| 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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| 01/21/2010 | US20100011772 Fuel injection system |
| 01/21/2010 | US20100011771 Coanda injection system for axially staged low emission combustors |
| 01/21/2010 | US20100011769 Forward-section resonator for high frequency dynamic damping |
| 01/21/2010 | US20100011739 Apparatus and method for drawing off and recirculating a cooling stream |
| 01/21/2010 | DE102008033860A1 Triebwerk bestehend aus Kerntriebwerk und nachgeschaltetem Vortriebserzeuger Engine consisting of core engine and propulsion downstream producers |
| 01/21/2010 | DE102008033814A1 Bearing section for turbo charger, has bearing device with bush, which is arranged in bearing section area of bearing section |
| 01/21/2010 | DE102008031980A1 Verfahren zum Betrieb einer Maschine mit einer Wellendichtung Method for operating a machine having a shaft seal |
| 01/21/2010 | CA2728701A1 A structural frame for a turbomachine |
| 01/21/2010 | CA2672502A1 Fuel nozzle centerbody and method of assembling the same |
| 01/20/2010 | EP2146075A2 Heat pipe for removing thermal energy from exhaust gas |
| 01/20/2010 | EP2146058A1 Eductor system for a gas turbine engine |
| 01/20/2010 | EP2145080A2 Assistance device for transient acceleration and deceleration phases |
| 01/20/2010 | EP1450984B1 A method for manufacturing a stator or rotor component |
| 01/20/2010 | CN101631941A Coating for acoustic treatment having a hot air icing processing function |
| 01/20/2010 | CN101629521A Anti-carbon deposition method of fuel nozzle component by using rare earth oxide (REO) coat |
| 01/20/2010 | CN101629520A Combustor transition piece aft end cooling and related method |
| 01/20/2010 | CN101629519A Turbomachine including an adaptable intake system and method of controlling airflow to a turbomachine |
| 01/20/2010 | CN101629518A Turbomachine filter system having a drain with one-way valve |
| 01/20/2010 | CN101629517A Jet propulsion method and jet engine |
| 01/20/2010 | CN100582441C Structural cover for gas turbine engine bolted flanges |
| 01/19/2010 | US7648330 Noise control |
| 01/19/2010 | US7647779 Compliant metal support for ceramic combustor liner in a gas turbine engine |
| 01/19/2010 | US7647778 Engine arrangements and control |
| 01/19/2010 | US7647777 Skid architecture for a power augmentation system |
| 01/19/2010 | US7647761 System for deicing the nose cone of an aircraft turbojet with oil |
| 01/16/2010 | CA2671463A1 Turbomachine filter system having a drain with one-way valve |
| 01/16/2010 | CA2665727A1 Electric motor driven lubrication pump control system and method for turbomachine windmill operation |
| 01/14/2010 | WO2010006151A2 Power transmission among shafts in a turbine engine |
| 01/14/2010 | US20100005776 Fuel supply system for a gas-turbine engine |
| 01/14/2010 | DE19538553B4 Rotorlagerung eines Abgasturboladers Rotor bearing arrangement of an exhaust turbocharger |
| 01/14/2010 | DE102009026056A1 Brennkammerstruktur Combustion chamber structure |
| 01/14/2010 | DE102009026052A1 Kühleinrichtung für das hintere Ende eines Brennkammerübergangstücks und zugehöriges Verfahren Cooling device for the rear end of a combustor transition piece and associated method |
| 01/14/2010 | DE102009025914A1 Turbinensystem mit Abgasrückführung und Zwischenüberhitzung Turbine system with exhaust gas recirculation and reheating |
| 01/14/2010 | DE102009025796A1 Systeme und Verfahren zur Modifizierung einer modalen Schwingung in Zusammenhang mit einer Turbine Systems and methods for modifying a modal vibration in the context of a turbine |
| 01/14/2010 | DE102008032808A1 Abgasturbolader für ein Kraftfahrzeug Exhaust gas turbocharger for a motor vehicle |
| 01/14/2010 | DE102008032565A1 Brennstoffzufuhrsystem für ein Gasturbinentriebwerk A fuel delivery system for a gas turbine engine |
| 01/14/2010 | DE102008031986A1 Gas turbine for aircraft engine, has compressor modules comprising compressor stage with rotor and stator, where direction of rotation of compressor modules is formed in opposite directions alternatively |
| 01/14/2010 | DE102008031984A1 Gas turbine for aircraft, has compressor unit provided with compressor modules, which are swivelably supported on drive shaft and are separable from shaft in propulsive manner, where each compressor module is provided with sensor units |
| 01/14/2010 | DE102008031932A1 Gasturbine mit zumindest einer mehrstufigen, mehrere Verdichtermodule umfassenden Verdichtereinheit Gas turbine with at least one multi-level, comprehensive multiple compressor modules compressor unit |
| 01/14/2010 | CA2671465A1 Turbomachine including an adaptable intake system and method of controlling airflow to a turbomachine |
| 01/13/2010 | EP2143981A1 Gasket for providing a seal between two objects |
| 01/13/2010 | EP2143912A1 Gas turbine with at least one multi-stage compressor unit with multiple compressor modules |
| 01/13/2010 | EP2143911A2 Fuel supply system for a gas turbine engine |
| 01/13/2010 | EP2143907A1 System and method for eddy flow conversion |
| 01/13/2010 | EP2143887A2 Spring seal for blade dovetail |
