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)
12/2003
12/16/2003US6662546 Gas turbine engine fan
12/16/2003CA2342809C Gas turbine and repair method therefor
12/11/2003WO2003102494A2 Flame detection method and apparatus for gas turbine exhaust path
12/11/2003WO2003102424A1 Method for operating a compressor
12/11/2003WO2003102401A1 Integrated cycle power system and method
12/11/2003US20030228483 Thermal spray compositions for abradable seals
12/11/2003US20030228212 Turbine fuel pump
12/11/2003US20030226878 Refractory metal backing material for weld repair
12/11/2003US20030226362 Structural cover for gas turbine engine bolted flanges
12/10/2003EP1369563A2 System for control and regulation of the flame temperature for single-shaft gas turbines
12/10/2003EP1369562A2 Support device for nozzles of a gas turbine stage
12/10/2003EP1369555A1 Device for joining two tubular pieces of an aircraft jet engine
12/10/2003EP1369552A2 Structural cover for gas turbine engine bolted flanges
12/10/2003EP1368560A1 Turbine engine
12/10/2003EP1368228A1 Plenum entry bulk swirl generator
12/10/2003EP1165942B1 Turbo-engine with an array of wall elements that can be cooled and method for cooling an array of wall elements
12/10/2003CN1460786A 燃气涡轮机控制装置 The gas turbine control apparatus
12/10/2003CN1460785A Gas turbine and gas turbin generator
12/10/2003CN1460565A Setting core for pouring cooling channel and reinforcement setting
12/10/2003CN1130522C Combustion chamber having integrated guide blades
12/10/2003CN1130498C Gas turbine suction air-cooling system
12/09/2003US6659716 Gas turbine having thermally insulating rings
12/09/2003US6659714 Baffle cooling device
12/09/2003US6659711 Methods and apparatus for regulating turbine cooling airflow supply systems
12/09/2003US6659472 Seal for gas turbine nozzle and shroud interface
12/09/2003US6659221 Engine intake silencer
12/09/2003US6658855 System for warming pressurized gas
12/09/2003US6658853 Seal structure for combustor liner
12/04/2003WO2003100242A1 Turbine engine apparatus and method
12/04/2003WO2003056284A3 Vibration monitoring system for gas turbine engines
12/04/2003US20030223893 Cooling the upstream end plate of a high pressure turbine by means of a system of dual injectors at the end of the combustion chamber
12/04/2003US20030223892 Compact turbocharger
12/04/2003US20030223863 Gas turbine compressor and clearance controlling method therefor
12/04/2003US20030223862 Methods and apparatus for cooling gas turbine engine nozzle assemblies
12/04/2003US20030223856 Gas turbine and method of bleeding gas therefrom
12/04/2003US20030222458 Method and apparatus for controlling a microturbine
12/04/2003US20030221431 Turbine engine apparatus and method
12/04/2003CA2487417A1 Turbine engine apparatus and method
12/03/2003EP1367690A2 Gas turbine engine and generator directly coupled without reduction gear; Device with electromagnet having amorphous metal core pieces
12/03/2003EP1367325A1 Fuel supply control for a gas turbine including multiple solenoid valves
12/03/2003EP1367251A1 Closure system for an orifice of an air-intake duct of a combustion chamber of a ramjet, as well as ramjet and missile comprising said system
12/03/2003EP1367226A1 Method and system for damage detection of an aircraft engine rotor
12/03/2003EP1367225A2 Gas turbine cooling arrangement and method of bleeding gas therefrom
12/03/2003EP1367224A1 Methods and apparatus for cooling gas turbine engine nozzle assemblies
12/03/2003EP1367221A1 Double injector arrangement for cooling of the sideplate of a high pressure turbine
12/03/2003EP1366322A1 Air assist fuel nozzle
12/03/2003EP1366271A1 Method and apparatus for cooling gas turbine engine blade tips
12/02/2003US6657332 Turbogenerator cooling system
12/02/2003US6655632 System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine
12/02/2003US6655153 Gas turbine shaft and heat shield cooling arrangement
