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)
12/2006
12/28/2006CA2611983A1 System for defrosting the leading edge sheath of an air inlet hood for a turboengine
12/28/2006CA2611656A1 Anti-icing and deicing system for aircraft engine pod with resistive mat
12/27/2006EP1736652A2 Method and device for improving combustion by fuel deoxygenation
12/27/2006EP1736651A2 Gas turbine burner fuel feeding system
12/27/2006EP1736650A2 Methods and apparatus for operating gas turbine engines
12/27/2006EP1736635A2 Air transfer system between compressor and turbine of a gas turbine engine
12/27/2006EP1735531A2 Method and device for reducing engine noise
12/27/2006EP1735529A1 Method and apparatus generating multiple pressure signals in a fuel system
12/27/2006EP1664506B1 Air turbine starter with unitary inlet and stator
12/27/2006EP1444388B1 Mcraly-coating
12/27/2006EP1190200B1 Fuel injector heat shield
12/27/2006CN2851601Y Positive-displacement sustained-combustion type engine
12/27/2006CN1886582A Power generation
12/27/2006CN1292150C High thrust turbosupercharger rotor with ball bearing
12/26/2006US7153599 Cooled turbine integrated fuel cell hybrid power plant
12/26/2006US7153343 Oxygen receiving channel and oxygen permeable self-supporting porous membrane; sweep gas and/or vacuum maintains an oxygen concentration differential across the membrane to deoxygenate the fuel; use in stabilizing jet fuels for aircraft
12/26/2006US7153099 Inter-vane platform with lateral deflection for a vane support of a turbine engine
12/26/2006US7153091 Gas turbine engine
12/26/2006US7153054 Fastener assembly for attaching a non-metal component to a metal component
12/26/2006US7152411 Rabbet mounted combuster
12/26/2006US7152410 System and method for dumping surge flow into eductor primary nozzle for free turbine
12/24/2006CA2550784A1 Anti-rotation stop of a retaining nut for a part on a shaft, retaining nut and shaft upon which the device is mounted and aircraft engine upon which the device is mounted
12/21/2006WO2006133541A1 Internally mounted fuel manifold with support pins
12/21/2006US20060284015 Fire shield method
12/21/2006US20060283206 Method for efficient nonsynchronous lng production
12/21/2006US20060283192 Engine fueling method
12/21/2006US20060283190 Engine status detection with external microphone
12/21/2006US20060283170 Radial flow turbine
12/20/2006EP1733170A1 Liquid fuel injection with purge air
12/20/2006EP1733127A1 Gas turbine inlet flow straightener with restricting member
12/20/2006CN1880742A Protective cover for turbofan engine of aeroplane
12/20/2006CN1291143C Once surface heat regenerator
12/20/2006CN1291142C Air-bleed transmission equipment of combustion turbine
12/20/2006CN1291141C Gas turbine combined plant and method of operating same
12/19/2006US7150921 oxidation-resistant layer comprising one or more intermetallics containing aluminum or chromium, and a second, less dense layer comprising polyester and one or more intermetallics containing aluminum and/or chromium
12/19/2006US7150416 Liquid fuel injection
12/19/2006US7150143 Hybrid fuel cell-pulse detonation power system
12/19/2006CA2381671C Steam-cooling-type turbine
12/19/2006CA2376582C Gas turbine plant with high detection sensitivity of extraordinary state
12/19/2006CA2268402C A method of reducing the gap between a liner and a turbine distributor of a turbojet engine
12/19/2006CA2202541C Tangential air entry fuel nozzle
12/14/2006WO2006131623A1 System for deicing the leading edge of a nose inlet cowl for a turbine engine
12/14/2006WO2006131405A1 Gas turbine with a gap blocking device
12/14/2006US20060282242 Methods and apparatus for modeling gas turbine engines
12/14/2006US20060280979 Power generating system
12/14/2006US20060280556 Device for stabilizing the engine inlet flow in static tests of engines
12/14/2006US20060277920 Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, power take-off module for the turbine engine and method of assembling the turbine engine
12/14/2006US20060277917 Thermochemical water splitting power generation process and system
12/14/2006US20060277916 Method of operating an atomizing arrangement
12/14/2006US20060277912 Gas turbine system
12/14/2006DE102004058404B4 Vorrichtung und Verfahren zum Berechnen der mechanischen Turbinen-Ausgangsleistung, und diese(s)anwendende Vorrichtung und Verfahren zum Steuern einer Gasturbine Device and method for calculating the mechanical turbine output, and this (S)-applying apparatus and method for controlling a gas turbine
12/14/2006DE102004047939B4 Wellenfehlausrichtungs-Messvorrichtung, Wellenfehlausrichtungs-Messverfahren, kombinierte Anlage mit Einzelwelle mit Wellenfehlausrichtungs-Messvorrichtung und Anfahrverfahren der kombinierte Anlage mit Einzelwelle Shaft misalignment measurement device, shaft misalignment measurement method combined system with single shaft with shaft misalignment measurement device, and start-up procedure of the combined system with single shaft
12/14/2006CA2610787A1 System for deicing the leading edge of a nose inlet cowl for a turbine engine
12/13/2006EP1732062A2 Silencer
12/13/2006EP1731735A2 A multi-spool gas turbine engine with a load shift and transfer system.
