| 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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| 04/14/2011 | US20110083439 Staged Multi-Tube Premixing Injector |
| 04/14/2011 | DE102010037863A1 System und Verfahren zur Verteilung von Brennstoff in einer Turbomaschine System and method for distribution of fuel into a turbomachine |
| 04/14/2011 | DE102010037811A1 Vorrichtung und Verfahren zum Kühlen von Düsen Apparatus and method for cooling nozzles |
| 04/14/2011 | DE102010037692A1 Geformte Wabendichtung für eine Turbomaschine Formed honeycomb seal for a turbomachine |
| 04/14/2011 | CA2776314A1 Circuit for supplying fuel to an aircraft engine |
| 04/14/2011 | CA2775829A1 Circuit for supplying fuel to an aircraft engine |
| 04/13/2011 | EP2309109A1 Gas turbine and method of operating gas turbine |
| 04/13/2011 | EP2309108A1 Gas turbine |
| 04/13/2011 | EP2307738A2 Compressor cover for turbine engine having axial abutment |
| 04/13/2011 | EP1390606B2 Device for cooling coolant in a gas turbine and gas and steam turbine with said device |
| 04/13/2011 | CN201794667U Air suction pulse detonation engine inlet |
| 04/13/2011 | CN102016280A Exhaust washed structure and associated composite structure and method of fabrication |
| 04/13/2011 | CN102016265A Casing comprising a peripheral shroud for a turbomachine rotor |
| 04/13/2011 | CN102016235A Gas turbine blade and gas turbine equipped with the same |
| 04/13/2011 | CN102016232A Rotor for the compressor of a turbine engine comprising a centripetal air-collecting means |
| 04/13/2011 | CN102015450A Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle |
| 04/13/2011 | CN102011651A Impingement cooled transition piece aft frame |
| 04/13/2011 | CN102011650A Multipoint frequent-explosion hydrogen energy steam turbine |
| 04/13/2011 | CN101566104B Method and device for zero emission of carbon dioxide by utilizing liquid hydrogen condensation |
| 04/12/2011 | US7921654 Cooled turbine stator vane |
| 04/12/2011 | US7921651 Operation of dual gas turbine fuel system |
| 04/09/2011 | CA2715600A1 Oil tube with integrated heat shield |
| 04/08/2011 | CA2681906A1 Plenum air preheat for cold startup of liquid-fueled pulse detonation engines |
| 04/07/2011 | WO2011041049A2 Internally nested variable-area fuel nozzle |
| 04/07/2011 | WO2011039879A1 Matrix resin composition for fiber-reinforced plastics, and fiber-reinforced plastic structures |
| 04/07/2011 | WO2011039422A1 Method and device for gas cleaning |
| 04/07/2011 | WO2011012985A3 Method and assembly for supplying fuel to a combustion chamber of a gas turbine plant |
| 04/07/2011 | US20110081229 Method for attaching a connector to deposited material |
| 04/07/2011 | US20110079667 Fuel nozzle and method of repair |
| 04/07/2011 | US20110079021 Apparatus and method for removing heat from a gas turbine |
| 04/07/2011 | US20110079020 Air metering device for gas turbine engine |
| 04/07/2011 | US20110079019 Cooling air system for mid turbine frame |
| 04/07/2011 | US20110079018 Bleed air transfer tube |
| 04/07/2011 | US20110079017 Methods and Systems Involving Carbon Sequestration and Engines |
| 04/07/2011 | US20110079016 Compact aircraft combustor |
| 04/07/2011 | US20110079015 Apparatus and method of operating a gas turbine engine |
| 04/07/2011 | US20110079013 Fuel injector and aerodynamic flow device |
| 04/07/2011 | DE102010037411A1 Brennkammer-zu-Brennkammer-Modenentkopplung mittels Brennstoffaufteilungen auf Brennkammerrohrebene Combustion chamber-to-chamber mode decoupling means fuel splits to combustor level |
| 04/07/2011 | DE102005054442B4 Brennkammer für eine Gasturbine Combustion chamber for a gas turbine |
| 04/07/2011 | CA2776136A1 Internally nested variable-area fuel nozzle |
| 04/07/2011 | CA2686713A1 Fuel nozzle and method of repair |
| 04/06/2011 | EP2306091A2 Fuel premixing module for gas turbine engine combustor |
| 04/06/2011 | EP2305986A2 Methods and systems for mitigating distortion of gas turbine shaft |
| 04/06/2011 | EP2305985A2 Containment casing for an aero engine |
| 04/06/2011 | EP2305984A2 A method of securing a liner panel to the casing of a turbomachine |
| 04/06/2011 | EP2305982A1 Cooling and tapping system for a gas turbine engine and corresponding operation method |
| 04/06/2011 | EP2305958A2 An apparatus and method of operating a gas turbine engine |
| 04/06/2011 | EP2305415A1 Welding material for ni-based alloy |
| 04/06/2011 | EP2304205A1 Method for rinsing a fuel system of a gas turbine and associated fuel system |
