| 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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| 02/02/2012 | US20120023964 Liquid-fueled premixed reverse-flow annular combustor for a gas turbine engine |
| 02/02/2012 | US20120023959 Power plant and method of use |
| 02/02/2012 | US20120023957 Power plant and method of operation |
| 02/02/2012 | US20120023955 Power plant and method of operation |
| 02/02/2012 | US20120023954 Power plant and method of operation |
| 02/02/2012 | US20120023952 Fuel nozzle and assembly and gas turbine comprising the same |
| 02/02/2012 | US20120023951 Fuel nozzle with air admission shroud |
| 02/02/2012 | US20120023897 Auxiliary power unit fire enclosure drain seal |
| 02/02/2012 | US20120023896 Auxiliary power unit fire enclosure drain |
| 02/02/2012 | US20120023895 Apparatus and filtering systems relating to combustors in combustion turbine engines |
| 02/02/2012 | US20120023894 Systems, methods, and apparatus for monitoring corrosion or corrosive contaminants associated with liquid fuel |
| 02/02/2012 | US20120023893 Cooling device for high temperature fluid, flight vehicle having the same and cooling method for high temperature fluid |
| 02/02/2012 | US20120023892 Systems and methods for co2 capture |
| 02/02/2012 | DE19940556B4 Vorrichtung zum Kühlen von Leit- oder Laufschaufeln in einer Gasturbine Device for the cooling of guide vanes or rotor blades in a gas turbine |
| 02/02/2012 | DE102010032324A1 Heat exchanger for use in arrangement, particularly for gas turbine engine, has cross-flow matrix, distributor tube for guiding heat carrier medium into cross-flow matrix and collecting tube for discharging heat transfer medium |
| 02/02/2012 | DE102008026941B4 Vorrichtung zum Verbinden einer Wabendichtung mit einem Dichtungsträger A device for connecting a honeycomb seal with a seal carrier |
| 02/02/2012 | DE102006024968B4 Gasturbine, Verfahren zum Steuern der Luftzufuhr und Computerprogrammprodukt zum Steuern der Luftzufuhr Gas turbine method for controlling the air supply, and computer program product for controlling the air supply |
| 02/02/2012 | DE102005023536B4 Vormischbrenner mit aufprallgekühltem Mittelkörper und Verfahren zum Kühlen des Mittelkörpers Premix burner with aufprallgekühltem central body and method of cooling of the centerbody |
| 02/02/2012 | CA2806165A1 Lateral turbojet improved in order to limit the deformation thereof |
| 02/01/2012 | EP2412953A2 Inorganic coke resistant coatings to prevent aircraft fuel system fouling |
| 02/01/2012 | EP2412952A2 Aircraft engine control during icing of temperature probe |
| 02/01/2012 | EP2412929A1 Cmc turbine stator vane |
| 02/01/2012 | EP2412928A1 Cmc turbine stator vane |
| 02/01/2012 | EP2412925A1 Turbine blade and gas turbine |
| 02/01/2012 | EP2411644A2 Variable actuation pressure system for independent pressure control |
| 02/01/2012 | EP2411281A2 Aircraft nacelle comprising a reinforced outer wall |
| 02/01/2012 | EP2274205B1 Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle |
| 02/01/2012 | CN202132114U 飞机发动机油封供油装置 Aircraft engine oil seal oil installations |
| 02/01/2012 | CN202132113U 蒸发管燃油雾化装置和包括其的燃气涡轮发动机 Fuel atomization and evaporation tube apparatus including a gas turbine engine |
| 02/01/2012 | CN202132112U Compressed air backflow compression system |
| 02/01/2012 | CN202132101U 动力流体气体工质压缩系统 Dynamic fluid refrigerant gas compression system |
| 02/01/2012 | CN102341588A Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train |
| 02/01/2012 | CN102341568A Rotor element with a fluid passage and passage-blocking member, and turbine engine including the rotor element |
| 02/01/2012 | CN101765744B 燃气轮机 Gas turbine |
| 01/31/2012 | US8105024 Seal in gas turbine |
| 01/31/2012 | US8104708 Suspension for mounting a turbojet engine on an aircraft |
| 01/31/2012 | US8104291 Combustion cap floating collar using E-seal |
| 01/31/2012 | US8104290 Combustion liner damper |
| 01/31/2012 | US8104289 Systems and methods involving multiple torque paths for gas turbine engines |
| 01/31/2012 | US8104286 Methods and systems to enhance flame holding in a gas turbine engine |
| 01/31/2012 | CA2601041C Modular fuel nozzle and method of making |
| 01/30/2012 | CA2747614A1 Fan embedded power generator |
| 01/30/2012 | CA2746242A1 Apparatus for a high speed sleeveless rotor |
| 01/26/2012 | WO2012010156A1 Compensator for connecting pipes for dust-laden flue gas |
| 01/26/2012 | WO2011152906A3 Optical monitoring system for a turbine engine |
