015 | US20150059350 System and method of recirculating exhaust gas for use in a plurality of flow paths in a gas turbine engine |
| 03/05/2015 | US20150059347 Method for controlling coupling between a first machine and a second machine |
| 03/05/2015 | US20150059346 Device for injecting air and fuel into a combustion chamber of a turbine engine |
| 03/05/2015 | DE112013002879T5 Verfahren zur Entfernung von Auswuchtungsmaterial eines Turbinenrades A method for removing a turbine wheel Auswuchtungsmaterial |
| 03/05/2015 | DE112013002029T5 Schleuderscheiben-Öldichtung und Turbolader mit Schleuderscheiben-Öldichtung Slingers oil seal and turbocharger centrifugal wheel oil seal |
| 03/05/2015 | DE102014217053A1 Tragkonstruktion für eine Läuferwelle sowie ein Turbolader Support structure for a rotor shaft and a turbocharger |
| 03/05/2015 | DE102014111770A1 System und Verfahren zur Steuerung der Brennstoffverteilung in der Brennkammer einer Gasturbine System and method for controlling fuel distribution in the combustion chamber of a gas turbine |
| 03/05/2015 | DE102014111697A1 Systeme und Verfahren zum Enteisen eines Einlaufsiebs einer Gasturbine und zum Entfeuchten von Lufteinlauffiltern Systems and methods for de-icing an Einlaufsiebs a gas turbine and for dehumidifying air inlet filter |
| 03/05/2015 | DE102013217612A1 Verfahren zur definierten Ausrichtung eines wälzgelagerten Rotors eines Turboladers sowie Turbolader mit einem wälzgelagerten Rotor Defined process for aligning a rolling bearing supports the rotor of a turbocharger and turbocharger with a rolling bearing-mounted rotor |
| 03/05/2015 | DE102013217504A1 Strömungsmaschine Flow machine |
| 03/05/2015 | DE102013109492A1 Schallabsorber, Schallabsorberanordnung und ein Triebwerk mit einer Schallabsorberanordnung Sound absorbers, sound absorber arrangement and an engine with a sound absorber arrangement |
| 03/05/2015 | DE102008062088B4 Vorrichtung zur Energie-Rückgewinnung in Flugzeugtriebwerken beim Landeanflug. An energy recovery in aircraft engines during the landing approach. |
| 03/04/2015 | EP2843213A1 Heat exchanger for aircraft engine |
| 03/04/2015 | EP2843212A1 Systems and methods for controlling gas turbines |
| 03/04/2015 | EP2843211A1 Gas turbine with improved part load emissions behavior |
| 03/04/2015 | EP2843210A1 Improved intake arrangement in gas turbine power plant |
| 03/04/2015 | EP2843191A1 Axial flow machine cooling system |
| 03/04/2015 | EP2841753A1 Thermal management system for a gas turbine engine |
| 03/04/2015 | EP2841742A1 Method and system for the emergency start-up of an energy generator set |
| 03/04/2015 | EP2841741A2 Systems and methods for preventing fuel leakage in a gas turbine engine |
| 03/04/2015 | EP2841718A2 Gas turbine engine with high speed low pressure turbine section and bearing support features |
| 03/04/2015 | EP2841717A2 Dual spring bearing support housing |
| 03/04/2015 | EP2841712A2 Aircraft engine driveshaft vessel assembly and method of assembling the same |
| 03/04/2015 | EP2841711A2 Gas turbine engine airfoil trailing edge passage and core for making 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 | EP2841707A2 Airfoil having minimum distance ribs |
| 03/04/2015 | EP2841706A2 Airfoil having internal lattice network |
| 03/04/2015 | EP2841705A1 Airfoil including loose damper |
| 03/04/2015 | EP2841704A1 Airfoil with powder damper |
| 03/04/2015 | EP2841703A1 Gas turbine engine airfoil geometries and cores for manufacturing process |
| 03/04/2015 | EP2841702A1 Airfoil having tapered buttress |
| 03/04/2015 | EP2841701A1 Gas turbine engine airfoil impingement cooling |
| 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 |
| 03/04/2015 | EP2841180A1 Gas filter device provided with a means for attaching and removing the filtering elements for maintenance |
| 03/03/2015 | USRE45397 Open-cycle internal combustion engine |
| 03/03/2015 | US8968437 Jet engine with deflector |
| 03/03/2015 | US8967978 Axial retention for fasteners in fan joint |
| 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 | US8967627 Intershaft seal |
| 03/03/2015 | US8967531 Aircraft and airborne electrical power and thermal management system |
| 03/03/2015 | US8967330 Method for repairing a sound attenuation panel |
| 03/03/2015 | US8966911 Turbofan engine with HP and LP power off-takes |
| 03/03/2015 | US8966909 System for reducing combustion dynamics |
| 03/03/2015 | US8966905 Combustion device |
| 03/03/2015 | US8966904 Architecture for feeding fuel to a power plant for driving a rotary wing of a rotorcraft |
| 03/03/2015 | US8966903 Combustor resonator with non-uniform resonator passages |
| 03/03/2015 | US8966878 Gas turbine |
| 03/03/2015 | US8966877 Gas turbine combustor with variable airflow |
| 03/03/2015 | US8966876 Controllable speed windmill operation of a gas turbine engine through low spool power extraction |
| 03/03/2015 | US8966875 Constant speed transmission for gas turbine engine |
| 02/26/2015 | WO2015027131A1 High performance convergent divergent nozzle |
| 02/26/2015 | WO2015027064A1 Components having vibration dampers enclosed therein and method of forming such components |
| 02/26/2015 | WO2015026798A1 Replacing an aperture with an annular bushing in a composite laminated composite component |
| 02/26/2015 | WO2015026760A1 Dual fuel nozzle system and apparatus |
| 02/26/2015 | WO2015026598A1 Gas turbine engine component providing prioritized cooling |
| 02/26/2015 | WO2015026597A1 Variable area turbine arrangement with secondary flow modulation |
| 02/26/2015 | WO2015026591A1 Gas turbine engine duct assembly |
| 02/26/2015 | WO2015026534A1 Belly band seal with circumferential spacer |
| 02/26/2015 | WO2015026444A1 Three spool turbofan engine with low noise intermediate turbine rotor |
| 02/26/2015 | WO2015025109A1 Method and system for injecting fuel into an engine combustion chamber |
| 02/26/2015 | US20150052907 Thermal management system for gas turbine engine |
| 02/26/2015 | US20150052905 Pulse Width Modulation for Control of Late Lean Liquid Injection Velocity |
| 02/26/2015 | US20150052903 Alignment and measuring tool for a turbomachine |