Patents
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)
09/2007
09/27/2007US20070224033 Fanned trailing edge teardrop array
09/27/2007US20070220899 System for deicing an aircraft turbine engine inlet cone
09/27/2007US20070220898 Secondary fuel nozzle with improved fuel pegs and fuel dispersion method
09/27/2007US20070220735 Fastener assembly for attaching a non-metal component to a metal component
09/27/2007DE19719777B4 Vorrichtung zur Begrenzung der Brandgefahr im Inneren einer Turbomaschine A device for limiting the risk of fire in the interior of a turbomachine
09/27/2007DE102007006723A1 Messvorrichtung zur Messung der Temperatur eines thermisch belasteten, mit einer schützenden Oberflächenbeschichtung versehenen, metallischen Grundkörpers sowie Verfahren zur Herstellung einer solchen Messvorichtung Measuring device for measuring the temperature of a thermal load, provided with a protective surface coating, the metallic base body, and methods for producing such Messvorichtung
09/27/2007CA2643374A1 Calibration of optical patternator spray parameter measurements
09/27/2007CA2643373A1 Method of computing spray parameters from optical patternation
09/27/2007CA2581822A1 Auxiliary gas turbine engine assembly, aircraft component and controller
09/27/2007CA2576004A1 Oxidation-resistant coating and formation method thereof, thermal barrier coating, heat-resistant member, and gas turbine
09/26/2007EP1837506A2 Monitoring gas turbine engines
09/26/2007EP1836443A1 Rich catalytic injection
09/26/2007EP1836407A1 Bearing assembly with debris trap
09/26/2007EP1334309B1 Method for supplying fuel to a premix burner
09/26/2007EP1295021B1 Method and apparatus for providing shutoff, overspeed protection, and directional control of a bypass flow in a fuel delivery system
09/26/2007CN101042073A Advanced turbulator arrangements for microcircuits
09/26/2007CN101042072A Temperature and/or pressure sensor assembly
09/26/2007CN101041385A De-icing system for the inlet cone of an aircraft turboengine
09/26/2007CN100339558C Internal core outline for vortex blade
09/25/2007US7273130 Device and method for active soundproofing, and power unit for aeroplanes
09/25/2007US7272933 Methods and apparatus for operating gas turbine engines
09/25/2007US7272931 Method and apparatus to decrease combustor acoustics
09/25/2007CA2292914C Air intake structure for aircraft engine
09/22/2007CA2581908A1 Repair of hpt shrouds with sintered preforms
09/22/2007CA2581540A1 Turbine engine inlet cone deicing system for aircraft
09/20/2007US20070214798 Process For Producing Electrical Power
09/20/2007US20070214791 Combustor dome assembly including retaining ring
09/19/2007EP1835148A2 Component for fuel supply
09/19/2007EP1835147A2 Turbofan
09/19/2007EP1835132A1 Covering of a casing in a jet engine
09/19/2007EP1835128A2 Air-oil heat exchanger
09/19/2007EP1834872A1 Pre-hung inlet door system
09/19/2007EP1834083A1 Variable rate ignition
09/19/2007EP1337748B1 Fan-stator interaction tone reduction
09/19/2007CN101037946A Fastening arrangement of a pipe on a circumferential surface
09/19/2007CN101037740A High-temperature alloy part and welding material
09/19/2007CN101037739A High-temperature alloy material
09/19/2007CN101037738A High-temperature alloy part and welding material
09/19/2007CN100338344C Method for utilizing gas reserves with low methane concentrations and high inert gas concentrations for fueling gas turbines
09/18/2007US7270852 Aluminizing slurry compositions free of hexavalent chromium, and related methods and articles
09/18/2007US7270519 Methods and apparatus for reducing flow across compressor airfoil tips
09/18/2007US7270175 Extended impingement cooling device and method
09/18/2007US7270170 Investment casting core methods
09/18/2007US7269958 Combustor exit duct
09/18/2007US7269956 Device for utilizing the waste heat of compressors
09/18/2007US7269954 Method for operating a gas turbine installation, and gas turbine installation
09/18/2007US7269939 Method and apparatus for automatically actuating fuel trim valves in a gas
09/18/2007CA2349994C Turbojet powerplant with heat exchanger
09/18/2007CA2347329C Methods and apparatus for supplying cooling airflow in turbine engines
09/13/2007WO2007101814A1 Gas turbine
09/13/2007DE19963374B4 Vorrichtung zur Kühlung einer, einen Strömungskanal umgebenden Strömungskanalwand mit wenigstens einem Rippenelement Apparatus for cooling a surrounding a flow channel flow channel wall with at least one rib member
09/13/2007DE102006031551A1 Flammenrückschlag-Erfassungseinrichtung, Flammenrückschlag-Erfassungsverfahren und Gasturbine Flashback-detecting means, flashback detection method and gas turbine
