| 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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| 06/01/2011 | EP2327859A2 Mounting system for a planetary gear train in a gas turbine engine |
| 06/01/2011 | EP2327858A2 Composite slider seal for turbojet penetration |
| 06/01/2011 | EP2326845A1 Compressor casing resistant to titanium fire, high pressure compressor including such a casing, and aircraft engine including such a compressor |
| 06/01/2011 | EP2326816A2 Fuel injector sans support/stem |
| 06/01/2011 | EP1296796B1 Welding superalloy articles |
| 06/01/2011 | DE102010006143A1 Schalldämpfer für ein Hilfstriebwerk eines Flugzeugs Silencer for an auxiliary power unit of an aircraft |
| 06/01/2011 | DE102009055880A1 Aircraft gas turbine, has closure element arranged in air discharging channel and made of material e.g. copper, which deforms during exceeding of predetermined temperature, so that closure element sets external function |
| 06/01/2011 | DE102009055879A1 Flugzeugenteisungsvorrichtung und Triebwerksgondel einer Fluggasturbine mit Enteisungsvorrichtung Flugzeugenteisungsvorrichtung and engine nacelle of an aircraft gas turbine with de-icer |
| 06/01/2011 | DE102009055865A1 Verstelleinrichtung für eine Aufladeeinrichtung Adjusting for charging |
| 06/01/2011 | CN201851217U Hydraulic starting and control oil system of aero-derivative gas turbine |
| 06/01/2011 | CN201851210U Low-temperature exhaust engine |
| 06/01/2011 | CN102084105A Thermal power plant with CO2 sequestration |
| 06/01/2011 | CN102080601A Pilot burner of a gas turbine engine, combustor, and gas turbine engine |
| 06/01/2011 | CN102080600A System and method for generating power by applying chemical purge gas |
| 06/01/2011 | CN101374723B Dual flow turbine engine equipped with a precooler |
| 05/31/2011 | US7950605 Torsionally de-coupled engine mount system |
| 05/31/2011 | US7950239 Method for operating a gas turbine plant |
| 05/31/2011 | US7950217 Oxygen-enriched air assisting system for improving the efficiency of cogeneration system |
| 05/31/2011 | CA2662039C Turbine shroud gas path duct interface |
| 05/31/2011 | CA2434492C Assist and back-up for electrical auxiliary drive |
| 05/26/2011 | WO2011062231A1 Heat-resistant superalloy |
| 05/26/2011 | WO2011061438A1 Device for changing the transmission ratio between a turbine shaft and a starter/generator shaft of aircraft engine |
| 05/26/2011 | WO2011061437A1 Mounting of accessory casing onto an intermediate housing for a jet engine air blower compartment |
| 05/26/2011 | WO2011061430A1 Acoustic skin for an aircraft nacelle acoustic panel |
| 05/26/2011 | WO2011061143A1 Combustion chamber having a ventilated spark plug |
| 05/26/2011 | WO2011061079A1 Gas turbine cycle with water injection for generating electricity |
| 05/26/2011 | WO2011060987A1 Laser spark plug |
| 05/26/2011 | WO2010105891A3 Burner assembly |
| 05/26/2011 | US20110123326 Bellows preload and centering spring for a fan drive gear system |
| 05/26/2011 | US20110123312 Gas turbine engine components with improved film cooling |
| 05/26/2011 | US20110123311 Serpentine cored airfoil with body microcircuits |
| 05/26/2011 | US20110123310 Turbine airfoil platform cooling core |
| 05/26/2011 | US20110120143 Jet engine nacelle intended to equip an aircraft |
| 05/26/2011 | US20110120142 Gas turbine engine fuel conveying member |
| 05/26/2011 | US20110120141 Combustor system |
| 05/26/2011 | US20110120139 Modified gas and steam turbine process with integrated coal gasification under pressure |
| 05/26/2011 | US20110120135 Turbulated aft-end liner assembly and cooling method |
| 05/26/2011 | US20110120132 Dual walled combustors with impingement cooled igniters |
| 05/26/2011 | US20110120125 Locating Mechanism for Turbocharger Bearing |
| 05/26/2011 | US20110120077 Burner having a protective element for ignition electrodes |
| 05/26/2011 | US20110120076 Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone |
| 05/26/2011 | DE102009054007A1 Gas turbine i.e. flight gas turbine, for engine of e.g. jet, has circular seal element including outer ring at axial side and thread at opposite axial side, where thread of circular seal element is screwed on thread of high pressure shaft |
| 05/26/2011 | DE102009046940A1 Mehrstufige Aufladegruppe, Aufladesystem und Brennkraftmaschine, jeweils mit der mehrstufigen Aufladegruppe Multi-stage supercharger, turbocharger system and the internal combustion engine, each with the multi-stage turbocharger |
| 05/26/2011 | DE10038452B4 Abdichtung einer thermischen Turbomaschine Sealing a thermal turbomachinery |
| 05/26/2011 | CA2780838A1 Device for changing the transmission ratio between a turbine shaft and a starter/generator shaft of aircraft engine |
| 05/26/2011 | CA2780659A1 Mounting of accessory casing onto an intermediate housing for a jet engine air blower compartment |
| 05/26/2011 | CA2780594A1 Combustion chamber having a ventilated spark plug |
| 05/26/2011 | CA2778385A1 Acoustic skin for an aircraft nacelle acoustic panel |
| 05/25/2011 | EP2325542A1 Swirler vane, swirler and burner assembly |
| 05/25/2011 | EP2325491A1 Compressor drive device and operation method |
