| 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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| 08/25/2011 | US20110203250 Combustion device for a gas turbine |
| 08/25/2011 | US20110203249 Turbine starter lubricant cooling |
| 08/25/2011 | DE102011000788A1 Brennkammerflammrohr für eine Turbinenmaschine The combustor liner for a turbine engine |
| 08/25/2011 | DE102011000586A1 Verfahren und Systeme in Zusammenhang mit der Brennstoffzufuhr in Gasturbinen Methods and systems in connection with the supply of fuel in gas turbines |
| 08/25/2011 | DE102010009289A1 Lubricating oil circuit for two exhaust gas turbochargers of internal combustion engine, has bypass channels for bearing housings, where former bypass channel leads lubricating oil that stands under pressure |
| 08/25/2011 | DE102010009274A1 Gas turbine concept for power generation for block-type thermal power stations and electric vehicles, includes concentric arrangement of combustion chamber to rotor axis |
| 08/25/2011 | DE102010009051A1 Fuel supply device for use in gas turbine combustion chamber system for technical combustion chamber system for flame less combustion, has main nozzle with fuel supply and another nozzle for supplying fuel |
| 08/24/2011 | EP2359962A2 Method and apparatus for production of a cast component |
| 08/24/2011 | EP2359959A1 Green ceramic casting mold system and refractory casting mold obtainable thereof |
| 08/24/2011 | EP2359958A1 Method for production of a ceramic casting mold system |
| 08/24/2011 | CN201943820U 可实现纯氧洁净燃烧的燃气轮机系统 Can achieve clean combustion of pure oxygen gas turbine system |
| 08/24/2011 | CN1676976B Seal assembly |
| 08/24/2011 | CN102164821A Device for connecting an air inlet with an aircraft nacelle actuator assembly |
| 08/23/2011 | US8001791 Turbine engine frame having an actuated equilibrating case |
| 08/23/2011 | US8001790 Gas turbine |
| 08/23/2011 | US8001789 Utilizing inlet bleed heat to improve mixing and engine turndown |
| 08/23/2011 | US8001762 Method and device to increase thrust and efficiency of jet engine |
| 08/23/2011 | CA2731914A1 Epicyclic gearbox |
| 08/23/2011 | CA2495624C Turbojet having a large bypass ratio |
| 08/23/2011 | CA2473276C Method for inspecting a titanium-based component |
| 08/22/2011 | CA2732330A1 Turbine starter lubricant cooling |
| 08/18/2011 | WO2011100663A2 Coil arrangements for air intake system for gas turbine and methods |
| 08/18/2011 | WO2011099383A1 Aircraft |
| 08/18/2011 | WO2011098737A1 Gas-guiding pipe comprising a noise-attenuating covering with variable porosity |
| 08/18/2011 | WO2011098729A1 Device for ejecting gas from a gas turbine engine and gas turbine engine |
| 08/18/2011 | WO2011098728A1 Link between the exhaust casing and a structural ring of the fan duct of a jet engine |
| 08/18/2011 | US20110198155 Method and system for lubricating a turbine engine |
| 08/18/2011 | US20110197595 Engine assembly for an aircraft comprising attachments for engines offset below on the fan frame |
| 08/18/2011 | US20110197594 Method of Controlling a Combustor for a Gas Turbine |
| 08/18/2011 | US20110197592 Coil arrangement for air intake system for gas turbine and methods |
| 08/18/2011 | US20110197589 Fuel Injector Nozzle |
| 08/18/2011 | US20110197588 Fuel Injector Nozzle |
| 08/18/2011 | US20110197587 Multi-tube premixing injector |
| 08/18/2011 | US20110197566 Systems and methods of operating a catalytic reforming assembly for use with a gas turbine engine system |
| 08/18/2011 | DE102011000480A1 Systeme und Verfahren zum Betreiben einer katalytischen Reformierungsbaugruppe zur Verwendung mit einem Gasturbinensystem Systems and methods for operating a catalytic reforming assembly for use with a gas turbine system |
| 08/18/2011 | DE102010060990A1 Multirohr-Vormischinjektor Multi-tube Vormischinjektor |
| 08/18/2011 | DE102010016580A1 Turboladeraufbau für eine Brennkraftmaschine Turbocharger assembly for an internal combustion engine |
| 08/18/2011 | DE102010007724A1 Schraubenlose Zwischenstufendichtung einer Gasturbine Screwless interstage seal a gas turbine |
| 08/18/2011 | DE102010006018A1 Aufladeeinrichtung zum Verdichten eines Mediums sowie Antriebsstrang für einen Kraftwagen mit einer solchen Aufladeeinrichtung Charging means for compressing a fluid and drive train for a motor vehicle with such a charging |
| 08/18/2011 | DE102009053238A1 Turboladergehäuse mit einer Dichtungseinrichtung Turbocharger housing with a sealing device |
| 08/18/2011 | DE102009009600A1 Bird guard for jet engines operated aircraft, has pointed-angular designed header derived by its angular function hitting objects, bird-swarms, geese, without hindering air traffic, laterally without loss |
| 08/18/2011 | CA2789555A1 Gas-guiding pipe comprising a noise-attenuating covering with variable porosity |
| 08/18/2011 | CA2789258A1 Device for ejecting gas from a gas turbine engine and gas turbine engine |
| 08/18/2011 | CA2779422A1 Aircraft |