| 04/06/2011 | EP2304204A1 Method of depositing a coating for improving laminar flow |
| 04/06/2011 | EP1689992B1 Method and apparatus for actuating fuel trim valves in a gas turbine |
| 04/06/2011 | CN1952435B Gas turbine engine assembly and methods of assembling same |
| 04/06/2011 | CN102007282A Propulsion unit for an aircraft and air intake structure for such a unit |
| 04/06/2011 | CN102003302A Air intake cone of air-breathing pulse detonation engine |
| 04/06/2011 | CN102003286A Acoustically stiffened gas turbine combustor supply |
| 04/06/2011 | CN102003285A Exhaust gas recirculation for a turbomachine |
| 04/06/2011 | CN102003284A Hydrogen-blended gas fuel engine |
| 04/06/2011 | CN102003220A Inter-stage seal ring |
| 04/06/2011 | CN101624945B Jet pressing burning splitting ring curled turbine engine |
| 04/06/2011 | CN101091400B Wireless terminal location using apparatus and methods employing carrier diversity |
| 04/05/2011 | US7918433 Transition piece mounting bracket and related method |
| 04/01/2011 | CA2715604A1 Method for centering engine structures |
| 04/01/2011 | CA2715598A1 Air metering device for gas turbine engine |
| 04/01/2011 | CA2715594A1 Interturbine vane with multiple air chambers |
| 04/01/2011 | CA2715591A1 Gas turbine engine thermal expansion joint |
| 04/01/2011 | CA2715271A1 Gas turbine engine balancing |
| 04/01/2011 | CA2715228A1 Cooling air system for mid turbine frame |
| 04/01/2011 | CA2715227A1 Sealing for vane segments |
| 04/01/2011 | CA2714826A1 Bleed air transfer tube |
| 03/31/2011 | WO2011038216A1 A convertible fan engine comprising a two block compressor |
| 03/31/2011 | WO2011038213A1 Convertible fan engine |
| 03/31/2011 | WO2011036363A1 Fuel flowmeter having an improved control device |
| 03/31/2011 | WO2011036205A1 Fuel line system, method for operating a gas turbine, and method for purging the fuel line system of a gas turbine |
| 03/31/2011 | WO2011007236A3 Gas turbine exhaust gas cooling system |
| 03/31/2011 | US20110072832 Ventilation for a turbine wheel in a turbine engine |
| 03/31/2011 | US20110072831 Sealing apparatus with multistage brush seal |
| 03/31/2011 | US20110072830 Combustor interface sealing arrangement |
| 03/31/2011 | US20110072827 Cooling system for a gas turbine and corresponding operation method |
| 03/31/2011 | US20110072826 Can to can modal decoupling using can-level fuel splits |
| 03/31/2011 | US20110072825 Air blast fuel injector |
| 03/31/2011 | US20110072824 Appartus and method for a gas turbine nozzle |
| 03/31/2011 | US20110072823 Gas turbine engine fuel injector |
| 03/31/2011 | US20110072822 Hose arrangement for a gas turbine engine |
| 03/31/2011 | DE112009001129T5 Verfahren und Vorrichtung zur Brennstoffsteuerung in einer Gasturbine Method and apparatus for controlling fuel in a gas turbine |
| 03/31/2011 | DE102009043117A1 Sealing arrangement for sealing tubular element of exhaust gas manifold and tubular element of exhaust gas turbo charger for guiding exhaust gas in internal combustion engine in car, has sealing contact formed in sealing area |
| 03/31/2011 | DE102009042857A1 Gasturbine mit Deckband-Labyrinthdichtung Gas turbine shroud labyrinth seal |
| 03/31/2011 | DE102009023891A1 Magnet-supported rotor shaft for exhaust-gas turbocharger that is used for petrol or diesel engines, has heat pipe provided in interior of rod-shaped shaft body, where longitudinal axis of pipe coincides with longitudinal axis of body |
| 03/31/2011 | CA2775116A1 A convertible fan engine comprising a two block compressor |
| 03/31/2011 | CA2775114A1 Convertible fan engine |
| 03/31/2011 | CA2774320A1 Fuel flowmeter having an improved control device |
| 03/31/2011 | CA2739208A1 Sealing between a combustion chamber and a turbine distributor in a turbine engine |
| 03/30/2011 | EP2300701A2 Power transmission among shafts in a turbine engine |
| 03/30/2011 | CN201778842U Connecting structure for expansion ring seal retainer |
| 03/30/2011 | CN101994573A Distributed type renewable gas energy generation method |
| 03/30/2011 | CN101994572A System and method for injection of cooling air into exhaust gas flow |
| 03/30/2011 | CN101994571A System for conditioning the airflow entering turbomachine |
| 03/30/2011 | CN101994570A Embedded air inlet based on vortex excretion and aircraft using embedded air inlet |
| 03/29/2011 | US7913936 Device for sound attenuation in a flow duct |
| 03/29/2011 | US7913815 Automated seal oil by-pass system for hydrogen cooled generators |
| 03/29/2011 | CA2658066C Filtration device for aircraft with filter rotation stop |