09/13/2007DE102006011513A1 Einlaufkonus aus einem Faserverbundwerkstoff für ein Gasturbinentriebwerk und Verfahren zu dessen Herstellung Inlet cone from a fiber composite material for a gas turbine engine and method of producing the
09/13/2007DE102006011248A1 Gas turbine combustion chamber wall has damping recesses for inner wall, with respective center axis arranged perpendicularly to inner wall, and cooling recesses, with respective center axis inclined at angle to inner wall
09/13/2007DE102006011062A1 Compressor for turbocharging vehicle engine, includes segments with cooling channels and optional heat exchanger, to reduce temperature of air charged to engine
09/13/2007CA2581386A1 Process for cleaning passages in workpieces, and associated apparatus
09/12/2007EP1832734A2 Gas turbine engine with dirt separator and method of removing impurities from a gas turbine engine
09/12/2007EP1832733A2 Inlet cone made of a fibre composite for a gas turbine plant and method for its manufacture
09/12/2007EP1832713A1 Gas turbine
09/12/2007EP1831530A1 Compressor variable stage remote actuation for turbine engine
09/12/2007EP1831505A1 Static gas turbine component and method for repairing such a component
09/12/2007EP1385668A4 Method of repairing a turbin blade tip
09/12/2007CN101035966A Structure for separating the internal areas of a high pressure and a low pressure turbine
09/11/2007US7267301 Aircraft engine with means of suspension from the structure of an aircraft
09/11/2007US7266946 Gas fuel compression by liquification
09/11/2007US7266945 Fuel injection apparatus
09/11/2007US7266941 Turbofan case and method of making
09/11/2007CA2432687C Gas turbine
09/11/2007CA2364768C Bolted joint for rotor disks and method of reducing thermal gradients therein
09/07/2007WO2007099895A1 Impingement cooling structure
09/07/2007WO2007099768A1 Multijet igniting detonator, pulse combustor equipped with that detonator, and method for generating detonation
09/07/2007WO2007098590A1 Internal fuel manifold with turned channel having a variable cross-sectional area
09/07/2007CA2644099A1 Impingement cooled structure
09/07/2007CA2643325A1 Internal fuel manifold with turned channel having a variable cross-sectional area
09/06/2007US20070205189 Method of repairing a stationary shroud of a gas turbine engine using laser cladding
09/06/2007US20070204624 Fuel injector for a turbine engine
09/06/2007US20070204621 Fuel conveying member with side-brazed sealing members
09/06/2007DE102006009860A1 Verfahren zur Herstellung eines Dichtsegments und Dichtsegment zur Verwendung in Verdichter- und Turbinenkomponenten A process for the preparation of a sealing segment and sealing segment for use in compressor and turbine components
09/05/2007EP1830036A2 Internal fuel manifold with turned channel having a variable cross-sectional area
09/05/2007EP1829006A1 Fire warning system
09/05/2007EP1828574A1 Close coupled gearbox assembly for a tip turbine engine
09/05/2007EP1828573A1 Hydraulic seal for a gearbox of a tip turbine engine
09/05/2007EP1828572A1 Method for the operation of a gas turbo group
09/05/2007EP1828571A1 Ventilating air intake arrangement
09/05/2007EP1828570A1 Configurations and methods for lng fueled power plants
09/05/2007EP1827656A1 Method for removing and recovering co2 from an exhaust gas
09/05/2007CN200943528Y Sliding bearing oil seal device for heavy gas turbine
09/05/2007CN101029598A Methods and systems of variable extraction for gas turbine control
09/05/2007CN101029597A Fixed geometrical supersonic-speed and high supersonic-speed adjusting air inlet
09/05/2007CN100335762C Method and apparatus for achieving power augmentation in gas turbines using wet compression
09/05/2007CN100335748C Blade for turbine engine and method for production of said blade
09/04/2007US7264710 Reacting vanadium-containing heavy oil, water, and an oxidizing agent thereby reforming heavy oil and oxidizing vanadium with oxidizing agent, and subsequently removing vanadium oxide with the aid of a vanadium oxide scavenger
09/04/2007US7264438 Method for cooling a turbo machine and turbo machine
09/04/2007US7263834 Method for cooling a gas turbine system and a gas turbine system for performing this method
09/04/2007US7263772 Foam wall combustor construction
09/04/2007CA2274412C Thermal barrier coating system utilizing localized bond coat and article having the same
08/2007
08/30/2007WO2007098360A1 Turbocharger with liquid-cooled center housing
08/30/2007WO2007097639A1 Device for an insulation plate for an exhaust pipe from a combustion engine
08/30/2007WO2007096493A1 Integration of a starter/generator module in a gas turbine transmission housing
08/30/2007US20070201974 Nested core gas turbine engine