| 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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| 02/27/2012 | CA2749481A1 Geared axial multistage expander device, system and method |
| 02/23/2012 | WO2012023302A1 System for supplying fuel to gas turbine combustor and method for supplying fuel to gas turbine combustor |
| 02/23/2012 | WO2012022873A2 Fuel injection system for turbojet engine and method of assembling such an injection system |
| 02/23/2012 | WO2012022869A2 Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 02/23/2012 | WO2012022551A2 Internal cooling arrangement for a turbomachine |
| 02/23/2012 | US20120042958 Jet engine intake guard |
| 02/23/2012 | US20120042660 Manifold mounting arrangement |
| 02/23/2012 | US20120042659 Air turbine starter inlet housing assembly airflow path |
| 02/23/2012 | US20120042658 Fuel supply system for gas turbine combustor and fuel supply method for gas turbine combustor |
| 02/23/2012 | US20120042656 Gas turbine engine with exhaust rankine cycle |
| 02/23/2012 | DE102010034766A1 Lageranordnung für die Verdichterseite eines Turboladers einer Verbrennungskraftmaschine Bearing arrangement for the compressor side of a turbocharger of an internal combustion engine |
| 02/23/2012 | CA2806024A1 Fuel injection system for turbojet engine and method of assembling such an injection system |
| 02/23/2012 | CA2803746A1 Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 02/22/2012 | EP2420652A2 Manifold mounting arrangement |
| 02/22/2012 | EP2420650A2 Steam turbine, system, and method of operation |
| 02/22/2012 | EP2420584A1 Nickel-base single-crystal superalloy and turbine wing using same |
| 02/22/2012 | EP2419617A1 Method for detecting an icing condition of or the need for servicing a fuel circuit of a turbine engine |
| 02/22/2012 | EP2419616A1 Double-body gas turbine engine provided with an inter-shaft bearing |
| 02/22/2012 | EP1454044B1 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 02/22/2012 | CN1950589B 燃气轮机的叶片 Gas turbine blades |
| 02/22/2012 | CN102362109A Shaft seal device |
| 02/22/2012 | CN102362107A Shaft seal and rotary machine with same |
| 02/22/2012 | CN102362086A Bearing device, bearing unit, and rotary machine |
| 02/22/2012 | CN102359437A Integrated system with wind power generation and compressed air energy storage and integration method thereof |
| 02/22/2012 | CN101131123B 涡轮发动机多功能进气口 Multifunctional turbine engine air intake |
| 02/21/2012 | US8118251 Mounting system for a gas turbine engine |
| 02/21/2012 | CA2412265C Thermal barrier coating |
| 02/16/2012 | WO2012021285A2 Adiabatic compressed air energy storage process |
| 02/16/2012 | US20120039708 Gas turbine engine |
| 02/16/2012 | US20120039707 Method of repairing knife edge seals |
| 02/16/2012 | US20120038173 Method, system and apparatus for providing water to a heat engine via a dammed water source |
| 02/16/2012 | US20120036864 Gas turbine engine and method for cooling the compressor of a gas turbine engine |
| 02/16/2012 | US20120036863 Method, apparatus and system for delivery of wide range of turbine fuels for combustion |
| 02/16/2012 | US20120036862 System and method for operating a gas turbine |
| 02/16/2012 | US20120036860 Gas turbine plant with exhaust gas recirculation and also method for operating such a plant |
| 02/16/2012 | US20120036859 Combustor transition piece with dilution sleeves and related method |
| 02/16/2012 | US20120036856 Dimpled/grooved face on a fuel injection nozzle body for flame stabilization and related method |
| 02/16/2012 | US20120036855 Burner |
| 02/16/2012 | US20120036829 System, Method and Apparatus for Lean Combustion with Plasma from an Electrical Arc |
| 02/16/2012 | US20120036827 Rotating inlet cowl for a turbine engine, comprising an eccentric forward end |
| 02/16/2012 | US20120036826 Engine and pod assembly for an aircraft, equipped with an anti-icing device |
| 02/16/2012 | US20120036825 Engine |
| 02/16/2012 | US20120036824 Reheat burner |
| 02/16/2012 | DE102011052589A1 Brennkammerübergangsstück mit Verdünnungshülsen und verwandte Verfahren Combustor transition piece with thinner shells and related methods |
| 02/16/2012 | DE102011052234A1 Wärmetauscherkissen für eine Gasturbine Heat exchanger for a gas turbine cushions |
| 02/16/2012 | DE102011009526A1 Belüftungssystem und -verfahren für Turbinen Ventilation system and method for turbines |
| 02/16/2012 | DE102010034276A1 Method for operating gas turbine, involves providing exhaust gas cleaning system with combined power generation process, where working medium is compressed in compression unit, and working medium is cooled in heat exchanger |