| 05/25/2011 | EP2325459A1 Cooling air supply structure of gas turbine and gas turbine |
| 05/25/2011 | EP2325458A2 Bellows preload and centering spring for a fan drive gear system |
| 05/25/2011 | EP2325456A1 Gas turbine cycle with water injection for generating electricity |
| 05/25/2011 | EP2324234A1 Ignition device for a laser ignition of an internal combustion engine |
| 05/25/2011 | EP2140121B8 Method and system for starting a turboshaft engine by cold weather |
| 05/25/2011 | EP2134928B1 Assembly device for assembling and disassembling a rotor of a turbomachine consisting of rotor disks |
| 05/25/2011 | EP1841960B1 Starter generator system for a tip turbine engine |
| 05/25/2011 | CN201843685U Air intake cooling device of gas turbine |
| 05/25/2011 | CN1900500B Decoupling sleeve |
| 05/25/2011 | CN102076941A Gas turbine device |
| 05/25/2011 | CN102076940A Gas turbine and method of operating gas turbine |
| 05/25/2011 | CN102076939A Cooling air supply structure of gas turbine and gas turbine |
| 05/25/2011 | CN102072023A Primary surface type regenerator |
| 05/25/2011 | CN102072022A Heat exchange matrix of double-wave primary surface recuperator for micro gas turbine |
| 05/25/2011 | CN102072021A Aircraft engine |
| 05/25/2011 | CN101550873B A kind of internal combustion engine using biofuel |
| 05/25/2011 | CN101421156B Inlet distortion and recovery control system |
| 05/24/2011 | US7946809 Exhaust-gas-turbine casing |
| 05/24/2011 | US7946119 Sealing arrangement |
| 05/24/2011 | CA2720607A1 Thermally actuated passive gas turbine engine compartment venting |
| 05/24/2011 | CA2488544C Flame detection method and apparatus for gas turbine exhaust path |
| 05/24/2011 | CA2458434C Protection device for a jet engine air intake structure |
| 05/23/2011 | CA2719995A1 Porous metal gland seal |
| 05/19/2011 | WO2011059064A1 Method for producing vane |
| 05/19/2011 | WO2011058931A1 Gas turbine combustor and gas turbine |
| 05/19/2011 | WO2011058041A1 Metal annular connecting structure for an aircraft turbine engine |
| 05/19/2011 | US20110116912 Zoned discontinuous coating for high pressure turbine component |
| 05/19/2011 | US20110115227 Turbogenerator with cooling system |
| 05/19/2011 | US20110114787 Acoustic treatment panel with integral connecting reinforcement |
| 05/19/2011 | US20110113790 Thermal machine |
| 05/19/2011 | US20110113789 Gas turbine engine combustion chamber comprising cmc deflectors |
| 05/19/2011 | US20110113787 Pilot combustor in a burner |
| 05/19/2011 | US20110113783 Premixing apparatus for fuel injection in a turbine engine |
| 05/19/2011 | US20110113748 Guiding an ignition spark plug in a turbomachine combustion chamber |
| 05/19/2011 | US20110113747 Guide for an ignition plug in a turbomachine combustion chamber |
| 05/19/2011 | DE10319017B4 Anlage zur Wartung, insbesondere Demontage, von Gasturbinen Plant for maintenance, in particular disassembly of gas turbines |
| 05/19/2011 | DE102010036888A1 System zur Aufbereitung des in eine Turbomaschine eintretenden Luftstroms System for processing the incoming air flow in turbomachinery |
| 05/19/2011 | DE102010036887A1 Integrale Auskleidungs- und Venturi-Anordnung zur Beseitigung einer Luftleckage Integral liner and venturi assembly to eliminate air leakage |
| 05/19/2011 | DE102009053638A1 Bearing for exhaust gas turbocharger for Otto engine of e.g. hybrid vehicle in aerodynamic field, has radial bearing part designed as pneumatic bearing, and axial bearing part designed as combined active and/or passive magnet bearing |
| 05/19/2011 | DE102009053237A1 Turbolader mit einer Lagerbockeinrichtung für ein in Längsrichtung geteiltes Turboladergehäuse Turbocharger with a bearing support means for a split longitudinally turbocharger housing |
| 05/19/2011 | DE102009053106A1 Turboladergehäuse und Werkzeugeinrichtung zur Bearbeitung des Turboladergehäuses Turbocharger housing and tool means for processing the turbocharger housing |
| 05/19/2011 | DE102009053104A1 Lageranordnung für eine Welle eines Turboladers Bearing arrangement for a turbocharger shaft |
| 05/19/2011 | DE102009053102A1 Axiallageranordnung für eine Welle eines Turboladers Thrust bearing assembly for a turbocharger shaft |
| 05/19/2011 | DE102009053101A1 Aufnahmeeinrichtung für das Laufzeug eines Turboladers Receiving means for the rotor assembly of a turbocharger |
| 05/19/2011 | DE102009052659A1 Gas turbine engine has drive arrangement for auxiliary equipment transmission, where transmission gear is connected with engine shaft over load transfer unit |
| 05/19/2011 | CA2780548A1 Metal annular connecting structure for an aircraft turbine engine |
| 05/18/2011 | EP2322782A1 Air intake of a turbine aircraft engine, aircraft equipped with such air intake and method for optimizing the operation of a turbine aircraft engine with an air intake |
| 05/18/2011 | EP2321520A2 Flow compensated proportional bypass valve combined with a control valve |
| 05/18/2011 | EP2321510A2 Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
| 05/18/2011 | EP2321179A1 Method for making an acoustic panel for the air intake lip of a nacelle |