Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
03/2003
03/27/2003US20030056521 Method for gas turbine light-off
03/27/2003US20030056518 Methods and apparatus for operating gas turbine engines
03/27/2003US20030056517 Apparatus and method for combusting low quality fuel
03/27/2003US20030056514 Modular fuel conditioning system
03/27/2003US20030056513 Gas turbine plant
03/27/2003US20030056490 Valve assembly for use in a gas fuel nozzle
03/27/2003CA2423932A1 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
03/26/2003EP1295970A1 MCrAlY type alloy coating
03/26/2003EP1295021A1 Method and apparatus for providing shutoff, overspeed protection, and directional control of a bypass flow in a fuel delivery system
03/26/2003EP1295020A1 Method and apparatus for cooling the inlet air of combustion turbines
03/26/2003EP1295015A1 Combined cycle power generation plant and method of operating such a plant
03/26/2003CN1406160A Device and method for casting a workpiece and workpiece
03/26/2003CN1405438A Gas turbine and method for operating gas turbine
03/25/2003US6537490 Reliable, relatively easy to maintain, inexpensive
03/25/2003US6537027 Turbine no-load speed limiter
03/25/2003US6537023 Supplemental seal for the chordal hinge seal in a gas turbine
03/25/2003US6537021 Increased erosion resistance; gas turbine engine; cubic boron nitride abrasive particles, seal assembly has a CrAlYNiCo superalloy substrate with a bond coat and a porous ceramic abradeable seal
03/25/2003US6537020 Casing structure of metal construction
03/25/2003US6536773 Compliant brush shroud assembly for gas turbine engine compressors
03/25/2003US6536556 Noise reduction sandwich panel, notably for aircraft turbojet engine
03/25/2003US6536457 Fluid and fuel delivery systems reducing pressure fluctuations and engines including such systems
03/25/2003US6536217 Liquid fuel reverse purge
03/25/2003US6536216 Apparatus for injecting fuel into gas turbine engines
03/25/2003US6536206 Apparatus for decreasing combustor emissions
03/25/2003US6536204 Burner configuration for gas turbine
03/25/2003US6536203 Gas turbine installation
03/25/2003US6536202 Jet engine having compressed air net preventing inhalation of objects to prevent FOD
03/25/2003US6536201 Combustor turbine successive dual cooling
03/25/2003US6536110 Providing a hub section formed from a metal alloy; welding an airfoil formed from a metal alloy to hub section; solution treating, heating, oil quenching prior to welding
03/25/2003US6536109 Method for extending the life of attachments that attach blades to a rotor
03/20/2003WO2003023336A1 Methods and apparatus for model based shrouded bellows stiffness determinations
03/20/2003WO2003023214A1 Combustion turbine fuel inlet temperature management for maximum power output
03/20/2003WO2003023207A1 Sealing method and device for a gas turbine shaft
03/20/2003WO2003023204A2 Redundant prime mover system
03/20/2003US20030052557 Rotor coupling having insulated structure
03/20/2003US20030052485 Redundant prime mover system
03/20/2003US20030052230 Compact millimeterwave system for De-icing and for preventing the formation of ice on the outer surfaces of shell structures exposed to meterological influences
03/20/2003US20030051536 Method and apparatus for testing engines
03/20/2003US20030051496 Cogeneration system
03/20/2003US20030051484 Gas turbine engine with compressor and turbine inside a hollow shaft
03/20/2003US20030051483 Simplification of engine core removal for maintenance of gas turbine engine
03/20/2003US20030051481 Combustion turbine cooling media supply system and related method
03/20/2003US20030051460 Safety device for a washing system for liquid fuel burners in gas turbines
03/20/2003CA2459737A1 Methods and apparatus for model based shrouded bellows stiffness determinations
03/20/2003CA2459332A1 Combustion turbine fuel inlet temperature management for maximum power output
03/19/2003EP1293730A2 Safety device for a washing system for liquid fuel burners in gas turbines
03/19/2003EP1293681A1 Mounting device for a turbomachine
03/19/2003EP1293656A2 Gas turbine and operation method of gas turbine combined electric generating plant, gas turbine combined electric generating plant, and computer product
