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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09/15/2009 | US7587887 Advanced humid air turbine power plant |
09/15/2009 | CA2494433C One-piece flame-retention nozzle arm for a turbofan after-burner |
09/14/2009 | CA2658072A1 Gas turbine accessory drive assembly |
09/10/2009 | US20090226308 Combined cold and power (ccp) system and method for improved turbine performance |
09/10/2009 | US20090226303 Variable area fan nozzle fan flutter management system |
09/10/2009 | US20090226295 Method and apparatus for delivering a liquid |
09/10/2009 | US20090223229 Method and System for Using Low BTU Fuel Gas in a Gas Turbine |
09/10/2009 | US20090223228 Method and apparatus for combusting fuel within a gas turbine engine |
09/10/2009 | US20090223227 Combustion cap with crown mixing holes |
09/10/2009 | US20090223226 Gas turbine combustor and gaseous fuel supply method for gas turbine combustor |
09/10/2009 | US20090223225 Method and apparatus for controlling combustor operability |
09/10/2009 | US20090223184 Single/multiple guard(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s) - centrifuge chamber/manifold particle collector |
09/10/2009 | US20090223054 Fuel nozzle for a gas turbine engine and method of fabricating the same |
09/10/2009 | DE202009007436U1 Vorrichtung zum Abdichten eines Lagergehäuses eines Abgasturboladers An apparatus for sealing a bearing housing of an exhaust turbocharger |
09/10/2009 | DE102009003574A1 Verfahren und System zur Herstellung eines Dichtrings A method and system for making a sealing ring |
09/10/2009 | DE102007054467B4 Verfahren zur Brennstoffvorwärmung Method for fuel preheating |
09/09/2009 | EP2098757A2 Gearbox gear and nacelle arrangement |
09/09/2009 | EP2098714A2 High bypass-ratio turbofan jet engine |
09/09/2009 | EP2098615A1 Highly oxidation resistant component |
09/09/2009 | EP2098614A1 Highly oxidation resistant component |
09/09/2009 | CN100538305C Vibration measurement and recording system and method |
09/09/2009 | CN100538138C Hingeless flapper valve for flow control |
09/09/2009 | CN100538047C System for defrosting the leading edge sheath of an air inlet hood for a turboengine |
09/09/2009 | CN100538044C Working method for turbocharger and turbocharger |
09/09/2009 | CN100538018C Turbine shroud segment |
09/09/2009 | CN100537354C Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
09/08/2009 | US7585152 Cooling jets |
09/08/2009 | US7584621 Radially expanding turbine engine exhaust cylinder interface |
09/08/2009 | US7584620 Support system for transition ducts |
09/08/2009 | US7584619 System for reducing oil consumption in gas turbine engines |
09/08/2009 | US7584617 Monitoring health of a combustion dynamics sensing system |
09/08/2009 | US7584600 Gas turbine, in particular aircraft engine and method for generating electrical energy in a gas turbine |
09/08/2009 | CA2480985C Triple circuit turbine blade |
09/03/2009 | WO2009108084A1 A gas turbine component and a method for producing a gas turbine component |
09/03/2009 | WO2009107805A1 Plant state monitoring method, plant state monitoring computer program, and plant state monitoring device |
09/03/2009 | WO2009107438A1 Connection structure of exhaust chamber, support structure of turbine, and gas turbine |
09/03/2009 | WO2009107437A1 Gas turbine, and interior opening method for the gas turbine |
09/03/2009 | WO2009107418A1 Turbine disc and gas turbine |
09/03/2009 | WO2009107410A1 Gas turbine and method for maintaining and inspecting the same |
09/03/2009 | WO2009107312A1 Gas turbin and disc and method for forming radial passage of disc |
09/03/2009 | WO2009107311A1 Gas turbine and method of opening casing of gas turbine |
09/03/2009 | WO2006119409A3 West compression apparatus and method |
09/03/2009 | US20090220333 Gas turbine comprising a unit for detecting a shaft rupture |
09/03/2009 | US20090218821 Low emission turbine system and method |
09/03/2009 | US20090217672 Fuel Ratio Control in a Combustion Apparatus with Multiple Fuel Supply Lines |
09/03/2009 | US20090217669 Fuel nozzles |
09/03/2009 | DE102008011747A1 Verfahren zum thermochemischen Reinigen und/oder Strippen von Turbinenbauteilen A method for thermo-chemical cleaning and / or stripping of turbine components |
09/02/2009 | EP2096271A2 System and method for passive cooling of gas turbine engine control components |
09/02/2009 | EP2096029A2 Nose cone assembly and gas turbine engine comprising such an assemby |
09/02/2009 | EP1885999B1 Air intake for a turbocharger for an internal combustion engine |
09/02/2009 | EP1725755A4 Internal fuel manifold for gas turbine engine or gas turbine fuel nozzle assembly |
09/02/2009 | CN201301753Y Inner wave rider type air inlet channel taking internal and external flow performance into consideration |
