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)
08/2003
08/20/2003EP1248924B1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall
08/20/2003EP1183088B1 Concentric fuel/oil filters and heat exchanger package
08/20/2003EP1177367B1 Seal for sealing a gap, in particular in a turbine, and a turbine
08/20/2003EP1163430B1 Covering element and arrangement with a covering element and a support structure
08/20/2003EP1131548B1 Rotary internal combustion engine
08/20/2003EP1113959B1 Multi-linkage suspension system including outboard isolators
08/19/2003US6607789 Forming nickel-aluminum coating over superalloy by first applying sublayer with smooth finish
08/19/2003US6607358 Multi-component hybrid turbine blade
08/19/2003US6607355 Turbine airfoil with enhanced heat transfer
08/19/2003US6607165 Aircraft engine mount with single thrust link
08/19/2003US6606865 Bellows type outer crossfire tube
08/19/2003US6606864 Advanced multi pressure mode gas turbine
08/19/2003US6606863 Simplification of engine core removal for maintenance of gas turbine engine
08/19/2003CA2264996C Sealing device for axial flow turbine
08/19/2003CA2263508C Sealing device for gas turbine stator blades
08/14/2003WO2003067056A1 Actuator for an air turbine starter valve
08/14/2003WO2003067055A1 Method for operating a gas turbine having several burners
08/14/2003WO2003067053A2 Air turbine starter with fluid flow control
08/14/2003WO2003066430A2 Aircraft fuel tank explosion prevention and smoke alarm response safety improvement method
08/14/2003WO2003066196A2 A method of treating gas
08/14/2003WO2002078010B1 A nuclear power plant and method of operating the same
08/14/2003US20030150206 Engine integrated auxiliary power unit
08/14/2003US20030150205 Exhaust gas housing of a thermal engine
08/14/2003CA2481974A1 Actuator for an air turbine starter valve
08/13/2003EP1335113A1 Fastening device for gas turbine distributor sectors
08/13/2003EP1334309A1 Method and device for supplying fuel to a premix burner
08/13/2003EP1334286A1 Rotary machine with axial stop incorporating a current generator
08/13/2003EP1333921A2 Method of preparing a catalyst layer over a metallic surface of a recuperator
08/12/2003US6606541 Automated system for repairing components
08/12/2003US6605928 Electrical system for turbine/alternator on common shaft
08/12/2003US6604286 Method of fabricating gas turbine fuel injection
08/07/2003WO2003018963A9 Procedure for treating the gas flow, operating in the final part of the steam turbines and the equipment for performing this procedure
08/07/2003US20030147755 Dual drive for hydraulic pump and air boost compressor
08/07/2003US20030147741 Device for controlling the cooling flows of gas turbines
08/07/2003US20030146578 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
08/07/2003US20030146344 Multi-fan system separated core engine type turbofan engine
08/07/2003US20030145603 Micro volume actuator for an air turbine starter
08/07/2003US20030145602 Air turbine starter with fluid flow control
08/07/2003US20030145598 Method of operation of gas turbine having multiple burners
08/06/2003EP1332964A1 Dual drive for hydraulic pump and air boost compressor
08/06/2003EP1332824A2 Method for manufacturing turbine blade and manufactured turbine blade
08/06/2003CN1434197A Gas turbine combined plant and method of operating same
08/05/2003US6603216 Exciter circuit with ferro-resonant transformer network for an ignition system of a turbine engine
08/05/2003US6602542 Device for cleaning an article
08/05/2003US6602328 Gas turbine suction air filter, a gas turbine using the same and a method for using the same
08/05/2003US6602050 Covering element and arrangement with a covering element and a support structure
08/05/2003US6602047 Methods and apparatus for cooling gas turbine nozzles
08/05/2003US6601392 Spring mounted recuperator
08/05/2003CA2263576C Stationary blade of gas turbine