| 02/16/2012 | DE102010015404B4 Verfahren zur Reparatur einer Rotoranordnung einer Turbomaschine, Ringelement für eine Rotoranordnung einer Turbomaschine sowie Rotoranordnung für eine Turbomaschine A method of repairing a rotor arrangement of a turbomachine, the ring element for a rotor arrangement of a turbomachine, as well as rotor assembly for a turbomachine |
| 02/16/2012 | CA2807502A1 Adiabatic compressed air energy storage process |
| 02/15/2012 | EP2418367A1 Cooling assembly and method for a gas-turbine electric power generating plant and gas-turbine electric power generating plant comprising said cooling assembly |
| 02/15/2012 | EP2418354A1 Method for producing an internally cooled turbine blade and gas turbine with a turbine blade produced according to the method |
| 02/15/2012 | EP2417359A1 Air bleed having an inertial filter in the tandem rotor of a compressor |
| 02/15/2012 | EP1646775B1 Method for the operation of an air-breathing engine |
| 02/15/2012 | CN202144762U 具有双阀座和双阀口的调节阀 With dual seat and dual port regulating valve |
| 02/15/2012 | CN202144751U Gas and steam turbine system |
| 02/15/2012 | CN102356224A Burner assembly |
| 02/15/2012 | CN102356116A Co-polymer based polyimide articles and their uses in an aircraft |
| 02/14/2012 | US8113001 Tubular fuel injector for secondary fuel nozzle |
| 02/14/2012 | CA2462933C Flexible link system between a satellite carrier and the fixed support in a reduction gear |
| 02/09/2012 | WO2012016725A1 Multi-piece turbocharger casing |
| 02/09/2012 | US20120034081 Compressor blade root heating system |
| 02/09/2012 | US20120034068 Ventilation inlet |
| 02/09/2012 | US20120031501 Aviation engine inlet with tangential blowing for buzz saw noise control |
| 02/09/2012 | US20120031106 System and method for measuring temperature within a turbine system |
| 02/09/2012 | US20120031105 Pressure-actuated plug |
| 02/09/2012 | US20120031104 Turbine engine |
| 02/09/2012 | US20120031103 Combustor and the Method of Fuel Supply and Converting Fuel Nozzle for Advanced Humid Air Turbine |
| 02/09/2012 | US20120031102 Turbine combustor with fuel nozzles having inner and outer fuel circuits |
| 02/09/2012 | US20120031101 Gas turbine with flow separation and recirculation |
| 02/09/2012 | US20120031099 Combustor assembly for use in a turbine engine and methods of assembling same |
| 02/09/2012 | US20120031098 Fuel nozzle with central body cooling system |
| 02/09/2012 | US20120031068 Compressed air plenum for a gas turbine engine |
| 02/09/2012 | DE102011052235A1 Druckbetätigter Stopfen Pressure actuated plug |
| 02/09/2012 | DE102010033665A1 Mehrteiliges Turboladergehäuse Multipart turbocharger housing |
| 02/08/2012 | EP2415992A2 Ventilation Inlet |
| 02/08/2012 | EP2415991A2 Turbine engine |
| 02/08/2012 | EP2415974A2 Sealed rotator shaft for borescopic inspection |
| 02/08/2012 | EP2415971A2 A seal assembly |
| 02/08/2012 | EP2414655A1 Rotating inlet cowl for a turbine engine, including an eccentric front end |
| 02/08/2012 | CN202140642U 初始流量超低的液体流量调节阀 The initial flow of ultra-low liquid flow control valve |
| 02/08/2012 | CN202140177U 大可调比的气体燃料流量调节阀 Large adjustable ratio of gas fuel flow control valve |
| 02/08/2012 | CN102349101A Aircraft acoustic attenuation member and method for forming said member |
| 02/08/2012 | CN102348880A Turbine engine support arms |
| 02/08/2012 | CN102348600A Aircraft nacelle comprising a reinforced outer wall |
| 02/08/2012 | CN102345966A Reduced carbon dioxide emission system and method |
| 02/08/2012 | CN102345514A Anti-rotation feature for air turbine starter |
| 02/08/2012 | CN102345513A Turbine intercooler |
| 02/08/2012 | CN102345512A Protective cover |
| 02/07/2012 | US8109073 Hybrid propulsive engine including at least one independently rotatable compressor stator |
| 02/07/2012 | CA2490628C Method and system for active tip clearance control in turbines |
| 02/07/2012 | CA2448465C Fabricated repair of cast nozzle |
| 02/05/2012 | CA2748093A1 Turbine engine |
| 02/02/2012 | WO2012014401A1 Intermediate cooling device for gas turbine and gas turbine using same |
| 02/02/2012 | WO2012013889A1 Lateral turbojet improved in order to limit the deformation thereof |
| 02/02/2012 | WO2012012912A1 Reconfigurable heat transfer system for gas turbine inlet |
| 02/02/2012 | US20120029786 Aircraft engine control during icing of temperature probe |
| 02/02/2012 | US20120023968 Exhaust manifold flange connection |
| 02/02/2012 | US20120023967 Auxiliary power unit with hot section fire enclosure arrangement |
| 02/02/2012 | US20120023966 Power plant start-up method |
| 02/02/2012 | US20120023965 Combustion controller |