| 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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| 09/30/2010 | US20100242494 Casing arrangement |
| 09/30/2010 | US20100242493 Fuel Nozzle Spring Support |
| 09/30/2010 | US20100242492 Distributed engine control systems and gas turbine engines |
| 09/30/2010 | US20100242491 Systems and Methods for Controlling Compressor Extraction Cooling |
| 09/30/2010 | US20100242490 Additive delivery systems and methods |
| 09/30/2010 | US20100242489 Systems, Methods, and Apparatus for Modifying Power Output and Efficiency of a Combined Cycle Power Plant |
| 09/30/2010 | US20100242487 Thermally decoupled can-annular transition piece |
| 09/30/2010 | US20100242485 Combustor liner |
| 09/30/2010 | US20100242483 Combustor for gas turbine engine |
| 09/30/2010 | US20100242482 Method and system for reducing the level of emissions generated by a system |
| 09/30/2010 | US20100242432 Adjustable igniter mount |
| 09/30/2010 | US20100242431 Variable Actuation Pressure System for Independent Pressure Control |
| 09/30/2010 | US20100242429 Split flow regenerative power cycle |
| 09/30/2010 | DE102009013083A1 Turbine housing insulation material made of a composite material, which contains temperature-resistant hard foam and has a ceramic layer in the area of a contact surface of the turbine housing |
| 09/30/2010 | CA2752927A1 Variable actuation pressure system for independent pressure control |
| 09/30/2010 | CA2752426A1 Cmc turbine stator blade |
| 09/30/2010 | CA2752424A1 Cmc turbine stator blade |
| 09/30/2010 | CA2697103A1 Lamellar seal for a turbo machine |
| 09/29/2010 | EP2233728A2 Fuel-cooled heat exchanger with thermoelectric device compression |
| 09/29/2010 | EP2233727A2 Fuel-cooled flexible heat exchanger with thermoelectric device compression |
| 09/29/2010 | EP2233722A2 Split flow regenerative power cycle |
| 09/29/2010 | EP2233721A1 Gas turbine engine |
| 09/29/2010 | EP2233700A1 Self balancing face seals and gas turbine engine systems involving such seals |
| 09/29/2010 | EP2233693A1 Cooling structure of turbine blade |
| 09/29/2010 | CN1938549B Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement |
| 09/29/2010 | CN101846101A 进口空气加热和冷却系统 The inlet air heating and cooling system |
| 09/29/2010 | CN101845999A Novel gas turbine |
| 09/29/2010 | CN101845998A Compressor clearance control system using turbine exhaust |
| 09/29/2010 | CN101845997A Apparatus for turbine engine cooling air management |
| 09/29/2010 | CN101845996A Interstage seal for gas turbine and corresponding gas turbine |
| 09/29/2010 | CN101845995A Split flow regenerative power cycle |
| 09/29/2010 | CN101509425B Gas turbine generating set |
| 09/29/2010 | CN101413440B Minitype gas turbine electric generating set |
| 09/28/2010 | US7802760 Boundary layer control arrangement |
| 09/28/2010 | US7802757 Method and system for taxiing an aircraft |
| 09/28/2010 | US7802433 Adaptive inertial particle separators and methods of use |
| 09/28/2010 | US7802431 Combustor liner with reverse flow for gas turbine engine |
| 09/26/2010 | CA2697121A1 Intentionally mistuned integrally bladed rotor |
| 09/26/2010 | CA2696623A1 Active tip clearance control arrangement for gas turbine engine |
| 09/23/2010 | WO2010107802A1 Co-polymer based polyimide articles and their uses in an aircraft |
| 09/23/2010 | WO2010107015A1 Gas turbine |
| 09/23/2010 | WO2010106570A1 Improvement of a turbine for the expansion of gas/vapour |
| 09/23/2010 | WO2010106568A1 Turbine for the expansion of gas/vapour provided with axial thrust compensation on the drive shaft |
| 09/23/2010 | WO2010105891A2 Burner assembly |
| 09/23/2010 | US20100241331 Control of gas turbine engine |
| 09/23/2010 | US20100236257 Gas turbine combustor exit duct and hp vane interface |
| 09/23/2010 | US20100236252 Swirl generator, method for preventing flashback in a burner having at least one swirl generator and burner |
| 09/23/2010 | US20100236251 Temperature measuring device, gas turbine having a temperature measuring device and method for directly determining the temperature in a combustion chamber |
| 09/23/2010 | US20100236250 Combustion chamber brazed with ceramic inserts |
| 09/23/2010 | US20100236247 Method and apparatus for delivery of a fuel and combustion air mixture to a gas turbine engine |
| 09/23/2010 | US20100236245 Gas Turbine Combustion System |
| 09/23/2010 | US20100236216 Turbofan engine with variable area fan nozzle and low spool generator for emergency power generation and method for providing emergency power |
