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)
02/2011
02/03/2011US20110027061 Method For Braking A Rotor Of A Turbine Engine And A Turning Gear For Driving The Rotor Of A Turbine Engine
02/03/2011US20110023499 Gas turbine combustor exit duct and hp vane interface
02/03/2011US20110023498 Process for production of electric energy and co2 from a hydrocarbon feedstock
02/03/2011US20110023495 Effusion cooled dual wall gas turbine combustors
02/03/2011US20110023494 Gas turbine burner
02/03/2011US20110023493 Fuel nozzle for a turbine combustor, and methods of forming same
02/03/2011US20110023492 Fuel efficient ultra-low emission and improved pattern factor colorless distributed combustion for stationary and propulsion gas turbine applications
02/03/2011US20110023491 System and method for supplying fuel to a gas turbine
02/03/2011US20110023448 Inertia wheel with progressive run up
02/03/2011US20110023447 Cooling system for electronic device in a gas turbine engine system
02/03/2011US20110023446 Gas turbine engine
02/03/2011US20110023444 Variable speed and displacement electric fluid delivery system for a gas turbine engine
02/03/2011DE102010036495A1 Brennstoffdüse für eine Turbinenbrennkammer und Verfahren zum Ausbilden derselben Fuel nozzle for a turbine combustor and method of forming same
02/02/2011EP2280150A1 Gas turbine engine with integrated starter-generator and corresponding operating method
02/02/2011EP2279826A1 Brazing repair material and brazing repair method using the brazing repair material
02/02/2011EP1146989B1 Laser drilling holes in a cylindrical workpiece
02/02/2011CN101965443A Gas turbine and method of opening chamber of gas turbine
02/02/2011CN101963103A Apparatus for fuel injection in a turbine engine
02/02/2011CN101963102A High performance gas turbine inlet filter (HEPA) using membrane media
02/02/2011CN101963101A Systems and methods for gas turbine combustors
02/02/2011CN101592082B Distributed gas turbine power generation system of heavy oil combustion
02/01/2011US7878799 Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement
02/01/2011US7878005 Gas turbine engine
02/01/2011US7878004 Method and device for optimizing a light-up procedure of a gas turbine engine
02/01/2011US7878003 Fuel control system for gas turbine engine reheat apparatus
01/2011
01/27/2011US20110016884 Cooling passage cover, manufacturing method of the cover, and gas turbine
01/27/2011US20110016883 Cross-sectional profile for the struts or the fairing of struts and service lines of a turbofan engine
01/27/2011US20110016882 Electrical Cable Shroud
01/27/2011US20110016881 Gas turbine with exhaust gas casing and method for producing a gas turbine
01/27/2011US20110016880 Retainer for suspended thermal protection elements in a gas turbine engine
01/27/2011US20110016879 Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct
01/27/2011US20110016878 Systems and Methods for Gas Turbine Combustors
01/27/2011US20110016877 Continuous slot in shroud
01/27/2011US20110016873 Fuel control method and fuel control apparatus for gas turbine and gas turbine
01/27/2011US20110016871 Gas turbine premixing systems
01/27/2011US20110016870 Method and apparatus for improved gas turbine efficiency and augmented power output
01/27/2011US20110016868 Fuel spraying apparatus of gas turbine engine
01/27/2011US20110016867 Quarls in a Burner
01/27/2011US20110016866 Apparatus for fuel injection in a turbine engine
01/27/2011US20110016844 Device for reducing turboprop infrared emissions
01/27/2011DE102010036349A1 Systeme und Verfahren für Gasturbinenbrennkammern Systems and methods for gas turbine combustors
01/27/2011DE102010036348A1 Modellgestützte Feinabstimmung einer Ammoniakverteilung und Regulierung, um Betriebskosten einer selektiven katalytischen Reduktion zu verringern Model-based fine-tuning an ammonia distribution and regulation to reduce operating costs of a selective catalytic reduction
01/27/2011DE102010036347A1 Dichtungen für eine Turbinenmaschine und Verfahren zur Montage einer Turbinenmaschine Seals for a turbine engine and method of assembling a turbine engine
01/27/2011DE102010017778A1 Vorrichtung zur Brennstoffeinspritzung bei einer Turbine Apparatus for fuel injection in a turbine
01/27/2011DE10021327B4 Automatisiertes Verfahren zur Herstellung einer Zelle für Wärmetauscher in Wiedergewinnungsvorrichtungen oder Rekuperatoren in Gasturbinentriebwerken, sowie eine nach dem Verfahren hergestellte Zelle An automated method for producing a cell for heat exchangers in recovery devices or recuperators in gas turbine engines, as well as a cell produced by the method
