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)
02/2004
02/25/2004EP1390611A1 Method of operating a gas turbine
02/25/2004EP1390606A1 Device for cooling coolant in a gas turbine and gas and steam turbine with said device
02/25/2004CN1478173A Metallic honeycomb cellular seal-structure for turbomachine
02/25/2004CN1477230A Hign temp-resistant article and its mfg. method
02/24/2004US6696774 Magnetohydrodynamic power extraction and flow conditioning in a gas flow turbine
02/24/2004US6695314 Brush seal
02/24/2004US6694746 Micro volume actuator for an air turbine starter
02/24/2004US6694745 Method for running up a gas turbine plant
02/24/2004US6694744 Fuel gas moisturization system level control
02/24/2004US6694738 Retrofit equipment for reducing the consumption of fossil fuel by a power plant using solar insolation
02/24/2004US6694723 Valve assembly for gas turbine engine
02/24/2004US6694722 Recuperator for thermal power installation
02/19/2004WO2004015257A2 Particle separator for a turbine engine
02/19/2004WO2003097394A3 Gas turbine power generating system with fuel cell
02/19/2004US20040033158 Precipitation hardened Co-Ni based heat-resistant alloy and production method therefor
02/19/2004US20040033133 Compressor bleed case
02/19/2004US20040033132 Simplified support device for nozzles of a gas turbine stage
02/19/2004US20040032089 Combustion chamber sealing ring, and a combustion chamber including such a ring
02/19/2004US20040031271 Convoluted seal with enhanced wear capability
02/19/2004US20040031270 Coated seal article with multiple coatings
02/19/2004US20040031269 Method for intermediate cooling and gas turbine system with intermediate cooling
02/19/2004US20040031268 Sulfur deposition control method and related control algorithm
02/19/2004DE20317026U1 Co-axial transmission for propeller drive has planetary transmission non-positively connected to turbine drive shaft
02/19/2004DE20317025U1 Co-axial transmission for impeller drive has planetary transmission non-positively connected to turbine drive shaft
02/19/2004DE10236339B3 Method for manufacturing turbine blades with cooling ducts involves making ceramic core with positioning pins embedded in free end to protrude into surrounding moulding shell for removal during mechanical finishing of hardened blades
02/19/2004DE10228986A1 Verfahren zur Zwischenkühlung sowie Gasturbinenanlage mit Zwischenkühlung Method for intermediate cooling and gas turbine plant with intermediate cooling
02/19/2004DE10152026A1 Warnung vor Pumpgrenze oder Schaufelschaden bei einer Turbomaschine Warning of the surge line or blade damage in a turbomachine
02/18/2004EP1389714A1 Combustion chamber for gas turbine
02/18/2004EP1389690A1 Screw interiorly cooled
02/18/2004EP1389668A1 Gas turbine
02/18/2004EP0894946B1 Gas turbine cooling stationary vane
02/18/2004CN1475663A 燃气轮机装置 A gas turbine plant
02/17/2004US6692228 Rotor insert assembly and method of retrofitting
02/17/2004US6691519 Adaptable modular gas turbine power plant
02/17/2004US6691503 Gas turbine having first and second combustion chambers and cooling system
02/17/2004CA2193165C Cooled turbine vane
02/14/2004CA2437155A1 Noise reduction conduit for static components in aircraft engines
02/13/2004CA2433613A1 Spray method for mcralx coating
02/12/2004WO2004013557A1 Heat exchanger and use thereof
02/12/2004WO2004013465A1 Thermally free aft frame for a transition duct
02/12/2004US20040029058 Method and appliance for supplying fuel to a premixiing burner
02/12/2004US20040028938 Method of making a protective coating forming a thermal barrier with a bonding underlayer on a superalloy substrate, and a part obtained thereby
02/12/2004US20040028816 Reducing particles; injecting liquid; antideposit, antistatic agents
02/12/2004US20040028523 Foreign material exclusion device
02/12/2004US20040027078 Gas turbine engine starter generator with multiple windings on each exciter stator pole
02/12/2004US20040027077 Gas turbine engine starter generator with switchable exciter stator windings
02/12/2004US20040025513 Gas turbine engine
02/12/2004US20040025512 Performance enhanced control of DLN gas turbines
02/12/2004US20040025511 Rapid shutdown and ecology system
