| 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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| 01/08/2003 | CN1098412C Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same |
| 01/07/2003 | US6505143 Machine protection system for rotating equipment and method |
| 01/07/2003 | US6503349 Heating a repair alloy to a temperature that avoids recrystallization and repair zone incipient melting; rapid cooling and aging; stability of mechanical properties; joint strength; fatique; gas turbine high-pressurue vanes |
| 01/07/2003 | US6503334 Forced mist cleaning of combustion turbines |
| 01/07/2003 | US6502825 Pressure activated cloth seal |
| 01/07/2003 | US6502403 Steam-injection type gas turbine |
| 01/07/2003 | US6502402 Fuel moisturization control |
| 01/07/2003 | US6502401 High pressure bypass sliding setpoint for steam-cooled turbine |
| 01/07/2003 | US6502383 Stub airfoil exhaust nozzle |
| 01/07/2003 | US6502303 Method of repairing a turbine blade tip |
| 01/07/2003 | CA2261744C Combustor flame detecting device |
| 01/03/2003 | WO2003001046A2 Method for operating an internal combustion engine |
| 01/03/2003 | WO2003001042A1 Means for wear reduction in a gas turbine combustor |
| 01/03/2003 | WO2002052211A3 Turbine recuperator |
| 01/03/2003 | CA2451481A1 Means for wear reduction in a gas turbine combustor |
| 01/02/2003 | US20030000602 Integrally bladed rotor airfoil fabrication and repair techniques |
| 01/02/2003 | US20030000222 Turbine equipment |
| 01/02/2003 | US20030000218 Method and apparatus for fuel gas heating in combined cycle power plants |
| 01/02/2003 | US20030000217 Methods and systems for cooling gas turbine engine combustors |
| 01/02/2003 | US20030000216 Gas turbine combustor |
| 01/02/2003 | US20030000214 Gas and steam turbine installation |
| 01/02/2003 | EP1271059A2 Methods and systems for cooling gas turbine engine combustors |
| 01/02/2003 | EP1271057A2 Gas turbine combustor |
| 01/02/2003 | EP1270903A1 Safety device for restarting windmilling turbojet |
| 01/02/2003 | EP1270902A1 Procedure for the start of a gas turbine system |
| 01/02/2003 | EP1270876A2 Spring-backed abradable seal for turbomachinery |
| 01/02/2003 | EP1270875A2 Turbine leaf seal mounting with headless pins |
| 01/02/2003 | EP1270141A2 Method for repairing cracks in a turbine blade root trailing edge |
| 01/02/2003 | EP1269097A1 A heat exchanger |
| 01/02/2003 | EP1269094A2 Method and installation for generating energy |
| 01/02/2003 | EP1269047A2 Improved brush-seal designs for turbines and similar rotary apparatus |
| 01/02/2003 | EP1268982A1 Gas turbine engine stator case |
| 01/02/2003 | EP1268981A1 Turbine installation |
| 01/01/2003 | CN1388306A Combustion gas turbine nited equipment |
| 12/31/2002 | US6502085 Methods and systems for estimating engine faults |
| 12/31/2002 | US6501244 Method and apparatus for controlling a high-speed AC permanent magnet synchronous motor coupled to an industrial turbo engine |
| 12/31/2002 | US6500058 Clogging-free drain system installed in a cutting apparatus |
| 12/31/2002 | US6499938 Method for enhancing part life in a gas stream |
| 12/31/2002 | US6499350 Turbine engine foreign object damage detection system |
| 12/31/2002 | US6499302 Method and apparatus for fuel gas heating in combined cycle power plants |
| 12/31/2002 | US6499285 Particle separator for a gas turbine engine |
| 12/31/2002 | CA2280751C Gas turbine blade |
| 12/31/2002 | CA2261531C Seal active clearance control system for gas turbine stationary blade |
| 12/31/2002 | CA2206160C Process for manufacturing a turbomachine hollow vane and multiple-effect press-kiln used in process operation |
| 12/27/2002 | WO2002103177A1 Method and system for diagnosing state of gas turbine |
| 12/27/2002 | WO2002103176A1 Power generator with low co2 emissions and associated method |
| 12/27/2002 | WO2002103164A1 Multi-stage turbo-machines with specific blade aspect ratios |
| 12/27/2002 | WO2002103075A1 Method for repairing ni base alloy component |
| 12/26/2002 | US20020197155 Abradeable seal system |
| 12/26/2002 | US20020195821 Microturbine/capacitor power distribution system |
| 12/26/2002 | US20020195176 Integrally bladed rotor airfoil fabrication and repair techniques |
| 12/26/2002 | US20020194851 Method for running up a gas turbine plant |
| 12/26/2002 | US20020194733 Method for repairing cracks in a turbine blade root trailing edge |
| 12/25/2002 | CN1386969A Spray-driven air-cooled recessed turbine |
| 12/25/2002 | CN1097176C Air compressor and wall treatment |