01/26/2011EP2278128A2 Gas turbine with exhaust casing and method for producing such a gas turbine
01/26/2011EP2276920A2 Subsonic and stationary ramjet engines
01/26/2011EP1853795B1 Method for machining an integrally bladed rotor
01/26/2011EP1633935B1 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture
01/26/2011CN201723314U Combustion gas turbine with outer water cooling device
01/26/2011CN201723313U Gas turbine combined cycling device for distributed air and fuel humidification
01/26/2011CN1707162B Gas turbine engine combustor mixer
01/26/2011CN1384794B Supersonic external-compression air ducts, diffuser and air ducts system
01/26/2011CN101960121A Gas turbine and method for maintaining and inspecting the same
01/26/2011CN101960101A Connection structure of exhaust chamber, support structure of turbine, and gas turbine
01/26/2011CN101960092A 涡轮盘及燃气轮机 Turbine and gas turbine disc
01/26/2011CN101959759A Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing
01/26/2011CN101959758A Aircraft engine assembly comprising an annular load-transfer structure surrounding the central casing of a turbojet engine
01/26/2011CN101956608A Seals for a turbine engine, and methods of assembling a turbine engine
01/26/2011CN101956606A Radial turbine engine
01/26/2011CN101410591B Jet engine with detachably arranged generator unit
01/26/2011CN101087928B Static gas turbine component and method for repairing such a component
01/25/2011US7874310 Water cooled liquid fuel valve
01/25/2011US7874164 Fuel nozzle flange with reduced heat transfer
01/25/2011US7874163 Starter generator system for a tip turbine engine
01/25/2011US7874156 Methods and apparatus for heating a fluid
01/25/2011US7874140 Method of and power plant for generating power by oxyfuel combustion
01/25/2011CA2589536C Configurations and methods for lng fueled power plants
01/25/2011CA2466215C Gas turbine stator
01/25/2011CA2442949C Oil-damped bearing
01/24/2011CA2710712A1 Continuous slot in shroud
01/24/2011CA2704873A1 Electrical cable shroud
01/24/2011CA2703388A1 Integrated electrical cable support
01/20/2011WO2011008576A2 Method for removal of entrained gas in a combined cycle power generation system
01/20/2011WO2011008333A1 Heated guide vane
01/20/2011WO2011007303A1 System and method for enhancing engine performance
01/20/2011WO2011007236A2 Gas turbine exhaust gas cooling system
01/20/2011WO2011007078A1 Method and system for controlling aircraft engine starter/generator
01/20/2011US20110014029 Seals for a turbine engine, and methods of assembling a turbine engine
01/20/2011US20110011981 Air intake structure for an aircraft nacelle
01/20/2011US20110011096 System for cooling cooling-air in a gas turbine engine
01/20/2011US20110011095 Washer with cooling passage for a turbine engine combustor
01/20/2011US20110011057 Method for Removal of Entrained Gas in a Combined Cycle Power Generation System
01/20/2011US20110011054 Combustor casing
01/20/2011US20110011052 Gas turbine exhaust gas cooling system
01/20/2011DE19918900B4 Hochtemperatur-Komponente für eine Gasturbine und Verfahren zu deren Herstellung High temperature component for a gas turbine and processes for their preparation
01/20/2011DE102009033592A1 Gasturbinenbrennkammer mit Starterfilm zur Kühlung der Brennkammerwand Gas turbine combustor with starter film to cool the combustion chamber wall
01/20/2011DE102009032277A1 Brennkammerkopf einer Gasturbine Head combustion chamber of a gas turbine
01/20/2011CA2814222A1 System and method for enhancing engine performance
01/20/2011CA2768347A1 Gas turbine exhaust gas cooling system
01/20/2011CA2766446A1 Heated guide vane
01/19/2011EP2275776A2 Method and apparatus for measuring turbine blade tip clearance
01/19/2011EP2275762A1 Method of cooling a hydrocarbon stream and appraratus therefor
01/19/2011EP2275656A2 System for cooling cooling-air in a gas turbine engine
01/19/2011EP2275648A1 System and method for augmenting turbine power output
01/19/2011EP2274205A2 Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle
01/19/2011EP1400755B1 Flanged hollow structure
01/19/2011CN201714491U Gas inlet cooling device of gas turbine based on solution dehumidification
01/19/2011CN201713287U Gas turbine rotor hoisting device
01/19/2011CN1740641B Combustor member and method for making a combustor assembly