02/12/2004US20040025510 Method for operating a gas and steam turbine installation and corresponding installation
02/12/2004US20040025509 Compact rotary ramjet engine generator set
02/12/2004US20040025495 Nested core gas turbine engine
02/12/2004US20040025494 Device for centering a tube in a turbine shaft
02/12/2004US20040025492 Fuel system
02/12/2004US20040025491 Gas turbine set
02/12/2004DE19537636B4 Kraftwerksanlage Power plant
02/12/2004DE10208487B4 Verfahren zur Nutzung der Wärme hocherhitzter Heißluft Procedures for using the heat-high temperature hot air
02/11/2004EP1388656A2 Extraneous matter removing system for turbine
02/11/2004EP1388131A1 Improved fluid metering device
02/11/2004CN1474037A Gas turbine and method for discharging gas from gas turbine
02/10/2004US6689487 Thermal barrier coating
02/10/2004US6688558 Method and apparatus for aircraft inlet ice protection
02/10/2004US6688552 Variable cycle propulsion system with mechanical transmission for a supersonic airplane
02/10/2004US6688534 Air assist fuel nozzle
02/10/2004US6688111 Method for operating a combustion chamber
02/10/2004US6688108 Power generating system comprising a combustion unit that includes an explosion atomizing unit for combusting a liquid fuel
02/05/2004WO2004011685A1 Producing metallic articles by reduction of nonmetallic precursor compounds and melting
02/05/2004US20040023596 Backer inserts for blocking backwall water jet strikes
02/05/2004US20040023056 Metallic material that can be worn away by abrasion; parts, casings, and a process for producing said material
02/05/2004US20040023020 Thermal barrier coating utilizing a dispersion strengthened metallic bond coat
02/05/2004US20040022949 Abradable coating and method for forming same
02/05/2004US20040022661 Nickel-base alloy
02/05/2004US20040022653 Rotary machine with axial stop incorporating a current generator
02/05/2004US20040022624 Stator vane actuator in gas turbine engine
02/05/2004US20040020212 Plate-like body connecting method, connected body, tail pipe for gas turbine combustor, and gas turbine combustor
02/05/2004US20040020187 Blanking-plug system for blanking off an orifice of a pipe, particularly for blanking off an orifice of a duct for introducing air into the combustion chamber of a ramjet
02/05/2004DE10234119A1 Air feed for a gas turbine is cooled in a quench cooler, using water as a coolant, to reduce the air temperature without loss of pressure
02/05/2004DE10232291A1 Active noise abatement appliance has housing containing chamber with opening in one wall to the side of gas flow, with deflector
02/04/2004EP1387046A1 Cooling air system and method for combined cycle power plants
02/04/2004EP1387041A2 Stator vane actuator in gas turbine engine
02/04/2004EP1386070A1 Method for cooling a gas turbine and gas turbine installation
02/04/2004EP1386060A1 Turbine or compressor device and method for assembling the device
02/04/2004EP1385668A1 Method of repairing a turbin blade tip
02/04/2004EP1196977B1 Brush seal
02/04/2004EP1097325B1 Sealing system, especially for a rotary machine
02/04/2004CN1473236A Sealing structure of spindle bolt and gas turbine
02/04/2004CN1472430A Iamge monitoring transfer recording system of carrier tool
02/03/2004US6687596 Diagnostic method and system for turbine engines
02/03/2004US6685431 Method for repairing a turbine vane
02/03/2004US6685425 Inlet bleed heater for heating inlet air to a compressor and methods of fabricating and transporting the heater
02/03/2004US6684898 Dual actuator air turbine starter valve
02/03/2004US6684643 Process for the operation of a gas turbine plant
02/03/2004US6684642 Gas turbine engine having a multi-stage multi-plane combustion system
02/03/2004US6684639 Combustion turbine power generation system and method of controlling the same
02/03/2004US6684623 Gearless electric thrust reverser actuators and actuation system incorporating same
02/03/2004US6684621 Jet engine igniter lead elbow assembly
01/2004
01/29/2004WO2004009980A1 Improved fuel delivery system
01/29/2004WO2004009979A1 Power system and method
01/29/2004WO2004009978A2 Methods and compositions for on-line gas turbine cleaning
01/29/2004WO2004009225A1 Evaporative duplex counterheat exchanger