09/02/2009 | CN201301752Y Inner wave rider type hypersonic speed air inlet channel with customized shapes of inlet and outlet |
09/02/2009 | CN201301751Y Inner wave rider type hypersonic speed air inlet channel based on arbitrary shaped shock wave |
09/02/2009 | CN101523031A Method and device for starting and stopping gas turbine |
09/02/2009 | CN101523030A Removable air intake structure for turbojet engine nacelle |
09/02/2009 | CN100535415C Closed circuit blade-cooled turbine |
09/01/2009 | US7582362 Thermal spray compositions for abradable seals |
09/01/2009 | US7581402 Turbine engine combustor with bolted swirlers |
09/01/2009 | US7581385 Metering sheet and iso-grid arrangement for a non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct |
09/01/2009 | US7581378 Anti-icing apparatus and method for aero-engine nose cone |
09/01/2009 | US7581301 Method for attaching a non-metal component to a metal component |
09/01/2009 | CA2371326C Procedure for de-icing a jet engine air inlet cowl by means of forced circulation of a fluid, and device for applying the said procedure |
09/01/2009 | CA2344210C Dynamic control system and method for catalytic combustion process and gas turbine engine utilizing same |
08/29/2009 | CA2655842A1 System and method for passive cooling of gas turbine engine control components |
08/27/2009 | WO2009103691A1 Fastening device for an exhaust-gas turbocharger |
08/27/2009 | WO2009103671A1 Gas turbine having an improved cooling architecture |
08/27/2009 | WO2009103632A1 Gas turbine |
08/27/2009 | WO2009085580A3 Turbine nozzle segment and method for repairing a turbine nozzle segment |
08/27/2009 | WO2009044093A3 Fuel supply system |
08/27/2009 | US20090214329 Filter system for blade outer air seal |
08/27/2009 | US20090211920 System for maintaining hydrogen purity in electrical generators and method thereof |
08/27/2009 | US20090211260 Multi-Spool Intercooled Recuperated Gas Turbine |
08/27/2009 | US20090211257 Fuel supply arrangement |
08/27/2009 | US20090211256 Feed arm for a multiple circuit fuel injector |
08/27/2009 | DE3820962B4 Brennstoffeinspritzsystem für Gasturbinentriebwerke A fuel injection system for gas turbine engines |
08/27/2009 | DE102009010604A1 Zuleitungsarm für eine Mehrkreisbrennstoffeinspritzeinrichtung Feed arm for a multi-circuit fuel injector |
08/27/2009 | DE102009003486A1 Energieerzeugungssystem mit einer Abgastemperaturabsenkvorrichtung und System zur Steuerung einer Temperatur von Abgasen A power generation system with a Abgastemperaturabsenkvorrichtung and system for controlling a temperature of exhaust gases |
08/27/2009 | DE102008011108A1 Verfahren und Reinigen von Gasturbinenbauteilen A method and cleaning of gas turbine components |
08/27/2009 | CA2655916A1 Split annular ring for turbine engine rotating part |
08/26/2009 | EP2093401A2 Seal assembly for a gas turbine |
08/26/2009 | EP2093400A2 Hybrid electrical-mechanical turbine engine fuel supply system |
08/26/2009 | EP2093399A1 Gas turbine comprising exhaust cooling |
08/26/2009 | EP2092184A1 A liner for a turbine section, a turbine section, a gas turbine engine and an aeroplane provided therewith |
08/26/2009 | EP1994269B1 Integration of a starter/generator module in a gas turbine transmission housing |
08/26/2009 | CN201297208Y Bearing unit with extruded oil film groove and squirrel-cage elasticity supporting structure |
08/26/2009 | CN201296385Y Supercharging system of double power airplane |
08/26/2009 | CN101517213A 燃气轮机 Gas turbine |
08/26/2009 | CN101514818A Power generation system having an exhaust gas attemperating device and system for controlling a temperature of exhaust gases |
08/26/2009 | CN101514658A Rear end liner assembly with turbulator and its cooling method |
08/26/2009 | CN101514657A Systems and methods for exhaust gas recirculation (egr) for turbine engines |
08/26/2009 | CN100532947C Annular combustion chamber of gas turbine and gas turbine |
08/26/2009 | CN100532946C Bolt capable of internal cooling |
08/25/2009 | US7579094 Orientation of the first warp direction of a preselected number of plies lie in the direction of maximum tensile stress during normal operation; shape is rigidized with a layer of BN and/or SiC; ceramic lies in interstitial regions between the tows of each ply and between the plies; aircraft |
08/25/2009 | US7578134 Methods and apparatus for assembling gas turbine engines |
08/25/2009 | US7578120 Device for injecting water or water vapor into the working medium of a gas turbine plant |
08/25/2009 | CA2552166C Ram air channel for the supply of ambient air in an aircraft |
08/25/2009 | CA2438353C Method of diagnosing gas turbine condition and system for diagnosing the same |
08/20/2009 | WO2009102907A2 System, method and apparatus for lean combustion with plasma from an electrical arc |
08/20/2009 | WO2009101912A1 Method for repairing turbine rotor blade |