| 12/25/2002 | CN1097153C Method and device for monitoring supply system of gas turbine with multiple jet burners |
| 12/25/2002 | CN1097152C Combined generating equipment by using forced-circulation steam boiler as gas turbine radiator |
| 12/25/2002 | CN1097151C Gas turbine power generation equipment and air humidifying apparatus |
| 12/25/2002 | CN1097150C Device for producing energy by means of turbo-machine |
| 12/24/2002 | US6498978 System and method for monitoring thermal state to normalize engine trending data |
| 12/24/2002 | US6497758 Method for applying a high-temperature bond coat on a metal substrate, and related compositions and articles |
| 12/24/2002 | US6497100 Device for controlling the pressure and delivery of a fuel feed to a servovalve unit |
| 12/24/2002 | US6497090 Externally fired combined cycle gas turbine system |
| 12/19/2002 | WO2002101616A1 Filter control method, and filter controlled by the method |
| 12/19/2002 | WO2002101218A1 Rapid shutdown and ecology system for engine fuel control systems |
| 12/19/2002 | WO2002101216A1 Method and installation for energy production by means of a gas turbine associated with an air separation unit |
| 12/19/2002 | US20020192491 Oxidation resistant coatings for niobium-based silicide composites |
| 12/19/2002 | US20020192082 Method for the fuel supply and a fuel supply system for aircraft equipped with at least one aero gas turbine |
| 12/19/2002 | US20020192074 Spring-backed abradable seal for turbomachinery |
| 12/19/2002 | US20020190159 Variable cycle propulsion system with compressed air tapping for a supersonic airplane |
| 12/19/2002 | US20020190158 Variable cycle propulsion system with mechanical transmission for a supersonic airplane |
| 12/19/2002 | US20020189262 Method for operating a steam turbine , and a turbine system provided with a steam turbine that functions according to said method |
| 12/19/2002 | US20020189231 Emergency device for relighting a windmilling turbojet |
| 12/19/2002 | US20020189230 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation |
| 12/19/2002 | US20020189096 Brush seals |
| 12/19/2002 | CA2450031A1 Rapid shutdown and ecology system for engine fuel control systems |
| 12/18/2002 | EP1267310A2 Method and apparatus for managing maintenance operations |
| 12/18/2002 | EP1267121A1 Duct burner diffuser |
| 12/18/2002 | EP1267064A1 Variable cycle propulsion device for supersonic airplanes using diverted exhaust gas and operation method thereof |
| 12/18/2002 | EP1267063A1 Variable cycle propulsion device for supersonic airplanes using mechanical transmission |
| 12/18/2002 | EP1267062A1 Variable cycle propulsion device for supersonic airplanes using diverted compressed air |
| 12/18/2002 | EP0722534B1 Pressurized ball bearing assemblies |
| 12/18/2002 | CN1385281A Method for making and repairing wing surface of integral propeller rotator |
| 12/17/2002 | US6495207 Open cell metal foam core layer bonded to an inner and an outer cladding layer; manufacturing a combustor for a gas turbine engine having an air permeable open cell metal foam core bounded by perforated thin metal or ceramic walls |
| 12/17/2002 | US6494250 Impregnated alumina-based core and method |
| 12/17/2002 | US6494044 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method |
| 12/17/2002 | US6494031 Gas turbine apparatus with heat exchanger |
| 12/12/2002 | WO2002099263A1 Gas turbine arrangement |
| 12/12/2002 | WO2002099254A1 Abradeable seal system |
| 12/12/2002 | US20020188494 Method and apparatus for managing an operation |
| 12/12/2002 | US20020187044 Turbine airfoil and method for manufacture and repair thereof |
| 12/12/2002 | US20020187042 Turbine airfoil with separately formed tip and method for manufacture and repair thereof |
| 12/12/2002 | US20020185243 Impregnated alumina-based core and method |
| 12/12/2002 | US20020185198 Repair of single crystal nickel based superalloy article |
| 12/12/2002 | US20020184891 Architecture for a combustion chamber made of ceramic matrix material |
| 12/12/2002 | US20020184890 Resilient mount for a CMC combustion of a turbomachine in a metal casing |
| 12/12/2002 | US20020184889 Fastening a CMC combustion chamber in a turbomachine using the dilution holes |
| 12/12/2002 | US20020184888 Connection for a two-part CMC chamber |
| 12/12/2002 | US20020184887 Combustion chamber provided with a system for fixing the chamber end wall |
| 12/12/2002 | US20020184886 Fixing metal caps onto walls of a CMC combustion chamber in a turbomachine |