12/02/2003US6655152 Fuel control system for multiple burners
12/02/2003US6655149 Preferential multihole combustor liner
12/02/2003US6655148 Fixing metal caps onto walls of a CMC combustion chamber in a turbomachine
12/02/2003US6655146 Hybrid film cooled combustor liner
12/02/2003US6655123 Device for economizing fuel supply in a fuel supply circuit
11/2003
11/27/2003WO2003098020A2 Gas turbine with stator shroud in the cavity beneath the chamber
11/27/2003WO2003098019A2 Fuel vaporization systems for vaporizing liquid fuel
11/27/2003WO2003098006A2 Turbine no-load speed limiter
11/27/2003WO2003097901A1 Heat insulating layer
11/27/2003WO2003097394A2 Gas turbine power generating system with fuel cell
11/27/2003US20030217548 Gas turbine and gas turbine power generator
11/27/2003US20030217545 Fuel supply control for a gas turbine including multiple solenoid valves
11/27/2003CA2484988A1 Gas turbine power generating system with fuel cell
11/26/2003EP1365343A1 Method and apparatus for managing a maintenance operation
11/26/2003EP1365127A2 Gas turbine engine and method of operating such a gas turbine engine
11/26/2003EP1365107A1 Combustion engine, gas turbine, and polishing layer
11/26/2003EP1040291B1 Noise attenuating device for butterfly valves
11/26/2003CN1457953A Device and method for renewing cooling path in turbine wing surface
11/25/2003US6652914 Method for selective surface protection of a gas turbine blade which has previously been in service
11/25/2003US6652231 Cloth seal for an inner compressor discharge case and methods of locating the seal in situ
11/25/2003US6652226 Methods and apparatus for reducing seal teeth wear
11/25/2003US6652222 Fan case design with metal foam between Kevlar
11/25/2003US6652220 Methods and apparatus for cooling gas turbine nozzles
11/25/2003US6651929 Passive cooling system for auxiliary power unit installation
11/25/2003US6651443 Integrated absorption cogeneration
11/25/2003US6651442 Apparatus and method for determining the status of a valve arrangement forming part of a fuelling system
11/25/2003US6651441 Fluid flow system for a gas turbine engine
11/25/2003US6651440 Steam cooling apparatus for gas turbine
11/25/2003US6651439 Methods and apparatus for supplying air to turbine engine combustors
11/25/2003US6651421 Coleman regenerative engine with exhaust gas water extraction
11/24/2003CA2429511A1 Method and apparatus for managing an operation
11/20/2003WO2003095827A1 Methods for starting a combustion turbine and combustion turbine generator configured to implement same methods
11/20/2003WO2003095812A1 Variable, exhaust-gas turbocharger with an auxiliary drive for an internal combustion engine
11/20/2003WO2003066196A3 A method of treating gas
11/20/2003US20030215329 Turbine nozzle segment and method of repairing same
11/20/2003US20030213871 Flammable fluid line shroud
11/20/2003US20030213249 Bulkhead panel for use in a combustion chamber of a gas turbine engine
11/20/2003US20030213210 Method of constructing a structure for electric cable introduction in an explosion-proof facility
11/19/2003EP1363217A2 Rotation planning apparatus and rotation planning system
11/19/2003EP1363078A2 Bulkhead panel for use in a combustion chamber of a gas turbine engine
11/19/2003EP1363076A2 Multihole patch for combustor liner of a gas turbine engine
11/19/2003EP1362984A2 Gas turbine engine
11/19/2003EP1362933A1 Thermal barrier coating
11/19/2003EP1123457B1 Gas turbine engine
11/19/2003CN1457384A Combustion engine, gas turbine and polishing layer
11/19/2003CN1456795A Gas turbine, integrated circulating device and droplet injector of gas turbine
11/18/2003US6648592 Centripetal air-bleed system
11/18/2003US6648333 Method of forming and installing a seal
11/18/2003US6647732 Gas turbine engine with compressor and turbine inside a hollow shaft
11/18/2003US6647730 Turbine engine having turbine cooled with diverted compressor intermediate pressure air
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