08/05/2003CA2103429C Fuel trim system for a multiple chamber gas turbine combustion system
07/2003
07/31/2003WO2003062618A1 Method for operating a gas turbine group
07/31/2003WO2003062617A1 Gas turbine apparatus
07/31/2003WO2003062605A1 Method and apparatus for increasing welding rates for high aspect ratio welds
07/31/2003WO2003061818A1 Method for making contaminant library, screening method and array plate
07/31/2003US20030144787 Performance enhanced control of dln gas turbines
07/31/2003US20030143074 Method for manufacturing turbine blade and manufactured turbine blade
07/31/2003US20030143063 Rotor assemblies for gas turbine engines
07/31/2003US20030142894 Rotary bearing assembly having a preset breaking point
07/31/2003US20030141383 Liquid atomizing nozzle
07/31/2003US20030141144 Noise attenuation panel
07/31/2003US20030141035 Method and apparatus for directionally solidified casting
07/31/2003US20030140635 Jet fuel and air system for starting auxiliary power unit
07/31/2003US20030140634 Aircraft engine water misting inter-cooler
07/31/2003US20030140633 Hollow structure with flange
07/30/2003EP1331448A2 Fuel control and tuning method for dry low NOx gas turbine engines
07/30/2003EP1331441A1 Liquid atomizing nozzle
07/30/2003EP1331386A2 Multi-turbofan system with separate core engine
07/30/2003EP1331379A2 Tip impingement turbine air starter for turbine engine
07/30/2003EP1331378A2 Separated core turbofan engine
07/30/2003EP1331366A2 Gas turbine combined plant and method of operating the same
07/30/2003EP1331364A2 Flexible coupling of a service tube to a dual shell bearing housing
07/30/2003EP1331363A1 Rotational bearing with a predetermined breaking point
07/30/2003EP1331361A1 Turbine blade and casting device for producing a turbine blade
07/30/2003EP1330593A1 Uninterruptible oil supply system
07/30/2003EP1115963B1 Gas turbine engine
07/30/2003EP1082529B1 Integral inertial particle separator for radial inlet gas turbine engine
07/30/2003EP1082524B1 Fluid deflecting and straining system
07/30/2003CN1432659A High-strength heat erosion resistant and antioxidant directionally solidified super alloy and its product
07/30/2003CN1116508C Method of operating gas-turbine gruop
07/30/2003CN1116500C Seal ring for steam turbine
07/29/2003US6599121 Premix burner
07/29/2003US6599089 Supplemental seal for the chordal hinge seal in a gas turbine
07/29/2003US6599083 Cooling system and method for cooling a turbo-machine housing
07/29/2003US6598801 Methods and apparatus for injecting water into gas turbine engines
07/29/2003US6598781 Article having turbulation and method of providing turbulation on an article
07/29/2003US6598402 Exhaust gas recirculation type combined plant
07/29/2003US6598401 Gas turbine combined cycle plant and compressor
07/29/2003US6598400 Gas turbine with articulated heat recovery heat exchanger
07/29/2003US6598384 Frames comprising hollow enclosures having walls porous to air but impervious to turbulence and debris; protective devices
07/29/2003US6598383 Fuel system configuration and method for staging fuel for gas turbines utilizing both gaseous and liquid fuels
07/29/2003CA2263521C Structure and method for inserting inserts in stationary blade of gas turbine
07/24/2003WO2003060312A1 Turbofan variable fan nozzle
07/24/2003WO2003060303A1 A gas turbine apparatus and a starting method thereof
07/24/2003WO2003060194A1 High-temperature protective coating
07/24/2003US20030139860 Method of detecting in-range engine sensor faults
07/24/2003US20030138319 Draining and cooling system for gas turbine cushions
07/24/2003US20030136147 Compression, expansion, combustion, separation cycles
07/24/2003US20030136130 Gas turbine combined plant and method of operating the same
07/24/2003US20030136103 Fluid flow system for a gas turbine engine
07/24/2003US20030136101 Gas turbine exhaust passage and damper system for same
1 ... 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 225 ... 309