12/13/2006EP1731717A2 Seal assembly for sealing space between stator and rotor in a gas turbine
12/13/2006EP1731714A1 Clearance blocking device and use of such a clearance blocking device
12/13/2006EP1731215A1 Spiral wound fuel stabilization unit for fuel de-oxygenation
12/13/2006EP1730449A1 Combustion chamber for a gas turbine and associated operating method
12/13/2006EP1730448A1 Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement
12/13/2006EP1730445A1 Method for operating a heat engine, preferably a gas turbine installation
12/13/2006EP1730444A1 Method for the operationof a heat engine, preferably a gas turbine plant
12/13/2006CN1878936A Method and apparatus for actuating fuel trim valves in a gas turbine
12/13/2006CN1878931A Sealing arrangement in a compressor
12/13/2006CN1877102A Impeller-pressurizing rotor-injection type steam turbine
12/13/2006CN1877101A Gas turbine, method of controlling air supply and computer program product for controlling air supply
12/12/2006US7149632 On-line system and method for processing information relating to the wear of turbine components
12/12/2006US7147899 Process of masking cooling holes of a gas turbine component
12/12/2006US7147684 Device for filtering particles out of a coolant flow in a turbo machine
12/12/2006US7147440 Methods and apparatus for cooling gas turbine engine rotor assemblies
12/12/2006US7147436 Turbine engine rotor retainer
12/12/2006US7147432 Turbine shroud asymmetrical cooling elements
12/12/2006US7147430 Pneumatic valve control using downstream pressure feedback and an air turbine starter incorporating the same
12/12/2006US7147050 Recuperator construction for a gas turbine engine
12/12/2006US7146815 Combustor
12/12/2006US7146794 Gas turbine installation
12/12/2006US7146705 Manufacturing cell using tooling apparatus
12/12/2006US7146697 Seal removal tool
12/12/2006US7146674 Rotary probe for cleaning an internal cavity
12/07/2006WO2006129398A1 Gasification hybrid power generation equipment and method for controlling the same
12/07/2006WO2006128827A1 An air intake for a turbocharger for an internal combustion engine
12/07/2006WO2006112807A3 Turbine engine and method for starting a turbine engine
12/07/2006US20060272957 Tandem blisk electrochemical machining
12/07/2006US20060272887 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive Herschel-Quincke tubes
12/07/2006US20060272332 System for introducing fuel to a fluid flow upstream of a combustion area
12/07/2006US20060272331 Thermal power plant with sequential combustion and reduced-CO2 emission, and a method for operating a plant of this type
12/07/2006US20060272330 Fuel distributor and mounting system therefor and method of mounting a fuel distributor
12/07/2006US20060272313 More electric aircraft power transfer systems and methods
12/07/2006DE102005025244A1 Air guiding system between compressor and turbine for gas-turbine engine operated at high pressure ratio has compressor and air chamber whereby first turbine cooling air is flowed through air chamber
12/07/2006DE102004003354B4 Turbinen-Laufschaufel und Gasturbine Turbine blade and gas turbine
12/06/2006EP1728991A2 Electrothermal inlet ice protection system
12/06/2006EP1728990A2 Auxiliary power unit supplied with air from the gas turbine
12/06/2006EP1728974A2 Modular fan inlet case
12/06/2006EP1728973A1 Method to block a clearance in a Turbomachine and Turbomachine to carry out the method
12/06/2006CN1873200A Original surface type heat regenerator for minitype gas turbine
12/06/2006CN1873035A High temperature aluminium alloys
12/06/2006CN1288334C Electricity generating and liquid purifying apparatus
12/06/2006CN1288266C Ni base sintered alloy
12/05/2006US7144740 Method for chromatographic finger printing and standardization of single medicines and formulations
12/05/2006US7144349 Gas turbine gearbox