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