| 01/13/2010 | EP2143821A1 Discharge surface treatment method and repairing method |
| 01/13/2010 | EP2142779A2 Acoustic panel having a variable acoustic characteristic |
| 01/12/2010 | US7645348 Repair process |
| 01/12/2010 | US7644572 Compact lightweight turbine |
| 01/12/2010 | CA2465837C Fan blade with embrittled tip |
| 01/12/2010 | CA2380677C Jet engine nose inlet cowl with de-icing protection |
| 01/10/2010 | CA2665799A1 Methods and systems to facilitate over-speed protection |
| 01/10/2010 | CA2665798A1 Methods and systems to facilitate over-speed protection |
| 01/10/2010 | CA2665797A1 Methods and systems to facilitate over-speed protection |
| 01/07/2010 | WO2010002296A1 A gas turbine engine component |
| 01/07/2010 | WO2010001656A1 Cooling air supply structure of gas turbine and gas turbine |
| 01/07/2010 | WO2010001655A1 Gas turbine and method of operating gas turbine |
| 01/07/2010 | WO2010001008A1 Method of depositing a coating for improving laminar flow |
| 01/07/2010 | WO2010000285A1 Exhaust-gas energy utilization by means of an open gas turbine process |
| 01/07/2010 | WO2009138685A3 Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle |
| 01/07/2010 | WO2009138581A3 Rotor for the compressor of a turbine engine comprising a centripetal air-collecting means |
| 01/07/2010 | WO2009052794A3 Fuel-metering unit for an aircraft engine |
| 01/07/2010 | US20100003553 Method for improved efficiency for producing fuel gas for power generation |
| 01/07/2010 | US20100003127 Air cooled bucket for a turbine |
| 01/07/2010 | US20100000227 Air intake for an aircraft turbine engine |
| 01/07/2010 | US20100000218 Gas turbine combustor and fuel supply method for same |
| 01/07/2010 | US20100000217 Turbine engine with interstage heat |
| 01/07/2010 | US20100000197 Impingement cooling for turbofan exhaust assembly |
| 01/07/2010 | DE102008031730A1 Bearing housing for exhaust gas turbo charger of internal-combustion engine, has bearing surface for mounting shaft, by which turbine wheel and compressor wheel are coupled with one another |
| 01/07/2010 | DE102008031724A1 Twin-scroll-Abgasturbolader für eine Brennkraftmaschine Twin-scroll turbocharger for an internal combustion engine |
| 01/07/2010 | DE102008031186A1 Jet engine has axial hollow shaft, which is supported by shaft bearing in housing of engine, and bearing compartment is provided, which is held by compressed air supply under excess pressure for shaft bearing |
| 01/07/2010 | DE102008031185A1 Turbofantriebwerk mit mindestens einer Vorrichtung zum Antreiben mindestens eines Generators Turbofan engine with at least one device for driving at least one generator |
| 01/07/2010 | DE102008027275A1 Air-breathing nacelle for aircraft engine, has circular front contour and sucking unit that is provided for sucking air into nacelle, where sucking unit comprises turbocharger with fan and turbine |
| 01/06/2010 | EP2141340A2 A fuel control arrangement for a gas turbine |
| 01/06/2010 | EP2141339A1 Turbofan engine with at least one device for driving at least one generator |
| 01/06/2010 | EP2141338A2 Control system |
| 01/06/2010 | EP2141337A2 Method and system for damped acoustic panels |
| 01/06/2010 | EP2141325A2 Gas turbine engine with counterrotating compressors |
| 01/06/2010 | EP2141262A1 Heat resistant component |
| 01/06/2010 | EP2140178A2 Double seal with pressurised lip |
| 01/06/2010 | EP2140121A2 Method and system for starting a turboshaft engine by cold weather |
| 01/06/2010 | EP2140120A2 Method for making an acoustic treatment coating including a cellular structure with a complex shape, and acoustic treatment coating thus obtained |
| 01/06/2010 | CN101622433A Blast furnace gas burning facility and its operation method |
| 01/06/2010 | CN101619677A Vortex air-oil separator system |
| 01/06/2010 | CN101619676A Vane separator for an air intake of a gas turbine |
| 01/05/2010 | US7640752 Device for guiding an element in an orifice in a wall of a turbomachine combustion chamber |
| 01/05/2010 | US7640751 Fuel heating system for turbine engines |
| 01/05/2010 | US7640748 System and method of cooling steam turbines |
| 01/05/2010 | US7640723 Engine with fuel/lubricant supply system for bearing lubrication |
| 01/05/2010 | US7640643 Conversion of combined cycle power plant to compressed air energy storage power plant |
| 01/05/2010 | CA2419788C Methods for filtering air for a gas turbine system |
| 01/05/2010 | CA2334628C Microcomponent assembly for efficient contacting of fluid |
| 01/05/2010 | CA2273598C Ceramic thermal barrier coating with low thermal conductivity, deposition process for said ceramic coating, and metal piece protected by this coating |
| 12/31/2009 | US20090324424 Air cooled bucket for a turbine |
| 12/31/2009 | US20090324395 Method of repairing knife edge seals |
| 12/31/2009 | US20090324393 Ceramic matrix composite turbine engine component |
| 12/31/2009 | US20090324390 Liner for a gas turbine engine casing |
| 12/31/2009 | US20090324388 Gas turbine and cooling air supply structure thereof |
| 12/31/2009 | US20090324386 Gas turbine |
| 12/31/2009 | US20090322102 System and Method for Power Production Using a Hybrid Helical Detonation Device |