| 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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| 12/31/2009 | US20090321178 Method and system for damped acoustic panels |
| 12/31/2009 | US20090320690 Suction filter, turbo compressor and method for compact assembling of the same |
| 12/31/2009 | US20090320498 Cooling air bleed device in a turbomachine |
| 12/31/2009 | US20090320497 Cooling air bleed device in a turbine engine |
| 12/31/2009 | US20090320491 Dual clutch arrangement |
| 12/31/2009 | US20090320484 Methods and systems to facilitate reducing flashback/flame holding in combustion systems |
| 12/31/2009 | US20090320482 Fuel control arrangement |
| 12/31/2009 | US20090320481 Fuel control arrangement |
| 12/31/2009 | US20090320480 Fuel control arrangement |
| 12/31/2009 | US20090320479 Nested channel ducts for nozzle construction and the like |
| 12/31/2009 | US20090320441 Inflatable seal assembly between an engine inlet and a vehicle |
| 12/31/2009 | US20090320440 Wet compression systems in turbine engines |
| 12/31/2009 | US20090320283 Suction filter, turbo compressor, and method for compact assembling of the same |
| 12/31/2009 | DE102009037956A1 Turbine exhaust case for low-pressure turbine of aircraft engine, has sound-absorbing element i.e. absorber box, in contact with gas stream passing through case, and circular flow channel formed between inner wall and external wall |
| 12/31/2009 | DE102009021516A1 Turboladersystem für einen Verbrennungsmotor mit einem internen isolierten Turbolader-Ölrückflussdurchlass The turbocharger system for an internal combustion engine with a turbocharger internal isolated oil return passage |
| 12/31/2009 | DE102009003244A1 Aufladeeinrichtung Charging |
| 12/31/2009 | DE10117127B4 Verbundaufbau zwischen metallischen und nichtmetallischen Materialien Composite structure between metallic and non-metallic materials |
| 12/30/2009 | WO2009115674A3 Air intake for aircraft engine nacelle, and nacelle equipped with such air intake |
| 12/30/2009 | WO2009086190A3 Gas turbine systems and methods employing a vaporizable liquid delivery device |
| 12/30/2009 | EP2138688A2 A fuel control arrangement |
| 12/30/2009 | EP2138217A1 Wash filter with wash velocity control cone |
| 12/30/2009 | CN100575789C Method for controlling calorific value of gas and apparatus for controlling calorific value of gas |
| 12/30/2009 | CN100575682C Turbogenerator |
| 12/29/2009 | US7637110 Methods and apparatuses for assembling a gas turbine engine |
| 12/29/2009 | US7637094 Cooling apparatus for a gas turbine engine igniter lead |
| 12/29/2009 | US7637093 Humid air turbine cycle with carbon dioxide recovery |
| 12/29/2009 | CA2399667C Gas turbine combustor apparatus |
| 12/29/2009 | CA2361103C Stator ring ventilation assembly |
| 12/24/2009 | US20090317286 High-temperature member for use in gas turbine |
| 12/24/2009 | US20090317244 Gas turbine engine with improved thermal isolation |
| 12/24/2009 | US20090317243 High reflectivity infrared coating applications for use in hirss applications |
| 12/24/2009 | US20090317029 Bearing system |
| 12/24/2009 | US20090314227 Method of operating a gas engine plant and fuel feeding system for a gas engine |
| 12/24/2009 | US20090314006 Gas turbine engine and integrated heat exchange system |
| 12/24/2009 | US20090314004 Turboprop engine with an apparatus for the generation of a cooling airflow |
| 12/24/2009 | US20090314003 Gas turbine with at least one multi-stage compressor unit including several compressor modules |
| 12/24/2009 | US20090314002 Bi-modal turbine assembly and starter / drive turbine system employing the same |
| 12/24/2009 | US20090314000 Coanda pilot nozzle for low emission combustors |
| 12/24/2009 | US20090313999 Method and apparatus for controlling fuel in a gas turbine engine |
| 12/24/2009 | US20090313968 Hypersonic Inlet Systems and Methods |
| 12/24/2009 | DE102008028987A1 Turboproptriebwerk mit einer Vorrichtung zum Erzeugen eines Kühlluftstroms Turboprop engine with a device for generating a cooling air flow |
| 12/24/2009 | DE102008028025A1 Hitzeschildanordnung Heat shield assembly |
| 12/24/2009 | DE102008002498A1 Verfahren zur Herstellung von Filmkühlungskanälen in einer Heissgasge-häusewand einer Gasturbine sowie Heissgasgehäuse einer Gasturbine A process for the production of film cooling passages in a Heissgasge-housing wall of a gas turbine, as well as hot gas casing of a gas turbine |
| 12/23/2009 | WO2009154517A1 A gas turbine component and a gas turbine engine comprising the component |
| 12/23/2009 | WO2009154245A1 Ni-BASE ALLOY-HIGH CHROMIUM STEEL STRUCTURE AND PROCESS FOR PRODUCING THE NI-BASE ALLOY-HIGH CHROMIUM STEEL STRUCTURE |
| 12/23/2009 | WO2009125120A3 Device and method for balancing pressure in a turbojet bearing housing |