| 09/23/2010 | US20100236215 Heat transfer system and method for turbine engine using heat pipes |
| 09/23/2010 | US20100236213 Method and apparatus for operating gas turbine engines |
| 09/23/2010 | US20100236200 System for inertial particles separation |
| 09/23/2010 | DE102008020932B4 Turbolader mit einer variablen Turbinengeometrieeinrichtung Turbocharger with a variable turbine geometry means |
| 09/23/2010 | CA2755624A1 Improvement of a turbine for the expansion of gas/vapour |
| 09/23/2010 | CA2752047A1 Co-polymer based polyimide articles and their uses in an aircraft |
| 09/22/2010 | EP2230459A1 Combustor of gas turbine |
| 09/22/2010 | EP2229323A2 Locking system for air intake structure for turbojet engine nacelle |
| 09/22/2010 | CN101839176A Bearing-lubricating device of turbojet engine |
| 09/22/2010 | CN101839174A Turbomachine inlet heating system |
| 09/22/2010 | CN101839150A Method of using and reconstructing a film-cooling augmentation device for a turbine airfoil |
| 09/21/2010 | US7797948 Transition-to-turbine seal apparatus and transition-to-turbine seal junction of a gas turbine engine |
| 09/21/2010 | US7797947 Mounting assembly for securing an engine to an aircraft wing |
| 09/21/2010 | US7797946 Double U design for mid-turbine frame struts |
| 09/21/2010 | US7797809 Zero acoustic splice fan case liner |
| 09/21/2010 | CA2551932C Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system includingsuch an air guiding flap |
| 09/21/2010 | CA2472541C Methods and apparatus for supplying feed air to turbine combustors |
| 09/21/2010 | CA2433636C Installation for the generation of energy |
| 09/17/2010 | CA2696547A1 Split ring seal with spring element |
| 09/16/2010 | WO2010103303A2 Turbine engine support arms |
| 09/16/2010 | WO2010103302A1 Aircraft acoustic attenuation member and method for forming said member |
| 09/16/2010 | WO2010103054A1 Rotor element with a fluid passage and passage-blocking member, and turbine engine including the rotor element |
| 09/16/2010 | WO2010102995A1 Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train |
| 09/16/2010 | WO2009123302A3 Thermal insulation structure for structural member, and scroll structure |
| 09/16/2010 | US20100232947 Impingement cooling arrangement for a gas turbine engine |
| 09/16/2010 | US20100232938 Gas Turbine Having Seal Assembly with Coverplate and Seal |
| 09/16/2010 | US20100232932 Air inlet shroud structure |
| 09/16/2010 | US20100232929 Cooling arrangement for a turbine engine component |
| 09/16/2010 | US20100229570 Burner for a gas turbine and method for locally cooling a hot gases flow passing through a burner |
| 09/16/2010 | US20100229569 Engine Exhaust System |
| 09/16/2010 | US20100229567 Turbine engine arrangement |
| 09/16/2010 | US20100229566 Two-shaft gas turbine system |
| 09/16/2010 | US20100229563 Wall elements for gas turbine engine combustors |
| 09/16/2010 | US20100229562 Reduced exhaust emissions gas turbine engine combustor |
| 09/16/2010 | US20100229560 Small gas turbine engine with multiple burn zones |
| 09/16/2010 | US20100229559 Fuel injection systems in a turbomachine combustion chamber |
| 09/16/2010 | US20100229558 Methods and Apparatus for Providing A Sacrificial Shield For A Fuel Injector |
| 09/16/2010 | US20100229557 Gas turbine combustor |
| 09/16/2010 | US20100229556 Turbine fuel nozzle having heat control |
| 09/16/2010 | US20100229555 Fuel manifold with reduced losses |
| 09/16/2010 | US20100229525 Turbine combustion air system |
| 09/16/2010 | US20100229522 Plasma-Assisted E-Waste Conversion Techniques |
| 09/16/2010 | DE102009013150A1 Bauteil zum Einsatz in Heißgasströmungen Component for use in streams of hot gas |
| 09/16/2010 | DE102009012971A1 Loading device i.e. exhaust gas turbocharger, for internal combustion engine, has spiral housing arranged coaxial to axis and comprising axial housing outlet connected to compressor inlet and housing inlet oriented transverse to axis |
| 09/16/2010 | DE102009012945A1 Verfahren zur Herstellung einer abrasiven Beschichtung und Bauteil für eine Turbomaschine A process for producing an abrasive coating and the component for a turbomachine |
| 09/16/2010 | DE102009001321A1 Supercharged internal combustion engine has intake line for supplying internal combustion engine with combustion air and compressor arranged in intake line |
| 09/16/2010 | CA2754782A1 Aircraft acoustic attenuation member and method for forming said member |
| 09/16/2010 | CA2754703A1 Turbine engine support arms |