03/19/2003EP1293655A1 Gas turbine, driving method thereof and gas turbine combined electric power generation plant
03/19/2003EP1293645A1 Turbomachine axial compressor with flow splitting device and assembly method for this device
03/19/2003EP1292656A1 Use of nickel compounds as vanadium corrosion inhibitors
03/19/2003EP1292551A1 Protective coating including porous silicon nitride matrix and noble metal
03/19/2003EP1192334B1 Fuel and oil system for a gas turbine
03/19/2003CN1403764A System for supplying thermoelectricity
03/18/2003US6533845 For filtering fluids, such as gas or liquid; useful with gas turbine systems
03/18/2003US6533840 Microchannel laminated mass exchanger and method of making
03/18/2003US6533541 High energy particle arrestor for air turbine starters
03/18/2003US6532840 Methods for robotically inspecting gas turbine combustion components
03/18/2003US6532744 Method for cooling a gas turbine system and a gas turbine system for performing this method
03/18/2003US6532727 Device for the supply of a liquid fuel to a burner member
03/18/2003US6532726 Gas-turbine engine combustion system
03/18/2003US6532656 Gas turbine engine compressor blade restoration method
03/14/2003WO2002025197A1 Thermal shielding brick for lining a combustion chamber wall, combustion chamber and a gas turbine
03/14/2003CA2422557A1 Thermal shielding brick for lining a combustion chamber wall, combustion chamber and a gas turbine
03/13/2003WO2003021149A1 Combustion chamber arrangement
03/13/2003WO2003020469A1 A method for manufacturing a stator or rotor component
03/13/2003WO2003001046A3 Method for operating an internal combustion engine
03/13/2003US20030049126 Joint structure of coolant passage, tube seal, and gas turbine
03/13/2003US20030049118 Axial and radial seal arrangement
03/13/2003US20030047878 Thermally stressable wall and method for sealing a gap in a thermally stressed wall
03/13/2003US20030047298 Device and method for producing a blade for a turbine and blade produced according to this method
03/13/2003US20030046940 Seal structure for combustor liner
03/13/2003US20030046939 Gas turbine, driving method thereof and gas turbine combined electric power generation plant
03/13/2003US20030046938 Apparatus and methods for controlling flow in turbomachinery
03/13/2003US20030046935 Method for injecting fuel into gas turbine engines
03/13/2003US20030046933 Cooling systems and methods of cooling
03/13/2003CA2402932A1 Gas turbine, driving method thereof and gas turbine combined electric power generation plant
03/12/2003EP1291493A2 Transition piece side sealing element and turbine assembly containing such seal
03/12/2003EP1291491A2 Transfer tube for gas turbine coolant passages
03/12/2003EP1291142A2 Method and backer inserts for blocking backwall water jet strikes
03/12/2003EP1109948B1 Multilayer thermal barrier coating systems
03/12/2003EP0865582B1 A coupling device
03/12/2003CN1401939A Combustion chamber unit of gas turbine
03/12/2003CN1401888A Gas turbine controlling apparatus and gas turbine system using same
03/12/2003CN1401887A Insulation structure type rotor coupler
03/12/2003CN1401458A Repair of single crystal nickel superalloy part
03/12/2003CN1103024C Burner for gas turbine
03/11/2003US6531005 Heat treatment of weld repaired gas turbine engine components
03/11/2003US6530229 Gas turbine having a cooling air system and a spray air system
03/11/2003US6530227 Methods and apparatus for cooling gas turbine engine combustors
03/11/2003US6530224 Gas turbine compressor inlet pressurization system and method for power augmentation
03/11/2003US6530211 Quasi-isothermal Brayton Cycle engine
03/11/2003US6530210 Gas turbine
03/11/2003US6530209 Thermal energy reusing system
03/11/2003US6530208 Steam cooled gas turbine system with regenerative heat exchange
03/07/2003WO2003002914A1 Flanged hollow structure
03/06/2003WO2003018977A1 Method for gas turbine light-off
03/06/2003WO2003018976A1 Method of closing working hole in gas turbine blade top
03/06/2003WO2003018963A1 Procedure for treating the gas flow, operating in the final part of the steam turbines and the equipment for performing this procedure
03/06/2003WO2003018962A1 Gas turbine stator housing
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