| 01/26/2012 | US20120020773 Filter cassette, filter arrangement, and gas turbine with such filter cassette |
| 01/26/2012 | US20120018005 Coupling device for connecting the two half-shells of an aircraft engine nacelle, and nacelle equipped with such a device |
| 01/26/2012 | US20120017605 Heat transfer augmented fluid flow surfaces |
| 01/26/2012 | US20120017604 Gas turbine arrangement and method for retrofitting same |
| 01/26/2012 | US20120017602 Systems and methods for controlling the startup of a gas turbine |
| 01/26/2012 | US20120017601 Gas turbine with improved part load emissions behavior |
| 01/26/2012 | US20120017598 Metallic ceramic spool for a gas turbine engine |
| 01/26/2012 | US20120017594 Seal assembly for controlling fluid flow |
| 01/26/2012 | US20120017564 Superconductive heat transfer system |
| 01/26/2012 | CA2803657A1 Compensator for connecting pipes for dust-laden flue gas |
| 01/25/2012 | EP2410154A2 Systems and methods for controlling the startup of a gas turbine |
| 01/25/2012 | EP2410153A2 A hybrid power generation system and a method thereof |
| 01/25/2012 | EP2410152A2 Fan case assembly and method |
| 01/25/2012 | EP2410128A1 Internal cooling for a flow machine |
| 01/25/2012 | EP2410125A1 Gas turbine |
| 01/25/2012 | EP2409009A2 Burner assembly |
| 01/25/2012 | EP2408845A1 Co-polymer based polyimide articles and their uses in an aircraft |
| 01/25/2012 | EP1456510B1 Turbine noise absorber |
| 01/25/2012 | CN202125357U Prepositioned module for gas system |
| 01/25/2012 | CN202125356U Casing for fuel module of auxiliary engine of combustion engine |
| 01/25/2012 | CN202125355U Fuel module in auxiliary engine for fuel machine |
| 01/25/2012 | CN1724851B Method and system for operating rotary machines |
| 01/25/2012 | CN102333935A Turbine blade and gas turbine |
| 01/25/2012 | CN102330605A Heavy combustion engine assembling method for assembling rotor and front and rear supports in combining manner |
| 01/25/2012 | CN102330604A Regenerator, regeneration process, and liquid polymer mixture for a regenerator |
| 01/25/2012 | CN102330603A Method and system for periodic cooling, storing, and heating of atmospheric gas |
| 01/25/2012 | CN102330602A Pre-filtration bypass for gas turbine inlet filter house |
| 01/25/2012 | CN101024324B Environment barrier coating for a component and method for fabricating the same |
| 01/24/2012 | US8100666 Rotor mounting system for gas turbine engine |
| 01/24/2012 | US8099963 Device for mounting an igniter plug in a combustion chamber of a gas turbine engine |
| 01/24/2012 | US8099962 Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine |
| 01/24/2012 | US8099960 Triple counter rotating swirler and method of use |
| 01/24/2012 | US8099943 Exhaust duct with bypass channel |
| 01/24/2012 | US8099941 Methods and systems for controlling a combustor in turbine engines |
| 01/24/2012 | CA2600104C Jig |
| 01/24/2012 | CA2570773C Fuel nozzle and manifold assembly connection |
| 01/24/2012 | CA2472324C Cooled blade of a gas turbine starter |
| 01/24/2012 | CA2467842C Nozzle flap for aircraft turbojets |
| 01/24/2012 | CA2465071C Diametrically energized piston ring |
| 01/20/2012 | CA2746927A1 Fan case assembly and method |
| 01/19/2012 | WO2012009575A2 Generating power using an ion transport membrane |
| 01/19/2012 | WO2012008213A1 Combined cycle power generator |
| 01/19/2012 | WO2012007638A2 A solution for controlling a turbo compressor |
| 01/19/2012 | WO2012007341A1 Gas turbine with a secondary air system and method for operating such a gas turbine |
| 01/19/2012 | WO2011148078A3 Gearbox in a turbomachine |
| 01/19/2012 | US20120011857 High-Flow-Capacity Centrifugal Hydrogen Gas Compression Systems, Methods and Components Therefor |
| 01/19/2012 | US20120011824 Integral lubrication tube and nozzle combination |
| 01/19/2012 | CA2805224A1 Generating power using an ion transport membrane |
| 01/18/2012 | EP2407660A2 Auxiliary hydraulic power generation system |
| 01/18/2012 | EP2407652A1 Gas turbine with a secondary air system and method for operating such a gas turbine |
| 01/18/2012 | EP2407644A2 Geared turbofan emergency power |
| 01/18/2012 | EP2406786A1 Aircraft acoustic attenuation member and method for forming said member |
| 01/18/2012 | EP2406484A1 Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train |
| 01/18/2012 | EP2406477A2 Turbine engine support arms |
| 01/18/2012 | EP2406462A1 Rotor element with a fluid passage and passage-blocking member, and turbine engine including the rotor element |