| 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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| 08/15/2012 | CN102639843A Variable performance valve |
| 08/15/2012 | CN102635446A Turbine inlet air filter system |
| 08/15/2012 | CN102635445A Acoustic panel treatment with a junction between two parties and repair method of an acoustic panel |
| 08/15/2012 | CN102635444A Turbine inlet air system |
| 08/15/2012 | CN102635443A Utilization device for spiral internal air energy |
| 08/15/2012 | CN102634392A System and method for producing a hydrogen enriched fuel |
| 08/14/2012 | US8241560 Nickel base superalloy and single crystal castings |
| 08/14/2012 | US8240153 Method and system for controlling a set point for extracting air from a compressor to provide turbine cooling air in a gas turbine |
| 08/14/2012 | US8240124 Method of taking off auxiliary power from an airplane turbojet, and a turbojet fitted to implement such a method |
| 08/14/2012 | US8240045 Gas turbine transition duct coupling apparatus |
| 08/14/2012 | CA2571236C Heat exchanger with header tubes |
| 08/11/2012 | CA2767321A1 Turbine inlet air system |
| 08/09/2012 | WO2012106734A1 Axial brush seal |
| 08/09/2012 | WO2012104180A1 Liquid fuel assist ignition system of a gas turbine and method to provide a fuel/air mixture to a gas turbine |
| 08/09/2012 | WO2012051315A3 Generating power using an ion transport membrane |
| 08/09/2012 | US20120198857 Condition measurement apparatus and method |
| 08/09/2012 | US20120198816 Gas turbine engine compressor arrangement |
| 08/09/2012 | US20120198815 Gas turbine engine with low stage count low pressure turbine |
| 08/09/2012 | US20120198810 Strut airfoil design for low solidity exhaust gas diffuser |
| 08/09/2012 | US20120198653 Fuel injector bearing plate assembly and swirler assembly |
| 08/09/2012 | DE102012100887A1 Dampfdichtungsabfluss-Wiedereinleitungssystem Vapor seal drain reinjection system |
| 08/09/2012 | DE102012100884A1 Feuchtigkeits-Ableitungsvorrichtung und -Verfahren für ein Lufteinlasssystem Moisture-dissipating device and method for an air intake system |
| 08/09/2012 | DE102011003702A1 Lagervorrichtung, insbesondere für eine Welle eines Turboladers, sowie ein Turbolader mit einer solchen Lagervorrichtung Storage device, in particular for a shaft of a turbocharger, and a turbocharger having a bearing device such |
| 08/08/2012 | EP2484882A1 Aircraft power generating assembly |
| 08/08/2012 | EP2484881A1 Turbine engine tailcone resonator |
| 08/08/2012 | EP2484880A1 Liquid fuel assist ignition system of a gas turbine and method to provide a fuel/air mixture to a gas turbine |
| 08/08/2012 | EP2484806A2 Surface treatment method and repair method |
| 08/08/2012 | EP2483545A2 Internally nested variable-area fuel nozzle |
| 08/08/2012 | EP2482988A1 Method and device for gas cleaning |
| 08/08/2012 | EP2244942B1 Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing |
| 08/08/2012 | EP1718857B1 Integrated air inlet system for multi-propulsion aircraft engines |
| 08/08/2012 | CN202370665U Novel pulse jet engine |
| 08/08/2012 | CN202370664U Gas turbine circulation device with middle water spraying cooling and steam reinjection functions |
| 08/08/2012 | CN102630193A Method for repairing wall member with passage |
| 08/08/2012 | CN102628403A Strut airfoil design for low solidity exhaust gas diffuser |
| 08/08/2012 | CN102626582A Moisture diversion apparatus for air inlet system and method |
| 08/08/2012 | CN101249725B Method of manufacturing a gas turbine casing out of composite material, and a casing as obtained thereby |
| 08/07/2012 | US8237298 Generator coupling for use with gas turbine engine |
| 08/07/2012 | US8234875 Gas turbine fuel metering unit |
| 08/07/2012 | US8234871 Method and apparatus for delivery of a fuel and combustion air mixture to a gas turbine engine using fuel distribution grooves in a manifold disk with discrete air passages |
| 08/07/2012 | US8234870 Additive injection system for improving thermal stability of jet fuel |
| 08/07/2012 | US8234869 Aviation engine inlet with tangential blowing for buzz saw noise control |
| 08/07/2012 | CA2550458C Valve assembly for a gas turbine engine |
| 08/07/2012 | CA2509489C Turbine engine with axial rotor restraint devices |
| 08/07/2012 | CA2432841C Methods and apparatus for operating gas turbine engines |
| 08/02/2012 | WO2012101087A1 Mixing element for gas turbine units with flue gas recirculation |
| 08/02/2012 | US20120195753 Gas turbine engine architecture with low pressure compressor hub between high and low rotor thrust bearings |
| 08/02/2012 | US20120193441 Aircraft Engine Nozzle |
| 08/02/2012 | US20120192572 Gas turbine engine |
| 08/02/2012 | US20120192571 Combustor liner support and seal assembly |
| 08/02/2012 | US20120192568 Gas Turbine Combustor |
| 08/02/2012 | US20120192567 Gas turbine engine flange assembly including flow circuit |
