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)
06/2003
06/04/2003EP1315886A1 Turbo-machine and turbine blade
06/04/2003EP1242990B1 Fan and compressor noise attenuation
06/04/2003EP1216190B1 Integrated engine and transmission units for rotary wing aircraft
06/04/2003EP1117913B1 Fuel preheating in a gas turbine
06/04/2003CN1421594A System for reducing fuel consumption in gas turbine engine
06/04/2003CN1421593A Blocking seal apparatus with heat adaptability
06/03/2003US6572114 Seal ring for steam turbine
06/03/2003US6571563 Gas turbine engine with offset shroud
06/03/2003US6571559 Anti-carboning fuel-air mixer for a gas turbine engine combustor
05/2003
05/30/2003WO2003044374A1 Compressor for gas turbines
05/30/2003WO2003044353A1 Method and apparatus for adaptive acceleration schedules in gas turbine engine control systems
05/30/2003WO2003044352A1 Gas turbine air starter gear assembly comprising a stationary roller shaft and method of manufacturing said roller shaft
05/30/2003WO2003044351A1 Off loading clutch for gas turbine engine starting
05/30/2003WO2003044350A1 Drying machine system utilizing gas turbine, and method of use
05/30/2003WO2003044329A1 Gas turbo group
05/30/2003WO2003044328A1 Gas turbine arrangement
05/30/2003WO2003043779A1 A method for manufacturing a stator or rotor component
05/30/2003WO2003043717A1 Dust collecting filter, dust collecting device, and intake device of gas turbine
05/30/2003WO2003033889A3 Control valve with integrated electro-hydraulic actuator
05/30/2003CA2466914A1 Gas turbine arrangement
05/29/2003US20030099542 Thermally compliant discourager seal
05/29/2003US20030099541 Article wall with interrupted ribbed heat transfer surface
05/29/2003US20030099540 Stationary roller shaft formed of a material having a low inclusion content and high hardness
05/29/2003US20030097872 System for reducing oil consumption in gas turbine engines
05/29/2003US20030097841 Method and device for cooling the inflow area of the shaft of a steam turbine
05/28/2003EP1314957A2 Method and apparatus for measuring turbine blade tip clearance
05/28/2003EP1314872A1 Gas turbine equipment and gas turbine cooling method
05/28/2003EP1314857A2 Controlling turbine blade tip clearance according to thermal growth model
05/28/2003EP1314507A2 Tandem blisk electrochemical machining
05/28/2003EP1313932A2 Thermal barrier coating system for turbine components
05/28/2003CN1420960A Silencer for compressor of exhaust gas turbocharger
05/28/2003CN1420262A Method and device for adjusting cooling blast supply system of turbine
05/27/2003US6568993 Fixture for clamping a gas turbine component and its use in shaping the gas turbine component
05/27/2003US6568903 Supplemental seal for the chordal hinge seals in a gas turbine
05/27/2003US6568192 Gas turbine, gas turbine apparatus, and refrigerant collection method for gas turbine moving blades
05/27/2003US6568191 Coolant recovery type gas turbine
05/27/2003US6568189 Process for controlling the pressure and delivery of a fuel feed to a servovalve unit
05/27/2003US6568168 Gas turbine having water spray injection control
05/27/2003US6568167 Gas turbine having water droplet injector
05/27/2003US6568091 Rotor component displacement measurement system
05/27/2003US6568077 Blisk weld repair
05/27/2003CA2335558C Operating a gas turbine with supplemental compressed air
05/22/2003WO2003042928A2 Fault management system for gas turbine engines
05/22/2003WO2003042504A1 Fan blade with embrittled tip
05/22/2003WO2003023204A3 Redundant prime mover system
05/22/2003US20030094956 Method and apparatus for measuring turbine blade tip clearance
05/22/2003US20030094197 System for injecting fuel into a turbomachine
05/22/2003US20030093999 Combustion chamber dynamic pressure transducer Tee probe holder and related method