| 12/23/2009 | WO2009120778A3 Subsonic and stationary ramjet engines |
| 12/23/2009 | EP2136052A1 Turboprop engine comprising a device for creating a cooling air flow |
| 12/23/2009 | EP2136051A2 Power augmentation system for a gas turbine |
| 12/23/2009 | EP2136050A2 Gas turbine plant |
| 12/23/2009 | EP2135718A2 Method for producing film cooling channels in a casing wall of a gas turbine and casing of a gas turbine |
| 12/23/2009 | EP2134928A1 Assembly device for assembling and disassembling a rotor of a turbomachine consisting of rotor disks |
| 12/23/2009 | EP2134927A1 Securing device for securing a rotor of a turbomachine counter to tilting, said rotor being arranged perpendicular to a horizontal plane and method for the alignment thereof |
| 12/23/2009 | EP2134604A1 Device for de-icing the air intake of a gas turbine |
| 12/23/2009 | EP1928743B1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
| 12/23/2009 | CN201367945Y Jet engine protecting cover |
| 12/23/2009 | CN101611218A Method for demounting blade ring and member for demounting blade ring |
| 12/23/2009 | CN101608576A Skid mounted equipment structure for power augmentation system |
| 12/23/2009 | CN100572758C Apparatus for fabricating a turbine nozzle assembly |
| 12/23/2009 | CA2726905A1 Compressor cover for turbine engine having axial abutment |
| 12/22/2009 | US7634916 Stiffener for low pressure compressor for an aircraft engine |
| 12/22/2009 | US7634901 Isotropic recycling engine |
| 12/22/2009 | CA2492914C Improved fuel delivery system |
| 12/22/2009 | CA2330218C Method of removing a thermal barrier coating |
| 12/20/2009 | CA2665329A1 Skid architecture for a power augmentation system |
| 12/17/2009 | WO2009151701A2 Gas turbine engine systems involving fairings with locating data |
| 12/17/2009 | WO2009151073A1 Lean fuel sucking gas turbine system |
| 12/17/2009 | WO2009150013A1 Multi-way valve of a fuel system of a gas turbine |
| 12/17/2009 | WO2009149990A1 Method for rinsing a fuel system of a gas turbine and associated fuel system |
| 12/17/2009 | WO2009149989A1 Check valve having a moveable valve body |
| 12/17/2009 | US20090311090 Windward cooled turbine nozzle |
| 12/17/2009 | US20090309364 Power generation system for an aircraft using a fuel cell |
| 12/17/2009 | US20090308273 Active vortex control system (avocs) method for isolation of sensitive components from external environments |
| 12/17/2009 | US20090308078 Engine mounting apparatus |
| 12/17/2009 | DE102009008434A1 Turbolader Turbocharger |
| 12/17/2009 | DE102009003857A1 Dualgas-Turbinenbrennstoffsystem mit unabhängigen Verteilern Dual gas turbine fuel system with independent distributors |
| 12/16/2009 | EP2133537A2 Bi-modal air turbine starter assembly |
| 12/16/2009 | EP2133515A1 Power supply equipment for natural gas liquefaction plant |
| 12/16/2009 | EP2132446A1 Air intake for a gas turbine compressor |
| 12/16/2009 | EP1587602B1 Configuration and process for carbonyl removal |
| 12/15/2009 | US7632363 Method for refurbishing a service-degraded component of a gas turbine |
| 12/15/2009 | US7632362 Property recovering method |
| 12/15/2009 | US7631501 Profiled sealing body with spring section |
| 12/15/2009 | US7631483 Method and system for reduction of jet engine noise |
| 12/15/2009 | US7631481 Cooled duct for gas turbine engine |
| 12/15/2009 | CA2445770C Arrangement for mounting two coaxial shaftlines |
| 12/10/2009 | WO2009147307A1 Casing comprising a peripheral shroud for a turbomachine rotor |
| 12/10/2009 | US20090304495 Device for supplying ventilation air to the low pressure blades of a gas turbine engine |
| 12/10/2009 | US20090302152 Engine arrangement |
| 12/10/2009 | US20090301101 Heat exchanger, propulsion unit and aircraft provided therewith |
| 12/10/2009 | US20090301100 Power Generation |
| 12/10/2009 | US20090301099 Power Generation |
| 12/10/2009 | US20090301096 Gas Turbine Engine and Method for Reducing Turbine Engine Combustor Gaseous Emission |
| 12/10/2009 | US20090301095 Passive boundary layer bleed system for nacelle inlet airflow control |
| 12/10/2009 | US20090301092 Burners for a gas turbine engine |
| 12/10/2009 | US20090301091 Compressor-less micro gas turbine power generating system |
| 12/10/2009 | US20090301085 Turbocharger for an internal combustion engine |
| 12/10/2009 | US20090301055 Gas Turbine Engine Systems and Methods Involving Vibration Monitoring |
| 12/10/2009 | US20090301053 Gas Turbine and Method of Operating a Gas Turbine |
| 12/10/2009 | DE102008027021A1 Sealing arrangement for sealing gap between two components, particularly rotor and stator of turbo-engine, has brush seal with bristles, which is arranged partially in receiving space of housing |