| 08/02/2012 | US20120192566 Fuel injection assembly for use in turbine engines and method of assembling same |
| 08/02/2012 | US20120192565 System for premixing air and fuel in a fuel nozzle |
| 08/02/2012 | DE102012100771A1 Verfahren und Vorrichtung für einen Labyrinthdichtungspackungsring Method and apparatus for a labyrinth packing ring |
| 08/02/2012 | DE102011009770A1 Verfahren und Vorrichtung zum Wechseln einer Dichtungsplatte und/oder einer Lagereinheit in einem Flugzeugtriebwerk Method and apparatus for changing a sealing plate and / or a storage unit in an aircraft engine |
| 08/02/2012 | DE102011009564A1 Bearing unit for shaft of turbo charger, has outer ring, inner ring and two bearing series guided between outer ring and inner ring |
| 08/02/2012 | DE102004054294B4 Kühlsystem für Plattformkanten von Leitradsegmenten Cooling system for platform edges of nozzle segments |
| 08/02/2012 | CA2824710A1 Mixing element for gas turbine units with flue gas recirculation |
| 08/01/2012 | EP2481902A2 Drain discharge equipment for compressor and gas turbine system |
| 08/01/2012 | EP2481887A2 Intershaft seal with support linkage |
| 08/01/2012 | EP2480779A1 Convertible fan engine |
| 08/01/2012 | EP2480778A1 A convertible fan engine comprising a two block compressor |
| 08/01/2012 | EP2480774A1 Fuel flowmeter having an improved control device |
| 08/01/2012 | EP2480773A1 Fuel line system, method for operating a gas turbine, and method for purging the fuel line system of a gas turbine |
| 08/01/2012 | CN202360227U Integral cantilever rotor structure |
| 08/01/2012 | CN202360226U System for heating natural gas by circulating cooling sea water |
| 08/01/2012 | CN202360225U Wave-type diffuser of combustion gas turbine |
| 08/01/2012 | CN102625877A Method and device for converting thermal energy from biomass into mechanical work |
| 08/01/2012 | CN102619624A Reformed multi-fuel premixed low emission combustor and related method |
| 08/01/2012 | CN102619623A Fuel reformer system for a turbomachine system |
| 07/31/2012 | US8230673 Rocket engine injectorhead with flashback barrier |
| 07/31/2012 | US8230672 Spark-integrated propellant injector head with flashback barrier |
| 07/31/2012 | CA2765672A1 Heated booster splitter plenum |
| 07/31/2012 | CA2580327C Fuel conveying member with side-brazed sealing members |
| 07/31/2012 | CA2500957C Air intake structure for aircraft engine |
| 07/26/2012 | WO2012099046A1 Power generation plant |
| 07/26/2012 | WO2012098322A2 Nacelle for an aircraft bypass turbojet engine |
| 07/26/2012 | WO2012098321A2 Nacelle for an aircraft bypass turbojet engine |
| 07/26/2012 | WO2012097998A1 Sound absorber for a gas turbine exhaust cone, and method for the production thereof |
| 07/26/2012 | WO2012097798A1 Intermediate housing of a gas turbine with an outer bounding wall, having upstream of a supporting rib a contour that changes in the circumferential direction, for reducing secondary flow losses |
| 07/26/2012 | US20120186270 Intershaft seal with support linkage |
| 07/26/2012 | US20120186269 Support between transition piece and impingement sleeve in combustor |
| 07/26/2012 | US20120186265 Stabilizing the flame of a burner |
| 07/26/2012 | US20120186264 Gas turbine combustor |
| 07/26/2012 | US20120186263 Power generation plant |
| 07/26/2012 | US20120186261 System and method for a gas turbine exhaust diffuser |
| 07/26/2012 | US20120186259 Fuel injector assembly |
| 07/26/2012 | US20120186258 Mixer assembly for a gas turbine engine |
| 07/26/2012 | US20120186257 Gas turbine internal manifold mounting arrangement |
| 07/26/2012 | US20120186256 Mixer assembly for a gas turbine engine |
| 07/26/2012 | US20120186255 System for pre-mixing in a fuel nozzle |
| 07/26/2012 | US20120186254 Damage-repairing method of transition piece and transition piece |
| 07/26/2012 | US20120186222 Combustion chamber of an aeronautical turbine engine with combustion holes having different configurations |
| 07/26/2012 | US20120186221 Internal combustion engine |
| 07/26/2012 | DE102012100523A1 System zur Vorvermischung in einer Brennstoffdüse System for premixing in a fuel nozzle |
| 07/26/2012 | DE102012100520A1 Halterung zwischen dem Übergangsstück und der Prallhülse in einer Brennkammer Support between the transition piece and the impingement sleeve in a combustion chamber |
| 07/26/2012 | DE102012100517A1 Prallhülse eines Übergangsstücks für eine Gasturbine Impingement sleeve of a transition piece for a gas turbine |
| 07/26/2012 | DE102012100468A1 Brennkammer für die emissionsarme Verbrennung von mehreren vorgemischten reformierten Brennstoffen und verwandtes Verfahren Combustion chamber for low-emission combustion of several premixed reformed fuels and related method |
| 07/26/2012 | DE102011009028A1 Turbine wheel for radial-flow turbine of supercharger of internal combustion engine of i.e. passenger car, has cooling passage extending into wheel for cooling wheel with cooling medium i.e. air, flowing through cooling passage |