05/22/2003US20030093997 Combustion chamber and method for operating said combustion chamber
05/21/2003EP1312816A2 Composite bushing with a monolithic ceramic core
05/21/2003EP1312806A2 Method of engine surge discrimination
05/21/2003EP1312781A2 Method of detecting in-range engine sensor faults
05/21/2003EP1312779A1 Fuel injection system for turbomachines
05/21/2003EP1312763A1 Method and apparatus for regulating turbine cooling airflow supply system
05/21/2003EP1312762A1 Fan blade having a brittle tip
05/21/2003EP1312758A2 Methods and apparatus for cooling gas turbine nozzles
05/21/2003EP1312757A2 Methods and apparatus for cooling gas turbine nozzles
05/21/2003EP1312693A2 Thermal barrier coating material, gas turbine parts and gas turbine
05/21/2003EP1125038B1 Isolated oil feed pipe
05/20/2003US6565324 Turbine blade with bracket in tip region
05/20/2003US6565322 Turbo-machine comprising a sealing system for a rotor
05/20/2003US6565311 Gas turbine steam passage seal structure between blade ring and stationary blade
05/20/2003US6565255 Sensors and methodology for improved turbine exhaust gas temperature measurements
05/20/2003US6564820 Gas flow stop device
05/20/2003US6564557 Cooling arrangement
05/15/2003WO2003040637A1 Device for recovering water from exhaust gas
05/15/2003WO2003040531A1 Gas turbine system comprising closed system between fuel and combustion gas using underground coal layer
05/15/2003WO2003040524A1 Gas turbine stator
05/15/2003US20030093211 Method of engine surge discrimination
05/15/2003US20030091788 Monolithic ceramic attachment bushing incorporated into a ceramic matrix composite component and related method
05/15/2003US20030091459 Superalloy for single crystal turbine vanes
05/15/2003US20030091428 Methods and apparatus for regulating turbine cooling airflow supply systems
05/15/2003US20030091427 Methods and apparatus for cooling gas turbine nozzles
05/15/2003US20030088958 Method and apparatus for correcting airfoil twist
05/14/2003EP1310659A1 Apparatus and method for initiating a combustion reaction with slurry fuel
05/14/2003EP1310632A1 Method and apparatus for correcting airfoil twist
05/14/2003EP1309800A1 Method and system of pulsed or unsteady ejector
05/14/2003EP1309778A1 Compressor starting torque converter
05/14/2003EP1309773A1 Turbine vane system
05/14/2003CN1418286A Method and system for generating power
05/14/2003CN1417462A Cooling system for gas turbine
05/14/2003CN1108441C 燃气轮机 Gas turbine
05/13/2003US6564317 Method and apparatus for securing computer firmware wherein unlocking of nonvolatile memory is prohibited unless address line masking Is disabled during an initialization event
05/13/2003US6561763 Gas turbine engine nose cone
05/13/2003US6561760 Booster compressor deicer
05/13/2003US6561758 Methods and systems for cooling gas turbine engine airfoils
05/13/2003US6561048 Water-flow testing apparatus
05/13/2003US6560966 Method for operating a power plant having turbine cooling
05/13/2003US6560957 Gas turbine installation
05/13/2003US6560870 Method for applying diffusion aluminide coating on a selective area of a turbine engine component
05/13/2003CA2324162C Gas turbine combined cycle system
05/08/2003WO2003038282A1 Warning before pump limit or in case of blade failure on a turbomachine
05/08/2003WO2003038256A1 Gas turbine group
05/08/2003WO2003038255A1 Method for controlling the cooling air mass flows of a gas turbine group
05/08/2003WO2003038254A1 Turbine engine with air cooled turbine
05/08/2003WO2003038244A1 Gas turbine group
05/08/2003WO2003038242A1 Turbine unit
05/08/2003WO2003037715A1 Passive cooling system for auxiliary power unit installation
05/08/2003WO2003008822A3 Enhanced capacity bearing
05/08/2003WO2000046488A3 Turbine engine
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