| 08/17/2011 | EP2356329A1 Fuel delivery and control system including a positive displacement actuation pump with a variable pressure regulator supplementing a fixed displacement main fuel pump |
| 08/17/2011 | EP1152848B1 Method and apparatus for production of a cast component |
| 08/17/2011 | CN201934151U 一种整环导向器装置 An integrin-guiding device |
| 08/17/2011 | CN102159795A Method and system for lubricating turbine engine |
| 08/17/2011 | CN102155300A Vane type silencers in elbow for gas turbine |
| 08/17/2011 | CN102155299A Combination system of stirling engine and combustion gas turbine utilizing liquefied natural gas |
| 08/17/2011 | CN102155297A Secondary combustion fuel supply systems |
| 08/16/2011 | US8000687 Wireless terminal location using apparatus and methods employing carrier diversity |
| 08/16/2011 | US7997085 Gas turbine engine assembly and method of assembling same |
| 08/16/2011 | US7997083 Method and system for detection of gas turbine combustion blowouts utilizing fuel normalized power response |
| 08/16/2011 | US7997082 Turbine engine arrangement |
| 08/16/2011 | US7997057 Gas turbine engine with an air cooled bearing |
| 08/12/2011 | CA2788929A1 Link between the exhaust casing and a structural ring of the fan duct of a jet engine |
| 08/11/2011 | WO2011096197A1 Fuel supply device for gas turbine engine |
| 08/11/2011 | WO2011073565A3 Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection means |
| 08/11/2011 | WO2011051598A3 Turbine engine starter/generator, and method for the control thereof |
| 08/11/2011 | WO2011000548A3 Method for operating a power plant using a gas turbine system |
| 08/11/2011 | US20110192171 Transition support system for combustion transition ducts for turbine engines |
| 08/11/2011 | US20110192169 Gas turbine engine fuel control system |
| 08/11/2011 | DE102010064061A1 Turbo compressor for fuel cell drive of internal combustion engine of hybrid drive for motor vehicle, has drive unit and two compressor wheels driven by drive unit |
| 08/11/2011 | DE102010007567A1 Supersonic kernel diffuser for use in e.g. rocket engine test stand, has elongated central body partly held in passage by clamping elements loaded on traction, where central body reduces surface of passage |
| 08/10/2011 | EP2354496A2 Brake mechanism for air turbine starter |
| 08/10/2011 | EP2354495A2 Integrated exhaust gas cooling system and corresponding method |
| 08/10/2011 | EP2354494A2 Turbomachine Nacelle And Anti-Icing System And Method Therefor |
| 08/10/2011 | EP2354493A2 Ejector/mixer nozzle for noise reduction |
| 08/10/2011 | EP2354492A2 Ejector in an Overboard Bleed scheme for a gas turbine |
| 08/10/2011 | EP2354473A2 Intermediate casing for a gas-turbine engine |
| 08/10/2011 | EP2354471A2 Sealing and purging arrangement for a main bearing region |
| 08/10/2011 | EP2354469A2 Turbomachine Nacelle And Anti-Icing System And Method Therefor |
| 08/10/2011 | EP2354449A2 Method and apparatus for double flow turbine first stage cooling |
| 08/10/2011 | EP2352914A1 Systems and methods for thermal management in a gas turbine powerplant |
| 08/10/2011 | EP1706620B1 Gas turbine engine architecture |
| 08/10/2011 | CN201925028U 燃气轮机进气系统防冰防霜装置 Gas turbine intake system anti-icing anti-frost device |
| 08/10/2011 | CN201925027U 一种应用化工驰放气发电的系统 An application of chemical Chi deflated system power |
| 08/10/2011 | CN102146844A Zero cooling air consumption super-strength cooling device for aircraft engine turbine blade |
| 08/09/2011 | CA2478202C Methods and apparatus to reduce turbine engine nozzle basesheet stresses |
| 08/09/2011 | CA2468242C Control method of gas turbine engine and control system of the same |
| 08/09/2011 | CA2432256C A combustion chamber sealing ring, and a combustion chamber including such a ring |
| 08/04/2011 | WO2011092917A1 Split ring cooling structure and gas turbine |
| 08/04/2011 | WO2011091591A1 Anti-impaction net of aero plane engine |
| 08/04/2011 | WO2011019422A3 Method of operating a heated guide vane assembly |
| 08/04/2011 | US20110189009 Mounting apparatus for low-ductility turbine shroud |
| 08/04/2011 | US20110188995 Axial load damping system for rotor shaft |
| 08/04/2011 | US20110185746 Gas turbine combustion device |
| 08/04/2011 | US20110185745 Emergency power engine restart system |
| 08/04/2011 | US20110185744 Method and apparatus for combined cycle power plant startup |
| 08/04/2011 | US20110185743 Methods For Operating Gas Turbine Engines |
| 08/04/2011 | US20110185741 Injection nozzle and method for operating an injection nozzle |
| 08/04/2011 | US20110185740 Combustor liner segment seal member |
| 08/04/2011 | US20110185739 Gas turbine combustors with dual walled liners |
| 08/04/2011 | US20110185738 Gas turbine engine component construction |
| 08/04/2011 | US20110185735 Gas turbine combustor with staged combustion |
| 08/04/2011 | US20110185731 Oil cooler |
| 08/04/2011 | US20110185703 Gas Turbine Combustor |
| 08/04/2011 | US20110185700 Jet engine bird diverters |
| 08/04/2011 | US20110185699 Gas turbine engine steam injection manifold |